N716AA

Part: FAN — FAILED (ACM BAY)

MIA - FLT 1845 - EN ROUTE MIA-ANU, ON CLIMB-OUT PASSING 24,000 FEET, HEARD CABIN ALTITUDE HORN. LEFT SIDE PACK MEL. RIGHT SIDE PACK UNABLE TO PRESSURIZE AIRCRAFT. DECLARED EMERGENCY, RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED OUTFLOW VALVE LUTS AND TWO RETAINERS. REPAIRED LEFT SIDE PACK RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - FOUND EMERGENCY AREA LIGHT IN CEILING STATION 680 INOPERATIVE. INSTALLED SERVICEABLE LIGHT ASSY PER MM 33-50-081-4 PAGE 401, OPS CHECK OK. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND BULGE IN SKIN STATION 720A LBL 7. CUT OUT DAMAGED SECTION OF SKIN. BLENDED CORROSION ON STRINGER 28L. FABRICATED AND INSTALLED STRINGER REPAIR IAW ESO 11697, 7-21-00. FABRICATED AND INSTALLED SKIN REPAIR PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND BULGING IN SKIN STATION 670-680 STRINGER 25R. FOUND CORROSION ON SKIN AND SPLICE. REMOVED DAMAGED PRODUCTION SPLICE, CUT END OF DAMAGED STRINGER 6 INCHES. FABRICATED EXTENDED PRODUCTION SPLICE AND INSTALLED PER ESO 11697 DATED 7/26/2000. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LOWER PORTION OF FRAME BETWEEN STRINGER 25L AND 26L. CUT OFF BOTTOM OF FRAME AND INSTALLED REPAIR PER ESO11697 7-27-00 AND SRM 53-10-4 FIG 15. (M)

Part: LAP JOINT — DAMAGED (FUSELAGE)

TUL - FASTENERS POPPED AT SKIN LAP STATION 700 STRINGER 26R, FOUND CORROSION ON SKIN. REMOVED CORROSION, MANUFACTURED AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND BULGE IN SKIN STATION 720B PLUS 12 INCHES, LBL 7. FOUND CORROSION AT SKIN BULGE. TRIMMED OUT DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR AS PER SRM 53-30-3 FIG 3. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - BULGING AND FASTENERS BROKEN STATION 580 STRINGER 26L, FOUND CORROSION AT BULGING. REMOVED FASTENERS AND CORRODED AREA STATION 552-620 AND INSTALLED SKIN LAP DOUBLER PER SRM 53-30-3 PART 1. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FASTENERS CRACKED AND SKIN BULGING STATION 560, STRINGER 26L. FOUND CORROSION IN BULGE AREA. REMOVED FASTENERS AND CORRODED AREAS STATION 552-620 AND INSTALLED SKIN LAP DOUBLER PER SRM 53-30-3 PART 1. (M)

Part: TORQUE BOX — CRACKED (FUSELAGE)

TUL - FOUND TWO 1 INCH LONG CRACKS RIGHT TORQUE BOX. INSTALLED DOUBLER ON RIGHT TORQUE BOX STATION 1243 RIGHT PER SRM 51-40-2, SIZE OF DOUBLER 4 INCHES BY 3 INCHES FASTENERS .1825 INCH AD RIVETS 2 ROWS AROUND DAMAGE, MATERIAL 2024T3.040. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP OF FLOOR SHEAR WEB JUST FORWARD OF LAV WALL, STATION 1130, LBL 38-42. REMOVED CORROSION, ALODINED AND PRIMED AND INSTALLED DOUBLER 4 INCH BY 8 INCH .063 2004 T3 PER SRM 51-40-2 AT STATION 1130 LBL 36-44. (M)

Part: STIFFENER — CORRODED (WING)

TUL - FOUND HEAVY CORROSION ON L/E VERTICAL STIFFENER AT TOP OUTBOARD OF FUEL PRESSURE SWITCHES. INSTALLED NEW STIFFENER AT L/E, OUTBOARD OF FUEL PRESSURE SWITCHES. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND BULGING IN SKIN STATION 700 BETWEEN STRINGER 25L AND 26L, FOUND CORROSION. INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: LIGHT — DEFECTIVE (AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT STAIRWELL LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT AFT STAIRWELL LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS NEAR AFT DOOR INOPERATIVE. RE-SEATED EMERGENCY EXIT PATH LIGHTS CONNECTOR NEAR AFT DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 541-560)

TUL - FOUND CORROSION ON STRINGER 28R 541 TO 560. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED STRINGER REPAIRS PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 480)

TUL - FOUND SKIN BULGED FASTENER HEADS POPPED STATION 480-482 FROM STRINGER 28L TO 2 INCHES OUTBOARD. CUT AND REMOVED CORRODED SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3A. (M)

Part: SKIN — CORRODED (LT WING)

TUL - LEFT LOWER WING SKIN HAS CORROSION IN AREA OF 4C, LBL 30/38/40, ABOVE PRIMARY HEAT EXCHANGER. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED DOUBLER REPAIR PER SRM 57-30-3 FIG 6, SH 2. (M)

Part: SHEAR TIE — CORRODED (BS 540)

TUL - SHEAR TIE CORRODED AT STATION 540 OUTBOARD OF STRINGER 27R. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1 PAGE 4. (M)

Part: SPLICE — CORRODED (BS 480-486)

TUL - FOUND CORROSION ON STRINGER SPLICE STRINGER 28L STATION 480 TO 486. REMOVED STRINGER SPLICE AND INSTALLED STRINGER SPLICE REPAIR PER ESO 11697, DATED 9-1-99. (M)

Part: SKIN — CORRODED (BS 695)

TUL - FOUND STATION 695, STRINGER 24L, SKIN BULGING AT RIVET. CUTOUT CORRODED SECTION OF SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A. (M)

Part: STRINGER — CORRODED (BS 720-740)

TUL - FOUND CORROSION ON 23 LEFT STATION 720F - STATION 740. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)

Part: FITTING — CORRODED (BS 540)

TUL - FOUND STRINGER TIE FITTING CORRODED STATION 540 STRINGER 26R. REMOVED AND REPLACED FITTING PER SRM 51-10-1 PAGE 4 AT STATION 540 STRINGER 26R. (M)

Part: SKIN — CORRODED (BS 685-690)

TUL - FOUND STATION 685-690 STRINGER 25L FUSE SKIN BULGING AT SEVERAL RIVETS. CUTOUT CORRODED SECTION OF SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 3A. (M)

Part: SKIN — CRACKED (BS 720)

TUL - FOUND FUSELAGE SKIN CRACKED (BULGED) AT RIGHT RAM AIR ROD, STATION 720B PLUS 5 INCHES, BELOW STRINGER 28R. CUT OUT DAMAGE IN SKIN 2 INCHES BY 4 INCHES. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. (M)

Part: SHEAR TIE — CORRODED (BS 540)

TUL - FOUND SHEAR TIE CORRODED STATION 540 BETWEEN STRINGER 27R AND 28R. REMOVED AND REPLACED SHEAR TIE AT STATION 540 PER SRM 51-10-1 PAGE 4. (M)

Part: STRINGER — CORRODED (BS 481-482)

TUL - FOUND CORROSION ON STRINGER 28L STATION 481-482. CUT AND REMOVED 3 INCH SECTION OF STRINGER 28L. INSTALLED STRINGER SPLICE REPAIR PER ESO 11697, DATED 9-1-99. (M)

Part: STRINGER — CORRODED (BS 700)

TUL - FOUND CORROSION STRINGER 28 RIGHT STATION 700. FABRICATED AND INSTALLED REPAIR STRINGER AND SPLICES PER SRM 53-10-3. (M)

Part: SKIN — GOUGED (BS 696-704)

TUL - FOUND FUSELAGE SKIN GOUGED BELOW STRINGER 28R STATION 696-704. BLENDED, INSTALLED DOUBLER OVER DAMAGED AREA PER SRM 53-30-3. (M)

Part: FLOORBEAM — CORRODED (BS 5300-5800)

TUL - FOUND CORROSION ON TOP OF FLOORBEAM AT 1127L, STATION 5300 TO 5800. REMOVED CORROSION AND INSTALLED T-ANGLE REPLACEMENT PER SRM 53-12-10-1. (M)

Part: WEB — CRACKED (VENTRAL STAIRS)

TUL - VENTRAL STAIRS, LEFT LOWER TORQUE BOX, CRACK IN WEB AT LIGHTING HOLE, STATION 1243. INSTALLED DOUBLER PER SRM 51-40-2. DOUBLER .050 2024T3, INSTALLED WITH 14 5/32 D-RIVETS. (M)

Part: WEB — CRACKED (VENTRAL STAIRS)

TUL - VENTRAL STAIRS, RIGHT LOWER TORQUE BOX, CRACK IN WEB AT LIGHTING HOLE, STATION 1223. INSTALLED DOUBLER PER SRM 51-40-02. DOUBLER .050 2024T3. INSTALLED WITH 13 .5/32 D-RIVETS. (M)

Part: SKIN — CRACKED (BS 235-250)

TUL - FOUND SKIN CRACKED AROUND FASTENER HEADS AT SECOND FASTENER ROW BELOW LEFT NR 3 COCKPIT WINDOWS STATION 235-STATION 250. INSTALLED REPAIR DOUBLER PER ESO 11697 (M)

Part: LIGHT — INOPERATIVE (PAX DOORWAY)

TUL - FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, CHECKED GOOD. (M)

Part: SKIN — CORRODED (BS 720)

TUL - FOUND CORROSION ON FUSELAGE SKIN OUTBOARD SIDE OF STRINGER 26L FROM STATION 720D PLUS 10 INCH TO 720E. INSTALLED NEW FILLER DOUBLER PER ESO 11697, DATED 9-3-99. (M)

Part: VALVE — DEFECTIVE (RT WING)

SJU - FLT 0680 - EN ROUTE AUA/MIA, NR 2 CROSSFEED VALVE FAILED TO OPEN. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT. CHECKED AND DEFERRED ACCORDING TO MEL. SECURED VALVE OPEN AND FLEW TO MIA WITHOUT INCIDENT. REPLACED NR 2 FUEL MANIFOLD VALVE AND CONNECTOR VALVE. PERFORMED OPERATIONAL CHECK WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (1L DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 1L DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (AC BAY)

ORD - FLT 1948 - DURING CLIMB-OUT AT FL 30, BOTH RIGHT AND LEFT DUCT AND PACK TEMPERATURES STARTED TO RISE WITH SMOKE REPORTED IN AFT CABIN. CREW RAN CHECKLIST AND BOTH PACKS TRIPPED WITH SMOKE DISSIPATING. AIRCRAFT AIR INTERRUPTED AND RETURNED ORD AND LANDED WITHOUT FURTHER INCDIENT. MAINTENANCE FOUND LEFT RAM AIR DOOR CHECK VALVE FROZEN SHUT AND LEFT 35 DEGREE VALVE NOT OPERATING. REPLACED 35 DEGREE VALVE AND REMOVED FROZEN OBSTRUCTION FROM RAM AIR DOOR CHECK VALVE. BOTH PACKS OPERATED NORMALLY AT VARIOUS SETTINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — GOUGED (BS 1183)

TUL - GOUGE AT INSIDE AIRSTAIR PUMP COMP CEILING RT SIDE THROUGH HORIZONTAL FLANGE OF WEB. TRIM WEB AND REPAIRED WITH STAINLESS DOUBLER PER SRM 51-40-2. REPAIRED CHORD PER 51-40-4 AND ESO 11697 DATED 9/3/98. (M)

Part: SKIN — GOUGED (BS 380)

TUL - DEEP GOUGE IN SKIN STATION 380 STRINGER 6L AND 5 TO STRINGER 7L AND 5 AREA ALSO DENTED WHERE GOUGE IS AT. BLENDED GOUGE AND FABRICATED DOUBLER REPAIR, NO CUTOUT REQUIRED PER AARD 53-30-3. (M)

Part: VALVE — DEFECTIVE (MLG WW)

DFW - FLT 1087 - DURING APPROACH, WHEN LANDING GEAR SELECTED DOWN, APPROXIMATE 5 SECOND HESITATION OCCURRED BEFORE LANDING GEAR BEGAN TO EXTEND. LANDING GEAR EXTENDED NORMALLY AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR VALVE. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — CORRODED (WS 5.5)

TUL- LOWER WING SKIN HAS LARGE AREA OF CORROSION UNDER RT SECONDARY HEAT EXCHANGER JUST AFT OF SPLICE (STR 5) RT. INSTALLED REPAIR DOUBLER PER SRM 57-30-3. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: SKIN — CORRODED (BS 700)

TUL - BELLY SKIN BULGING AT ZERO BL AND BS 700. CLEANED AND TREATED REPAIR AREA PER SRM 51-10-02. FABRICATED AND INSTALLED DOUBLER OVER CUT-OUT AREA 4 INCHES BY 11 INCHES PER SRM 53-30-3. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: SKIN — CRACKED (BS 1095/1110)

TUL - 4 EACH CRACKS IN FUSELAGE SKIN BETWEEN STA 1095 - STA 1110, LEFT AND RIGHT OF STR 1. CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR PER SB 727-5311-0204. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: FITTING — CORRODED (NR 4 SPOILER)

TUL - NR 4 SPOILER BOX HAS CORROSION AROUND UPPER INBOARD HINGE FITTING. INSTALLED NEW SERVICEABLE SPOILER BOX. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: SKIN — CORRODED (BS 820)

TUL - LOWER WING SKIN HAS LARGE AREA OF CORROSION UNDER RT SECONDARY HEAT EXCHANGER JUST AFT OF SPLICE. INSTALLED REPAIR DOUBLER PER SRM 57-30-3. APPLY SEALANT TO FASTENER HEADS AND TAILS. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: SKIN — DENTED (BS 400)

TUL - DENT LOWER RT FS 400. DAMAGED AREA 4 INCHES BY 1.75 INCHES AT STR 24R. INSTALLED DOUBLER OVER DENTED AREA SRM 53-30-30614A. DID NOT REMOVE DAMAGED SKIN PER ESO 11697 DATED 1-14-96. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: RIB — CORRODED (LT AILERON)

TUL - OUTBOARD AILERON INBOARD CLOSURE RIB CORRODED. REMOVED AND REPLACED INBOARD CLOSURE RIB PER ESO 2615. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: STRINGER — CORRODED (BS 1030/1050)

TUL - CORROSION ON STA 26R BETWEEN STA 1030 AND STA 1050. REMOVED DAMAGED SECTION AND REPAIRED AT OUTBOARD/INBOARD IN SRM 53-10-3. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: CASTING — CORRODED (NR 6 SPOILER)

TUL - NR 6 SPOILER CASTING HAS CORROSION ON INBOARD AND OUTBOARD SIDES. REMOVED CORRODED CASTING, INSTALLED NEW SERVICEABLE CASTING FOR NR 6 SPOILER. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: DOUBLER — CORRODED (BS 475)

TUL - CORROSION ON UPPER SIDE OF STR 19R AT BS 475 BELOW COOLING AIR EXHAUST DUCT. REPAIRED STRINGER PER SRM 53-10-3. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: CASTING — CORRODED (RT AILERON)

TUL - RIGHT OUTBOARD AILERON MAG CASTING CORRODED BEYOND LIMITS AT NUMEROUS PLACES. REMOVED AND INSTALLED NEW RT OTBD AILERON CASTING. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: FLOOR BEAM — CORRODED (BS 380)

TUL - FLOOR BEAM TOP CORROSION AT BS 380 FROM RBL 24 TO RBL 61. REPAIRED IAW BOEING SRM 53-10-8, PAGE 9A. TST: 70,323.2 HOURS. CYCLES, 48,502. 7(X)

Part: SUPPORT — CORRODED (BS 290)

TUL - CORROSION AROUND FASTENERS ON TOP AND BOTTOM NOSE DRAG BRACE AFT ATTACHMENT PLATFORM AND SIDE SUPPORT STIFFENER. REMOVED AFT NOSE GEAR DRAG BRACE PLATFORM AND BRACKET STIFFENER AND REPLACED WITH NEW SERVICEABLE PARTS. TST: 70,323.2 HOURS. CYCLES, 48,507. (X)

Part: FLOOR BEAM — CORRODED (BS 380)

TUL - WEB BELOW FLOOR BEAM HAD INTERGRANULAR CORROSION FORWARD AND AFT SIDES, RBL 30 TO RBL 61. REPAIRED IAW BOEING 727 SRM 51-40-02, FIG 1, SHEET 3, PAGE 3. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)

Part: SUPPORT — CORRODED (WING)

AFW - NR 1 FLAP TRACK FORWARD SUPPORT HAS CORROSION. REPAIRED PER MRB 727-0022. (M)

Part: FLOOR BEAM — CORRODED (BS 1166)

TUL - FOUND CORROSION ON FLOOR BEAM UPPER FLANGE STATION 1166, LBL 39. CUT OUT CORRODED AREA AND REPAIRED PER SRM 53-10-8 PG 9C-9E. (M)

Part: SKIN — CORRODED (WING CTR SECT)

TUL - FOUND CORROSION ON SKIN INBOARD OF LT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697, DATED 8-9-96. (M)

Part: SKIN — CRACKED (BS 670-680)

TUL - FOUND SKIN BULGED AND CRACKED STATION 670-680 AT STRINGER 26R AT SKIN LAP. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (WING CTR SECT)

TUL - FOUND CORROSION ON SKIN INBOARD OF RT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697 DATED 8-9-96. (M)

Part: STRINGER — CORRODED (BS 480)

TUL - FOUND CORROSION ON SKIN AND STRINGER. REMOVED FASTENERS, CLEANED SKIN. INSTALLED STRINGER REPAIR PER SRM 53-10-5 FIG 1. (M)

Part: DRIVE MOTOR — DEFECTIVE (LT TE FLAP)

IAD - FLT 1089 - AFTER TAKEOFF PHL DURING CLIMB-OUT, SYSTEM A HYDRAULIC LOW LEVEL LIGHT ILLUMINATED AND SYSTEM A QUANTITY DECREASED TO LESS THAN 1 GALLON. AIRCRAFT DIVERTED TO IAD, LANDING GEAR MANUALLY LOWERED, AND AIRCRAFT LANDED IAD WITHOUT INCIDENT. REPLACED LEFT FLAP DRIVE MOTOR AND SERVICED HYDRAULIC SYSTEM A. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SCREWS — LOOSE (LT WING)

IAD - FLT 1267 - AFTER TAKEOFF IAD DURING CLIMB-OUT, FLUID NOTED LEAKING FROM AREA OF LT OUTBOARD AILERON. AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. RETORQUED LOOSE SCREWS AT THIRD FROM WING TIP UNDERWING FUEL TANK ACCESS PLATE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO LEAKS OR SEEPAGE NOTED. (X)

Part: RAFT — DEFECTIVE (FWD STORAGE COMP)

LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION RAFT HAD SEAM SEPARATION. EMERGENCY EVACUATION RAFT SCRAPPED. (X)

Part: STRIP — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RIVETS — FAILED (BS 300-328)

TULE - FOUND SKIN LAP 24R RIVETS PULLING, 1 HEAD SHEARED STATION 300-328. REMOVED CORRODED SKIN LAP. INSTALLED DOUBLER PER SRM 53-30-3 PG 76 THROUGH 80B. (M)

Part: STRAP — DISBONDED (BS 720)

TULE - FOUND BONDED STRAP DISBONDED AT 720C BL 0. REPAIRED STRAP PER SRM 51-40-2, PG 1-6. REPAIRED SKIN PER SRM 53-30-3 PG 8. (M)

Part: DOUBLER — CORRODED (RT WING)

TULE - FOUND CORROSION ON RT PRIMARY HEAT EXCHANGER PLENUM DOUBLER. INSTALLED DOUBLER PER SRM 57-30-3 FIG 10. (M)

Part: SKIN — CORRODED (BS 350-360)

TULE - FOUND CORROSION IN SKIN LAP, RIVETS PULLING. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 35-30-3 PG 80A. (M)

Part: SKIN — CORRODED (BS 682-684)

TULE - FOUND CORROSION ON FUSELAGE SKIN, BEYOND LIMITS, STATION 682-684 BL 6 INCHES L TO 8 INCHES L. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: BEAM — CORRODED (RT HORIZ STAB TE)

TULE - FOUND CORROSION ON RT TRAILING EDGE HORIZONTAL STABILIZER BEAM. REPLACED TRAILING EDGE BEAM TOP OF HORIZONTAL STABILIZER, RT TRAILING EDGE. (M)

Part: SPLICE — CORRODED (BS 675)

TULE - FOUND CORROSION LEFT STRINGER 27L, STATION 675. REPLACED STRINGER SPLICE PER SRM 51-10-1 PG 4. (M)

Part: SKIN — CORRODED (BS 535-540)

TUL - STRINGER 26L, RIVETS PULLING, 1 INCH CRACK AT STATION 535 TO 540. REPAIRED PER SRM 53-30-3 PGS 76-80. (M)

Part: SEAT TRACK — CORRODED (BS 1063-1070)

TULE - FOUND CORROSION ON SEAT/GALLEY TIE DOWN TRACK, STATION 1063-1070, LEFT INBOARD SIDE. INSTALLED NEW TRACK PER SRM 53-10-5. (M)