N2813W

Part: BATTERY PACK — INOPERATIVE (AFT CARGO) · airframe 79,683 hrs · 54,269 cycles

AFT CARGO DOOR EMERG LIGHT INOP. REPLACED POWER PACK

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,340 hrs · 54,037 cycles

OUTBOARD AFT LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND POWER SUPPLY.

Part: BATTERY PACK — INOPERATIVE (FUSELAGE) · airframe 79,340 hrs · 54,037 cycles

EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY AND POWER SUPPLY.

Part: ACTUATOR — FAILED (LT WING SLAT) · airframe 79,225 hrs · 53,959 cycles

ON TAKEOFF NR 2 SLAT ON LEFT WING DID NOT RETRACT. REPLACED NR 2 SLAT ACTUATOR, VISUALLY INSPECTED AND ALL CHECKS OK. SLAT ACTUATOR LEAK AND OPS CKS OK. NR 2 L/E SLAT ACTUATOR INSTALLATION, LEAK CK AND OPS CK OK PER M/M.

Part: STIFFENER — CRACKED (NR 2 SLAT TRACK) · airframe 78,457 hrs · 53,458 cycles

SPAR STIFFENER CRACKED I/B OF I/B TRACK NR 2 SLAT. REPLACED STIFFENER PER MM 57-20-21.

Part: STIFFENER — CRACKED (RT WING SLAT) · airframe 78,457 hrs · 53,458 cycles

NR 7 SLAT I/B TRACK I/B SPAR STIFFENER FOUND CRACKED. DURING E-1 LETTER CHECK.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 78,420 hrs · 53,433 cycles

RT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R/R RT FWD BATTERY PACK OPS CK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 78,284 hrs · 53,344 cycles

A 1 INCH CRACK FOUND ON THE WEB OF THE STA 178 BULKHEAD AT RBL 3 AND WL 197. DAMAGE FOUND ADJACENT TO EXISTING REPAIR. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED FOR CUTOUT MEASURING 7.5 UP/DWN BY 12.5 IB/OB. ER/A 334537-14 REV A.

Part: ACTUATOR — FAILED (NR 8 SLAT) · airframe 78,032 hrs · 53,174 cycles

ON DEPARTURE CLIMB WHEN FLAPS RETRACTED FROM 5 DEG TO 2 DEG, NR 8 LED REMAINED EXTENDED. REPLACED NR 8 SLAT ACT PER M/M, OPS AND LEAK CHECK GOOD.

Part: SKIN — CORRODED (BS 312)

THE FUSELAGE SKIN BELOW THE LAVATORY SERVICE PANEL WAS FOUND WITH AN AREA OF SKIN CORROSION AT STRINGER 20R BETWEEN FS 300 & FS 312. THE CORROSION WAS REMOVED WITH AN 8 X 2 SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368892-14, REV A.

Part: BRACKET — CRACKED (LE FLAP)

NR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED TOP AND BOTTOM RADIUS. REPAIRED PER MM 57-20-21.

Part: INSULATION — SPLIT (NR 1 ENGINE)

ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-24-026-A.

Part: INSULATION — SPLIT (NR 3 ENGINE)

ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-24-026-A.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

NR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 3 SPOILER)

TPA - LTR CHK D-1, NR 3 SPOILER I/B ACTUATOR ATTACH ANGLE CRACKED AT LWR BOLT. REPLACED ANGLE PER MM 57-42-0.

Part: BRACKET — CRACKED (NR 1 LE FLAP)

NR 1 L/E FLAP ACT O/B AND I/B MOUNT BRACKETS CRACKED AT UPPER AND LOWER MOUNT BOLTS. REPAIRED PER MM 57-20-21.

Part: SKIN — CORRODED (BS 720)

FUSELAGE SKIN FS 720 S-28L-28R, REPAIR FOR SKIN CORROSION. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 720 BETWEEN STRINGERS 28L AND 28R, DURING ROUTINE INSPECTIONS PER AD 91-09-09. THE CORRODED AREA OF SKIN WAS CUTOUT AN REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG. 1. THE REPAIR WAS DOCUMENTED PER ER/A 365810-14AD, REV A.

Part: STRINGER — CORRODED (BS 720)

THE FUSELAGE STRINGER AND SKIN AT S-29R WERE FOUND BADLY CORRODED BETWEEN FS 720A+10 AND 720C+10. THE SKIN DAMAGE WAS CUTOUT AND A DOUBLER AND TRIPLER INSTALLED. THE DAMAGED AREA OF STIFFENER WAS REMOVED AND A NEW SECTION SPLICED IN. THE REPAIR WAS ACCOMPLISHED PER ER/A 364137-14, REV A.

Part: SKIN — CORRODED (BS 700)

AN AREA OF CORROSION WAS DISCOVERED ON THE SKIN PANEL AT FS 700, BL 0. THE CORROSION WAS CUTOUT OVER A 7.75 X 6.75 AREA. THE REQUIRED SKIN REPAIR WAS GOING TO INFRINGE ON TWO PREVIOUSLY ACCOMPLISHED SKIN REPAIRS, SO THE PREVIOUS REPAIRS WERE REMOVED AND A NEW SKIN DOUBLER REPAIR INSTALLED TO ENCOMPASS ALL OF THE DAMAGED AREAS. THE REPAIR WAS INSTALLED PER THE SRM GUIDELINES AND DOCUMENTED PER 364097.

Part: WEB — CRACKED (BS 1243)

FOUND ON MV1 CHECK, TWO .375 INCH CRACKS UPPER END OF TORQUE BOX VERTICAL WEB STA 1243. FABRICATED/INSTALLED DOUBLER PER M/M 53-11-0.

Part: SKIN — CRACKED (R1 DOORWAY)

FUSELAGE SKIN R1 DOOR CUTOUT UPPER HINGE CUTOUT, REPAIR FOR CRACK IN REINFORCING DOUBLER (BEAR STRAP). THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WAS FOUND TO HAVE A TYPICAL CRACK IN THE REINFORCING DOUBLER (BEAR STRAP) THE CRACK WAS IN LOCATION D PER BOEING S/B 727-53-0136. THE CRACK WAS REPAIRED WITH A SKIN DOULBER PER THE S/B AND AS DOCUMENTED IN ER/A 364078-14.

Part: ENGINE — FAILED (NR 3 ENGINE)

NR 3 ENG OIL STRAINER CLOG LIGHT ON / ENG SHUT DOWN. DIVERTED TO DFW. FOUND METAL ON CHIP DETECTOR AND FILTER. MTC IN PROGRESS, REPLACING ENG.

Part: SKIN — CRACKED (NR 1 LE FLAP)

FOUND ON L/O CK, NUMBER 1 L/E FLAP CRACKED AT THE INBD HINGE CUTOUT. REPAIRED PER MM 57-30-0 AND ERA 363182-14.

Part: LIGHT — INOPERATIVE (CABIN)

AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WOULD NOT TEST. REPLACED LIGHT ASSY.

Part: SKIN — CRACKED (LT HORIZ STAB)

A 3.75 INCH CRACK IN LOWER SKIN OF LT HORIZONTAL STABILIZER NR 2 BALANCE BOARD ACCESS PANEL. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.

Part: BOLT — SHEARED (STRIINGER 3A)

THE INBOARD TENSION TIE BOLT AT LT S-3A WAS FOUND SHEARED. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING INSPECTED IN ACCORDANCE WITH S/B 727-53-0178, REV 2.

Part: BRACKET — CRACKED (NR 1 LE FLAP ACT)

FOUND ON B1 LETTER CK, .5 INCH CRACK AT NR 1 L/E FLAP ACTUATOR MOUNT BRACKET UPPER INBD CORNER. REPAIRED PER MM 57-20-21.

Part: STIFFENER — CRACKED (LT FRONT SPAR)

A 1.75 INCH CRACK AT FRONT SPAR VERTICAL STIFFENER NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21.

Part: LIGHT — INOPERATIVE (CABIN)

AFT AREA EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY EMERGENCY LIGHTS, CK OK.

Part: BULKHEAD — CRACKED (BS 1183)

A .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8 AND WL 172. REPAIRED PER DELTA ER/A 303629-14AD.

Part: BULKHEAD — CRACKED (STA 1183)

A .5 CRACK FOUND IN 1183 BULKHEAD AT RBL 8 AND WL 172. THIS ERA WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AD 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FORWARD SIDE OF THE 1183 BULKHEAD.

Part: HINGE CUTOUT — CRACKED (L2 DOOR)

FOUND DURING A-2 LETTER CHECK, L-2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.

Part: STRINGER — CRACKED (VERT STAB)

FOUND DURING A-2 LETTER CHECK, 1 INCH CRACK AT STRINGER TO BULKHEAD ATTACH BOLT AT FIN STA 180.6 STR 8 LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.

Part: CHANNEL — CRACKED (FS 1263)

FOUND A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DELTA ER/A 303628-14AD.

Part: TRAVERSE BEAM — CRACKED (FS 1263)

CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B.

Part: SKIN — CRACKED (VERT STAB)

FOUND DURING A-2 LETTER CHECK, TWO .25 INCH CRACKS AT CONSECUTIVE RIVET HOLES LT SIDE OF VERT STAB 10 FT AFT OF NR 2 ENG INLET. REPAIRED PER M/M 54-30-0 FIG 801.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND ON A1 LETTER CK, .5 INCH CRACK AT INBD STOP PAD NUMBER 7 SLAT. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 2 SLAT)

FOUND ON A1 LETTER CK, NR 2 SLAT COVE SKIN ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.

Part: EEL — INOPERATIVE (AFT STAIRWAY)

AFT STAIRWAY EMERGENCY LIGHT INOP. REPLACED BATTERIES, NO HELP. FWD TO MCO AND PLACARD. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.

Part: OVEN — SMOKING (FWD GALLEY)

DURING CRUISE, FLT ATTENDANT REPORTED FWD GALLEY OVEN EMITTED SMOKE AS SOON AS IT WAS TURNED ON. OVEN WAS INSPECTED, PROBLEM COULD NOT BE DUPLICATED, RETURNED TO SERVICE.

Part: STAIR — CRACKED (AFT AIR STAIR)

DURING SHOP INSP, A HOLE IN STR (CTR CHANNEL) 1.5 INCHES FROM THE AFT END WAS FOUND IN AFT AIRSTAIR ASSEMBLY. REPAIRED PER SRM 53-10-8 FIG 1.

Part: DOWNSTOP — CRACKED (NR 2 SLAT)

FOUND AT HMV, NR 2 SLAT DOWNSTOP HAS CRACK WHERE DOWNSTOP CONTACTS. ADJACENT TO DOWNSTOP ON SLAT CORNER, AT UPSTOP. REPAIRED PER MM 57-54-0 PG 820 AND 821, REF NR CARD NR 1672.

Part: DOUBLER — MISINSTALLED (NR 4 TE SLAT)

AT HMV, FOUND DOUBLERS INSTALLED BACKWARDS ON UPPER T/E SKIN OF NR 4 SLAT, NOT AERODYNAMICALLY SMOOTH. INSTALLED DOUBLERS PER SRM 57-50-3 PG 27.

Part: SKIN — DENTED (BS 1061)

AT HMV, FOUND FUS SKIN DENTED AT STA 1061 STR 21L. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER PER SRM 53-30-3 PG 12.

Part: COWL — GOUGED (NR 3 ENG)

AT HMV, NR 3 ENGINE NOSE COWL WAS FOUND WITH GOUGED L/E SKIN. REPAIRED PER SRM 54-30-3 FIG 2.

Part: STRINGER — CORRODED (26RT STA 740)

AT HMV FOUND CORROSION ON STR 26R AT STA 740 FWD BB. TRIMMED AND DRILLED UP STR SPLICE PER SRM 53-10-3.

Part: FLANGE — CRACKED (RT WING STA 656)

AT HMV FOUND FLANGE CRACKED AT RT WS 656.5 AT UPPER STR 4. REPAIRED ANGLES AND PARTS PER MM 57-13-0 FIG 804.

Part: AILERON — GOUGED (LT WING INBD)

AT HMV FOUND LWR SKIN GOUGED/DENTED LT WING INBD AILERON. REMOVED DAMAGE AND FABRICATED REPAIR PER SRM 57-50-5.

Part: STRINGER — CORRODED (BS 740)

DURING HMV, FOUND CORROSION ON STR 27L AND END FITTING AT STA 740. REPAIRED PER SRM 53-10-3 PG 3.

Part: ANGLE — CRACKED (NR 2 TE MID FLAP)

THE NR 2 MID FLAP WAS FOUND TO HAVE THE ATTACH ANGLE AT I/B AFT FLAP TRACK CUTOUT CRACKED. THIS DAMAGED WAS REPAIRED PER MM 57-52-0 PG 807 FIG 802. ALSO, THE THRUST BEARING RETAINER BOLT HOLE CORRODED AT BOTTOM O/B SIDE OF I/B CARRIAGE SUPPORT FITTING. THIS WAS REPAIRED PER SRM 57-50-4 FIG 14. FOUND AT HMV, SHOP INSP.

Part: FRAME — CORRODED (FS 990)

DURING INSPECTION AT HMV, THE FRAME AT STATION 990 WAS FOUND TO HAVE BOTH CORROSION ON BOTH THE VERTICAL AND HORIZONTAL FLANGES OF THE INBD CHORD BETWEEN S-27R AND S-26R. THE CORROSION EXTENDS OVER APPROXIMATELY 3 INCHES ON THE HORIZONTAL FLANGE. IN ACCORDANCE WITH BAC S/B 727-53A0199, REV 1, THE DAMAGE WAS CUT OUT AND SPLICED, PER ERA 301310-14AD.

Part: WEB — CRACKED (FS 950E S26R)

DURING INSPECTION AT HMV, THE C-2 DOOR CUTOUT FRAME AT FS 950E WAS FOUND CRACKED IN BOTH THE WEB AND THE INBD CHORD ABOVE S26R. THE CRACK ON THE CHORD IS IN THE RADIUS OF THE CHORD AND IS APPROX .375 INCH LONG RUNNING FWD AND AFT. ALSO, THERE WAS A WORN AREA AT THE CRACK LOCATION OF THE INBD CHORD. IN ACCORDANCE WITH BAC S/B 727-53A0199 REV 1, THE CHORD WAS SPLICED AND REPAIRED. THE WEB WAS REPAIRED PER E.O. 4-61247-12.

Part: SKIN — DAMAGED (FS 328)

AT HMV, FOUND SKIN DAMAGED AT FS 328 RT SIDE OF NLG OPENING. REPAIRED PER ERA 301438-14.

Part: RIB — CRACKED (NR 4 SLAT)

AT HMV, FOUND LEFT WING NR 4 SLAT WITH RIB NR 7 CRACKED. REPAIRED PER SRM 57-54-0.

Part: SLAT — CRACKED (NR 4 LT)

DURING INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKING IN SUPPORT WEB FOR SPADE FITTINGS.

Part: RIB — CRACKED (NR 1 SLAT)

AT HMV FOUND NR 1 SLAT NR 1 RIB CRACKED AT LWR CLOSEOUT ANGLE. REMOVED AND INSTALLED PER MM 57-54-0.

Part: RIB — CRACKED (NR 1 SLAT)

AT HMV FOUND NR 1 SLAT, NR 2 RIB CRACKED AT UPPER RADIUS. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER MM 57-54-00.

Part: FLOOR BEAM — CORRODED (STA 344/1030)

DURING HMV, FOUND FLOOR BEAMS CORRODED AT STA 344 AND 1030. REPAIRED PER SRM 53-10-8.

Part: FITTING — CRACK (LT BOTTLE PIN)

DURING HMV, FOUND LEFT REAR BOTTLE PIN FITTING INDICATING CRACK AT 10 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7.

Part: RIB — CRACKED (NR 1 SLAT)

AT HMV FOUND NR 1 SLAT, NR 2 RIB CRACKED AT LWR CLOSEOUT ATTACH ANGLE. REMOVED DAMAGED AREA AND MANUFACTURE REPAIR PER MM 57-40-0 PG810.

Part: RIBS — CRACKED (NR 4 SLAT)

A NR 4 SLAT WAS SENT TO SHOP WITH NR 1174 FOR 2 CRACKS ON NR 2 AND NR 4 RIBS FROM I/B END. BOTH RIBS WERE REPAIRED PER SRM 57-54-0 FIG 814.

Part: FLOORBEAM — CORRODED (FS 360)

DURING HMV, UPPER CAP OF CABIN FLOORBEAM FS 360 WAS FOUND CORRODED FROM LBL12 TO RBL 20. REPAIRED FLOORBEAM PER SRM 53-10-8 PG 18 FIG 3.

Part: STRINGER — CORRODED (STR 27 R FS 740)

AT HMV FOUND STR 27R CORRODED AT STA 740 AFT BB. FABRICATED AND INSTALLED PART PER SRM 53-10-3.

Part: BEAM — CORRODED (STA 400)

DURING HMV, FOUND FLOOR BEAM AT STA 400 CORRODED. REPAIRED PER SRM 53-10-8 PG 24 FIG 1.

Part: CAP — CORRODED (FS 420 FLR BEAM)

AT HMV, FOUND LWR SURFACE OF UPPER CAP CORRODED AT FS 420 FLOOR BEAM. DRILLED AND REPLACED SECTION PER SRM 53-10-8 FIG 3.

Part: STRINGER — CORRODED (STA 680-700)

DURING HMV FOUND STR SPLICE CORRODED STR 26L, STA 680-700. REPLACED SPLICE PER SRM 53-10-3.

Part: FILLET PNL — DAMAGED (FUSELAGE)

AT HMV, FILLET PNL 3441 FOUND WITH TIME LIMITED REPAIR. CUT OUT DAMAGE MFG SPLICE REPLACEMENT SECTION AND DOUBLER AS PER SRM 53-30-3 FIG 2, PER 53-50-1 FIG 1. INSTALLED REPAIR PER SRM 53-30-3 FIG 2,PER 53-50-1 FIG 1.

Part: STRINGER — CRACKED (RT WING STA 656)

AT HMV FOUND WING STA 656.5 STR FLANGE CRACKED ON OB END. DRILLED REPAIR AND INSTALLED REPAIR PER MM 57-13-0 PG 801.

Part: FRAME — CRACKED (BS 910)

DURING HMV, FOUND FORMER AT STA 910 LT SIDE CRACKED. REPAIRED PER SRM 53-10-4, FIG 22 PG 87-89

Part: SPOILER — DAMAGED (LEFT WING)

DURING HMV FOUND NR 7 SPOILER HAS A HOLE IN IT AND IB BOTTOM END IS WORN DOWN. MADE BONDED REPAIR PER SRM 51-40-6.

Part: STRINGER — CRACKED (STA 720 B-C)

AT HMV FOUND STRINGER CRACKED AT FS 720 WING LT BOX. FABRICATED SPLICE PER SRM 53-10-3.

Part: STRINGER — CRACKED (STA 720 B-C)

AT HMV FOUND STA 720 B-C STR TIPS CRACKED LEFT SIDE. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3.

Part: ANGLE — CRACKED (AFT ENTRY DOOR)

DURING HMV FOUND AFT ENTRY DOOR BOTTOM ANGLE CRACKED. REPAIRED PER SRM 51-40-3.

Part: RETAINER — CORRODED (LT TE MID FLAP)

THE O/B CARRIAGE THRUST BEARING RETAINER LOWER O/B HOLE CORRODED. ALSO, I/B CARRIAGE THRUST BEARING RETAINER LOWER O/B BOLT HOLE CORRODED. REPAIRED PER SRM 57-50-04 FIG 14. REAMED AND BUSHED HOLES. DURING HMV, FOR NR 1 MID FLAP.

Part: SKIN — DAMAGED (NR 3 FORE FLAP)

727 NR 3 FORE FLAP HAS L/E EDGE DAMAGE 16 AND 22 INCHES FROM I/B END. THIS DAMAGE WAS REPAIRED PER SRM 57-50-4 FIG 1. FOUND AT HMV SHOP INSPECTION.

Part: LE SKIN — WORN (NR 4 MID FLAP)

NR 4 MID FLAP, L/E SKIN WORN AT I/B END OF FLAP. REPAIRED PER MM 575200, REMOVED WORN AREA INSTALLED INLAY AND DOUBLER. AT HMV, SHOP INSPECTION.

Part: SPAR — CRACKED (NR 3 TE MID FLAP)

THE NR 3 MID FLAP, LOWER AFT SPAR RAIL CRACKED 19 INCHES FROM I/B END OF FLAP. REPAIRED PER MM 57-52-00 PG 807. SPLICED IN NEW SECTION OF RAIL. DURING HMV SHOP INSPECTION.

Part: RIB — CRACKED (LT TE MID FLAP)

THE NR 1 MID FLAP I/B AFT RIB CRACKED. REPAIRED PER SRM 57-52-00 FIG-808. INSTALLED DOUBLER. FOUND AT HMV SHOP INSPECTION.

Part: SKIN — DAMAGED (RT OUTBD AILERON)

DURING HMV, FOUND OUTBD AILERON OUTBD TAB ROD END LOOSE. REPLACED TAB ROD END AND REPLACED SECTION OF UPPER SKIN PER SRM 57-50-5 FIG 3.

Part: DOUBLER — WORN (TE SPOILER)

SMALL HOLE WORN IN 3 IN DOUBLER ON BOTTOM T/E OF SPOILER, MADE BONDED REPAIR PER SRM 51-40-6.

Part: SKIN — DAMAGED (NR 8 SPOILER)

DURING INSPECTION, NR 8 SPOILER PANEL WAS FOUND DENTED AND DELAMINATED ON LOWER SKIN. MADE BONDED REPAIR PER SRM 57-40-6 WITH REF TO 51-40-6.