N507DA

Part: BATTERY — INOPERATIVE (CABIN) · airframe 73,702 hrs · 49,097 cycles

IRREG / L1 DOOR EMERGENCY LIGHT WILL NOT GO BRIGHT . REPLACED BATTERY - OPN CKS NML

Part: LIGHT — BROKEN (CABIN) · airframe 73,561 hrs · 49,005 cycles

EMERGENCY SEAT LIGHT ROW 10D LENS MISSING. REPLACED ASSY, CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,532 hrs · 48,984 cycles

DURING EMERGENCY LIGHT CHECK OUT FOUND RT OUTSIDE OVERWING EXIT LIGHT OUT. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (SEAT 3) · airframe 73,359 hrs · 48,864 cycles

ON LAYOVER FOUND ESCAPE PATH LIGHTING INOP AT SEAT 3AB. FOUND PIN PULLED ON CABLE UNDER SEAT. RESET PIN, OPS CKS GOOD.

Part: MOUNT — CRACKED (NR 3 ENGINE) · airframe 73,336 hrs · 48,849 cycles

ROUTINE HFEC BOLT HOLE INSPECTIONS OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT SUPPORT FITTING REVEALED A CRACK INDICATION IN HOLE G. THE CRACKING IS TYPICAL OF BAC S/B 727-54A0010AND AD 97-05-08. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND A .0312 INCH INSURANCE CUT TAKEN. A LARGER DIAMETER BOLT WAS INSTALLED PER ER/A 378902-14AD.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 72,792 hrs · 48,511 cycles

ON LAYOVER INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR NOT TESTING. REPLACED BATTERIES AND LIGHT OPERATION NORMAL.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 72,545 hrs · 48,352 cycles

L-2 DOOR EMERGENCY O/H EXIT SIGN INOP. REPLACED BATTERY PACK LIGHT, OPS CHECK NORM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 72,492 hrs · 48,319 cycles

DURING LAYOVER, FOUND AFT OVERHEAD CEILING EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CHECKS GOOD PER M/M

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,492 hrs · 48,319 cycles

DURING LAYOVER, FOUND LEFT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. CHECKS GOOD PER MM.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 71,706 hrs · 47,808 cycles

RT OVERWING EMERG EXIT IDENTIFIER INOP ON STANDBY POWER CHECK. REPLACED RACK, OPERATION NML.

Part: SPAR — CRACKED (RT WING) · airframe 71,660 hrs · 47,781 cycles

CRACKS IN AFT SPAR RAIL AT 21 AND 35 FROM I/B END OF FLAP. ALSO DOUBLER SHORT AT 30 FROM O/B END OF FLAP. CORRECTED ON SHOP ORDER NR 957610.

Part: FLAP TRACK — CORRODED (TE FLAP)

DURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS. IN ADDITION, WEAR WAS FOUND AT THE FWD ATTACH LUGS, THE MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. REPAIRED PER ER/A 387331-14AD AND BF GOODRICH ENGINEERING. REPAIR DOCUMENT NUMBER 23-0626.

Part: FLAP TRACK — CORRODED (TE FLAP)

DURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, THE MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. REPAIRED PER ER/A 387302-14AD AND BF GOODRICH ENGINEERING REPAIR NR 23-0630A.

Part: RIB — CRACKED (LE FLAP)

NR 5 SLAT NR 12 RIB CRACKED. REPAIRED PER MM 57-54-0.

Part: SKIN — CRACKED (VERT STAB)

STOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTALL. INSTALLED REPAIR ANGLE PER M/M 55-30-0 PG 803. STRINGER WAS FOUND CRACKED ON VERTICAL STAB.

Part: STRINGER — CRACKED (VERTICAL STAB)

STRINGER 6 RT CRACKED VERT INTERIOR 4TH FRAME DOWN FROM 9504 RIB NR 2. BEGAN FABRICATED REPAIR PER M/M 55-30-0 PG 803. FINISHED FABRICATING REPAIR ANGLE PER M/M 55-30-0 FIG 803. OK TO TREAT AND PAINT. CHEM TREATED AS PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-3-6 NR 3. OK TO INSTALL ANGLE. INSTALLED REPAIR ANGLE PER M/M 55-30-0 FIG 803.

Part: SKIN — CRACKED (LE FLAP) · airframe 71,586 hrs · 47,735 cycles

NR 2 MIDFLAP AFT SPAR DOUBLER CRACKED TWO PLACES AND COVE SKIN CRACKED. REPAIRED PER M/M 57-52-0 FIGURE 802 AND FIGURE 809.

Part: ANGLE — WORN (VERTICAL STAB)

SUPPORT ANGLE WORN VERT STAB LT SIDE JUST FWD OF SLIDING SEAL. REMOVED DAMAGED AREA AND DRILLED UP REPAIR PER SRM 55-30-6D. INSTALLED REPAIR PER SRM 55-30-6D.

Part: RIB — CRACKED (LE FLAP)

SLAT RIB WAS CRACK AT THE O/B LWR AFT END. REPAIRED PER MM 57-54-0 FIG 814.

Part: RIB — CRACKED (LE FLAP)

SLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.

Part: SKIN — CRACKED (LE FLAP)

ANTI-ICE SKIN CRACKED AT 4 LOCATIONS. INSTALLED DOUBLER PER MM 57-54-0.

Part: SKIN — CRACKED (LE FLAP)

SLAT CRACKED. INSTALLED REPAIR DOUBLER PER MM 57-54-0 FIG 814.

Part: RIB — CRACKED (LE FLAP)

SLAT RIB WAS CRACKED AT LWR AFT END NR 2 RIB. INSTALLED A REPAIR DOUBLER PER MM 57-54-0 FIG 814.

Part: ANGLE — CORRODED (NR 2 ENGINE)

ON HEAVY WEIGHT HUSH-KIT MOD, FOUND RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.

Part: ANGLE — CORRODED (NR 2 ENGINE)

ON HEAVY WEIGHT HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT SUPPORT LT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT CHORD ANGLE WITH ONE OF NEW MFG.

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

FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.

Part: SKIN — CRACKED (BS 1234)

FOUND AT A-1 LETTER CK, .5 INCH CRACK IN EMPENNAGE SKIN RT SIDE STA 1234 + STR 22. REPAIRED PER SRM 53-30-3 FIG 25.

Part: TRACK — CORRODED (TE FLAP)

NR 5 INB'D FLAP TRACK AD 90-07-05 AND 90-06-09 TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS. AUTHORIZED MACHINING CORROSION AND WEAR. INSTALLED SPLICE PLATE REPAIR TO MLG BEAM ATTACH PAD AS PER SB 57-0178.

Part: RETURN LINE — CRACKED (NR 2 SPOILER)

SYS A HYD QTY IND DROPPED TO ZERO QTY APPROX ONE HR AND 20 MINS INTO FLT. NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. CHECKLIST PROCEDURE INITIATED LANDING UNEVENTFUL. GROUND INVESTIGATION LEAKING HALF WAY POINT LEFT WING. FOUND NR 2 SPOIL-ER RETURN LINE CRACKED BELOW NR 3 SPOILER. REPLACED LINE WITH TEMP FLEX LINE. CYCLED FLAPS AND SLATS SEVERAL TIMES, NO LEAKS FOUND. NO CLEARANCE PROBLEMS FOUND. THIS WAS AN EMERGENCY LANDING INTO PDX. A/C CALLED 20 MINS OUT BEFORE LANDING IN PDX.

Part: SKIN — CRACKED (BS 360-481)

FUSELAGE SKIN FS 360-481 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED 6 CRACKS IN THREE CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367262-14AD.

Part: SKIN — CRACKED (BS 680-740)

FUSELAGE SKIN FS 680-740 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367266-14AD.

Part: SKIN — CRACKED (BS 481-681)

FUSELAGE SKIN FS 481-681, STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 52 CRACKS ALONG THE PANEL. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367261 -14AD.

Part: SKIN — CRACKED (BS 360-480)

FUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN THREE DIFFERENT FRAME BAYS. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367264-14AD.

Part: LIGHT — INOP (ROW 13)

L-1 AND FWD AISLE AREA EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN THE L-1 DOOR POS AND REPLACED LIGHT ASSY FOR THE FWD AISLE EMERGENCY LIGHT.

Part: WEB — CRACKED (BS 1309)

FOUND ON MV2 CK, .5 INCH CRACK IN THE STA 1309 WEB LEFT SIDE ABOVE THE S DUCT. REPAIRED PER SRM 53-10-4.

Part: WEB — CRACKED (BS 1309)

FOUND ON MV2 CK, 1 INCH AND .5 INCH CRACKS FOUND IN STA 1309 WEB RT SIDE ABOVE S DUCT. REPAIRED PER SRM 53-10-4.

Part: SKIN — CORRODED (BS 720)

THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND LOCAL REPAIR DOUBLERS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365577-14, REV C DATA ANALYSIS WILL BE ACCOMPLISHED WITHIN 12 MONTHS OF THE REPAIR.

Part: SKIN — CORRODED (BS 700)

THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 700 BETWEEN STR 28R AND 28L. THE CORROSION WAS CUT OUT WITH A 9 X 6.5 CUTOUT. THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR FOR ANOTHER SKIN CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS WERE REPAIRED WITH A SINGLE DOUBLER INSTALLED PER THE GUIDELINES OF B727 SRM 53-30-3, FIG 3. THE REPAIR WAS DOCUMENTED PER ER/A 365586-14AD.

Part: WEB — CRACKED (BS 1223)

A .375 INCH CRACK IN TORQUE BOX VERTICAL WEB STA 1223 LT SIDE, ABOVE STAIRS CLOSE OUT PANEL. REPAIRED PER MM 53-11-0.

Part: ANGLE — CORROSION (BS 740)

FOUND DURING MV2 CORROSION VISIT NRC 154, WHILE WORKING NRC 91 FOUND RT SKIN SUPPORT ANGLE CORRODED UNDER STR 27R STA 740. REPLACED SKIN SUPPORT ANGLE PER M/M 53-11-0 PG 859.

Part: FRAME — CRACKED (PAX DOOR)

2 INCH CRACK ON R-1 DOOR AFT FRAME AT LOWER CORNER. REPAIRED PER MM 52-12-0 FIG 804.

Part: STIFFENER — CRACKED (NR 5 SLAT ACT)

A .625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFFENER PER M/M 57-20-21 PG 813.

Part: TRANSFORMER — FAILED (NR 2)

STRONG ELECTRICAL SMELL IN COCKPIT AND FWD CABIN FL 310. FOUND ESSENTIAL T/R AT FAULT. SWAPPED WITH NR 2 T/R AND PUT NR 2 T/R ON MCO.

Part: SKIN — DELAMINATED (LT AILERON)

ON T/C, FOUND LEFT O/B AILERON DELAMINATED BEYOND SRM LIMITS. REPLACED LT O/B AILERON TRAILING EDGE WEDGE.

Part: POWER PACK — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTING FROM ROW 27 AFT INOP. REPLACED POWER PACK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT FLOOR EMERGENCY LIGHTS DID NOT GO ON WHEN TESTED. REPLACED POWER SUPPLY.

Part: BATTERY — DISCHARGED (CABIN)

AFT CABIN EMER TRACK LIGHT SECTION INOP. REPLACED BATTERY PACK AND CHARGER, OPS CK OK.

Part: SUPPORT — CRACKED (NR 6 LE FLAP)

NR 6 L/E FLAP ACTUATOR SUPPORT BRACKET CRACKED AT RADIUS I/B UPPER END AND O/B LOWER END. INSTALLED DOUBLERS PER M/M 57-20-21.

Part: WEB — CRACKED (BS 1228)

WEB CRACKED AT STA 1228 RBL 20 WL208 AT LIGHTNING HOLE. REPAIR PER M/M 53-11-0 PG 832.

Part: ANGLE — CRACKED (NR 2 LE FLAP)

FOUND ON F1 LETTER CK, NR 2 LE FLAP ACTUATOR SUPPORT BOX CRACKED O/B SIDE. REPAIRED PER MM 57-20-21.

Part: RIB — CRACKED (NR 1 LE FLAP)

THIRD FROM OUTBOARD RIB CRACKED, REPAIRED PER M/M 57-54-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR ESCAPE PATH LIGHT FROM SEAT 27 AFT INOP. - REPLACED BATTERY PACK POWER SUPPLY M9027-OPS

Part: LIGHT — INOPERATIVE (CABIN)

OVERHEAD EMERGENCY LIGHT ABOVE AISLE AT SEAT ROW 15 INOP. REPLACED LIGHT ASSY.

Part: AIRSTAIR — NOT LATCHED (AFT AIRSTAIR)

AFT AIRSTAIR FELL OPEN ON T/O ROLL. CHECKED AIRSTAIR OPERATION PER MM. NO TROUBLE FOUND.

Part: BATTERIES — DISCHARGED (CABIN)

O/H CEILING EMER LIGHT AT ROW 13 WOULD NOT TEST. REPLACED BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN)

EMERG TRACK LIGHT DID NOT TEST AT ROW 32. REPLACED SOCKETS AND LENSES, CKS OK.

Part: LENS — MISSING (CABIN)

EMERGENCY TRACK LIGHTS 2 BULBS INOP AND LENSES MISSING AT ROW 36. REPLACED LIGHT SOCKETS AND LENSES.

Part: RELAY — FAILED (CABIN)

EMERGENCY EXIT LIGHTS ILLUM DURING CRUISE WITH SW IN ARMED POSITION. REPLACED CHARGER CONTROL RELAY R70.

Part: WEB — CRACKED (BS 1270)

LOWER TORQUE BOX LIGHTENING HOLE CRACKED .25 INCH AT STA 1270 LT SIDE. ROUTED OUT DAMAGE PER MM 53-11-0 PG 828.

Part: WEB — CRACKED (BS 1213)

VERTICAL WEB OF TORQUE BOX CRACKED AT STA 1213 RT SIDE. INSTALLED DOUBLER PER MM 53-11-0 PG 832.

Part: ANGLE — CORROSION (AC BAY)

FOUND ON D2 LETTER CK, CORROSION AT FWD HINGE ATTACH POINT OF PANEL 3448R. REPAIRED PER MM 53-30-1.

Part: SKIN — CRACKED (VERT STAB)

A .25 INCH CRACK AT FASTENER HOLE LT SIDE OF VERT STAB AT BASE AT STR 10L. INSTALLED DOUBLER PER MM 55-30-0 PG 801.

Part: LIGHT — INOPERATIVE (CABIN)

EMER TRACK LIGHT AT ROW 25 DAMAGED AND DOES NOT ILLUMINATE. REPLACED LIGHT ASSY, OPS NORMAL.

Part: WEB — CRACKED (FUSELAGE)

FOUND DURING D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER MM 53-11-0 PG 828.

Part: BRACKET — CRACKED (NR 5 LE FLAP)

FOUND DURING D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER MM 57-20-21.

Part: BRACKET — CRACKED (NR 5 LE FLAP)

FOUND ON D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-0-21 PG 811.

Part: WEB — CRACKED (LEFT TQ BOX)

FOUND ON D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0 PG 828.

Part: LIGHT — INOPERATIVE (AIRSTAIR)

OVERHEAD EMERGENCY LIGHT AT BOTTOM OF AIRSTAIRS IS INOP. REPLACED LIGHT ASSEMBLY.

Part: SKIN — CORRODED (FS 720)

FUSELAGE SKIN, FS 720 TO 720B S-26R BL 0, CORROSION REPAIR. CORROSION ON THE LOWER SKIN PANEL REQUIRED CUT OUTS IN FOUR AREAS LOCATED FROM FS 720 + 10 TO 720B BETWEEN STRINGERS 26R AND BL 0. TWO OF THE CUT OUTS ARE UNDER THE LAPPED SKIN AT STRINGER 26R. THE FORWARD CUTOUT IS 2.25 BY 1 AND THE AFT IS 2.25 BY 2. THE THIRD IS 16 BY 5.375 LOCATED JUST FORWARD OF STA 720A BETWEEN STRINGERS 28R AND BL 0, THE FOURTH CUTOUT IS 2.75 BY 1.125 AND IS AFT OF STA 720A BETWEEN STRINGER 28R AND BL 0. THIS REPAIR REMOVED THE EXISTING EXTERNAL RING DOUBLER AND ADDED A DOUBLER AND A TRIPLER.

Part: FLOORBEAM — CORRODED (BS 1050)

FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 1050 AT SCREW HOLES TOP AND BOTTOM LBL 60 TO LBL 12. REPAIRED PER M/M 53-20-11.

Part: FLOORBEAM — CORRODED (BS 400)

FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 400 RBL 1. REF NR 90, REPAIRED PER M/M 53-20-11.

Part: FLOORBEAM — CORRODED (BS 400)

FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM AT STA 400 RBL 54. REPAIRED AS PER M/M 53-20-4.

Part: FLOORBEAM — CORRODED (BS 400)

FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 400 RBL 33. REPAIRED PER M/M 53-20-11.

Part: PRESS SW — MALFUNCTIONED (CABIN)

CABIN ALT WARNING HORN WOULD NOT RESET WITH BUTTON. AUTO AND STBY PRESSURIZATION INOP. FWD CABIN ALT WARNING SYS TO MCO 21-00-14.

Part: RIB — CRACKED (NR 6 LE SLAT)

FOUND DURING C-2 LETTER CHECK - SLAT RIB CRACKED .3750 INCH FOR NR 6 ACTUATOR RIB UPPER FLANGE. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 8 LE SLAT)

FOUND DURING C-2 LETTER CHECK - COVE SKIN ANGLE CRACKED FOR NR 8 L/E SLAT UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.

Part: WEB — CRACKED (BS 1250)

FOUND DURING C-2 LETTER CHECK, .1250 INCH CRACK AT LOWER LIGHTNING HOLE AT STA 1250 LT SIDE, ACCOMPLISHED REPAIRS PER M/M 53-11-0.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

FOUND DURING C-2 LETTER CHECK - NR 2 L/E SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED 1 INCH. REPAIRED ANGLE PER MM 57-54-0,

Part: SKIN — DENTED (LT AILERON)

DURING ROUTINE INSPECTION, NR 7865 WAS WRITTEN FOR A DENT IN LT OUTBOARD AILERON UPPER SKIN. DENT WAS REPAIRED PER SRM 57-50-5.

Part: RIB — CRACKED (NR 6 LE SLAT)

UPPER CORNER OF BOTH ACTUATOR RIBS ON NR 6 SLAT WERE FOUND CRACKED. REPAIRS WERE COMPLETED PER THE MM 57-54-0. FOUND AT SHOP VISIT.

Part: RIB — CRACKED (NR 6 LE SLAT)

NR 6 SLAT, SECOND RIB FROM I/B END CRACKED AT LOWER END. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. DAMAGE FOUND DURING SHOP INSPECTION.

Part: ANGLE — WORN (NR 6 LE SLAT)

NR 6 SLAT, ITEM NR 1, INNER CLOSE OUT PANEL LOWER ATTACH ANGLE HAS ELONGATED HOLE 4.5 INCHES FROM I/B END. ITEM NR 2, REPAIR INSUFFICIENT AT LOWER ATTACH ANGLE T-DUCT CUTOUT. REPAIRED BOTH ITEMS PER SRM 57-54-0 FIG 805A.