N497DA

Part: FRAME — CRACKED (C1 DOORWAY)

THE WEB OF THE C1 DOOR CUTOUT AFT JAMB WAS FOUND WITH A SMALL CRACK EMANATING FROM A FASTENER HOLE JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS REPAIRED WITH A DOUBLER PER ER/A 368332-14.

Part: STIFFENER — CRACKED (NR 3 SLAT TRACK)

NR 3 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. NR 3 SLAT I/B TRACK O/B SPAR STIFFENER CRACKED. REPLACED STIFFENERS PER M/M 57-20-21 PG 813.

Part: STIFFENER — CRACKED (RT WING)

REF SHIP 497 TPA LTR CHK D-1, NR 7 SLAT I/B TRACK I/B L/E SPAR STIFFENER CRACKED. REPLACED STIFFENER PER MM 57-20-21.

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATT PACK, OPS NOW OK.

Part: BATTERIES — DISCHARGED (LT EMER EXIT)

LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NORMAL.

Part: ACTUATOR — FAILED (NR 4 LE SLAT)

ON APP FLAP EXT 2 TO 5 AMBER L/E FLAP LIGHT REMAINED ILLUM. POSITION TEST SHOWED NO LIGHT FOR LEFT NR 4 SLAT RETRACTED. PERFORMED APP PER POM. C/W PROCS FOR LANDING. TAXIING AFTER LAND UPON FLAP RETRACTION, LOST A HYD SYS FLUID. PERFORMED PROCS AS PER POM. STOPPED A/C AND TOWED IN. REPLACED LT WING NR 4 SLAT ACT PER MM, LEAK CHECK OK. HYD SERVICED, LIGHTS AND OPN CKS NORMAL. SECURED ACCESS PANELS RII C/W PER CVG QA.

Part: LIGHT — INOPERATIVE (AFT STAIR LIGHT)

AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT.

Part: SKIN — CRACKED (BS 440-460)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED TWO CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A366797-14AD, REV B.

Part: SKIN — CRACKED (BS 481-680)

LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 54 CRACK INDICATIONS ALONG THE LENGTH OF THE PANEL. THE LAP SPLICE WAS CUTOUT ALONG ITS ENTIRE LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366795-14AD, REV A.

Part: SKIN — CRACKED (BS 681-740)

LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN PANE AT THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 38 CRACKS ALONG THE LENGTH OF THE PANEL. THE SKIN LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366796-14AD, REV A.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND ON LETTER CK, C-2 - .5 INCH VISIBLE CRACK IN LT FRAME OF AFT ENTRY DOOR CUTOUT AT DATA PLATE. REPAIR PER SRM 53-10-9.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND AT LETTER CHECK C-2, .5 INCH VISIBLE CRACK IN RT FRAME OF AFT ENTRY DOOR CUTOUT AT 2ND FROM TOP STOP CASTING. REPAIRED PER SRM 53-10-9.

Part: SKIN — CRACKED (R-1 DOOR)

REF SHIP 497 TPA LTR CHK C2, TWO SMALL CRACKS UPPER AFT CORNER UPPER HINGE CUTOUT, R1 DOOR SKIN. REPAIRED PER MM 52-11-01.

Part: TIP — DAMAGED (RT WING)

FLAP FAIRING RT WING TIP DAMAGED ON LANDING. FOUND ON INSP RT O/B AILERON AND TAB DAMAGED, NR 4 AFT FLAP AND FAIRING DAMAGED, RT WING TIP DAMAGED O/B EDGE. REPAIRED ALL.

Part: OXYGEN BOTTLE — EMPTY (E/E COMPT)

CREW OXYGEN READS ZERO, SUSPECT REGULATOR AT JUMPSEAT STUCK IN EMERGENCY POSITION. FREED JUMPSEAT 02 SWITCH, REPLACED CREW O2 BOTTLE LEAK AND OPS CKS OK.

Part: BEAM — CRACKED (BS 1263)

THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK IN THE FS 1263 BEAM. THE CRACK IS TYPICAL OF BAC S/B 53-0129. THE CRACKED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365003-14AD.

Part: FLOORBEAM — CORRODED (BS 1110)

CORROSION FOUND ON STA 1110 FLOORBEAM O/B OF RT SEAT TRACK. REPAIRED PER SRM 53-20-11 PG 811B.

Part: BULKHEAD — CRACKED (BS 277)

THE RT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL WAS FOUND WITH A .75 VERTICAL CRACK AT FS 277. THE CRACK IS TYPICAL OF BAC S/B 727-53-0145. THE CRACK WAS CUTOUT AND A DOUBLER INSTALLED PER SRM 51-40-2. A PORTION OF THE S/B MODIFICATION WAS ALSO INSTALLED AT THE DAMAGE LOCATION. THE REPAIR WAS DOCUMENTED PER ER/A 364683-14AD.

Part: SKIN — CRACKED (FUSELAGE)

FOUND ON C1 LETTER CK, .75 INCH CRACK FUSE SKIN UPPER AFT CORNER OF R-5 WINDOW CUTOUT. REPAIR PER MM 53-30-3.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT OVERWING EMERGENCY LIGHT WAS INOP. FOUND THAT BATTERY PACK WAS DEAD. REPLACED BATTERY PACK WITH NEW, OPS NML.

Part: REAR SPAR — CRACKED (RT ELEVATOR)

THE REAR SPAR OF THE RT ELEVATOR IS CRACKED IN TWO LOCATIONS. THERE IS A CRACK MEASURING .099 EMANATING FROM THE SHEAR PLATE AT THE SECOND FROM THE O/B HINGE, AND THE OTHER IS .167 EMANATING FROM THE SHEAR PLATE AT THE THIRD FROM THE O/B HINGE. THIS ER/A AUTHORIZES A TIME LIMITED STOP DRILL REPAIR PER THE REFERENCED SERVICE BULLETIN (S/B 727-55-0089) BASED ON THE RESTRICTIONS IN THE AD (96-06-05). REPETIVE INSPECTIONS WILL BE ACCOMPLISHED WITHIN 1,600 FLIGHT HRS AND PERMANET REPAIR WILL BE ACCOMPLISHED WITHIN 3,200 FLIGHT HRS OF 25 SEPT 97.

Part: WEB — CRACKED (BS 870)

FOUND ON B2 LETTER CK BS 870 WEB CRACKED AT RT INBD KEEL BEAM SUPPORT ANGLE. REPAIRED PER SRM 53-10-9 TIME LIMITED INST.

Part: ANGLE — CRACKED (BS 870)

KEEL BEAM SUPPORT ANGLE CRACKED THROUGH, FWD SIDE OF STA 870 RT SIDE OF KEEL BEAM. REPLACE ANGLE REF M/M 53-10-9 F13.

Part: ANGLE — CRACKED (RT ELEVATOR)

REPAIR ANGLE CRACKED RT ELEVATOR HINGE RIB STA 136. REPLACED REPAIR ANGLE REF 55-10-31 FIG 803.

Part: VALVE — FAILED (RT MLG)

ON T/O AFTER GEAR HANDLE WAS RAISED, HYD SYS A PRESS AND QTY WENT TO 0. REPLACED RT MAIN LANDING GEAR SEQUENCING VLV.

Part: WINDOW — CRACKED (RT COCKPIT)

R-1 WINDOW CRACKED INFLIGHT. RETURNED TO ATL. REPLACED WINDOW.

Part: HYD LINE — CRACKED (TAILSKID)

LOST A-SYS HYDS GEAR DOWN FLAPS 25 DEGREES BOTH PRESSURE AND QTY ZERO. FOUND LINE TO TAIL SKID HYDRAULIC ACTUATOR BROKEN IN FITTING LOCATED IN LEFT REAR CARGO COMPARTMENT. REPAIRED SAME.

Part: CHANNEL — CRACKED (BS 1263)

FOUND A 1 INCH CRACK IN THE CHANNEL AT FS 1263, TORQUE BOX. REPLACED PER BOEING S/B 53-0129.

Part: BULB — FAILED (COCKPIT)

EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WILL NOT TEST. RELAMPED, OPS CHECKS OK.

Part: BATTERIES — DISCHARGED (CABIN)

L1 AND COCKPIT DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN RACKS, BOTH OP CHECK GOOD.

Part: BEAM ANGLE — CRACKED (AFT STAIR)

TORQUE BOX BEAM ANGLE CRACKED BELOW FORWARD ACTUATOR ATTACH FITTING. REPLACE CRACKED ANGLE. REF: E.O. 4-061071-12.

Part: BATTERIES — DISCHARGED (L1 DOOR)

EMERGENCY EXIT LIGHT AT L1 DOOR INOP. REPLACED BATTERIES, CKS GOOD.

Part: FUSE — FAILED (CABIN)

ON PREFLIGHT, EMERGENCY TRACK LIGHTS FOUND INOP. REPLACED FUSES AT EMERGENCY EXIT PATH BATTERY PACKS. CHECKED WIRING SYSTEM AND OPERATION NORMAL.

Part: SKIN — CRACKED (NR 8 LE SLAT)

FOUND DURING A-1 LETTER CHECK, NR 8 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.

Part: SKIN — CRACKED (NR 7 LE SLAT)

FOUND DURING A-1 LETTER CHECK, NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.

Part: ANGLE — CRACKED (RT WING LE)

FOUND DURING A-1 LETTER CHECK, NR 6 L/E FLAP ACTUATOR I/B ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PAR 12.

Part: EEL BATTERY PACK — DISCHARGED (CARGO DOOR)

DURING LAYOVER, EMERGENCY LIGHT AT C-2 CARGO DOOR INOP. REPLACED BATTERY PACK M957, OPERATION NORMAL.

Part: FAIRING — CRACKED (WING)

AFT MOUNT HOLES ENLARGED, WELDED AS PER MM 57-52-0 2. CRACK IN CLOSEOUT PANEL UNDER GUIDE PIN. REPAIRED PER SRM 51-40-2. REPAIRS FOUND AT SHOP INSP FOR AFT O/B FLAP TRACK FAIRING.

Part: BEAR STRAP — CORRODED (FS 1137)

DURING OVERHAUL, THE C-3 DOOR INTERNAL BEAR STRAP (.125 THICK 2024-T42 BARE) WAS FOUND CORRODED AT STA 1137 AND STA 1094, STR 27R. IN ACCORDANCE WITH FAA/DER FORM 8110, DATED 09 JUNE 1995, AN INTERNAL TITANIUM REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION.

Part: BEARING — FROZEN (NR 1 ELEV)

AT HMV, FOUND ELEV TO STAB BEARING FROZEN, NR 1 ELEV TO STAB MOUNT WORN. REPAIRED PER MM 55-50-0.

Part: S DUCT — BENT (NR 2 ENGINE)

AT HMV FOUND S-DUCT LE RIM BENT AND WORN. REPAIRED PER SRM 54-10-3 FIG 13.

Part: DOUBLER — CRACKED (R1 DOOR AREA)

DURING HMV, A CRACK WAS FOUND IN THE DOORWAY SURROUND DOUBLER AT THE UPPER FORWARD CORNER OF THE UPPER HINGE CUTOUT AT THE R1 DOOR. IN ACCORDANCE WITH BAC TWX DAL-ATL-95-0573RR DATED 30 MAY 1995, THE CRACK WAS STOP DRILLED AND A EXTENRNAL DOUBLER WILL BE USED AS PER BAC S/B 727-53-0136.

Part: SKIN — CORRODED (FS 720)

CORROSION ON SKIN AFT OF STA 720 BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-30-3 FIG 1, FOUND AT HMV.

Part: SKIN — CRACKED (NR 6 LE SLAT)

NR 6 L/E FLAP HAD A CRACK AT I/B HINGE FITTING AFT END. REPAIRED PER SRM 57-50-03 PG 32.

Part: SKIN — CRACKED (NR 6 LE FLAP)

NR 6 L/E FLAP HAD A PREVIOUS REPAIRED CRACK WHICH CRACKED FURTHER. REPAIRED PER SRM 57-50-3, FOUND AT HMV.

Part: DOUBLER — CRACKED (NR 3 TE MIDFLAP)

DOUBLER CRACKED AT AFT CHORD ANGLE 19 INCHES FROM I/B END. REMOVED AND REPLACED DOUBLER PER MM 57-52-0, NR 3 MIDFLAP AT HMV, SHOP VISIT.

Part: STRINGER — CORRODED (FS 540)

FWD B/B STR 28R CORRODED ON UPPER FLANGE, JUST FWD OF STA 540. REPAIRED PER SRM 53-10-3 PG 4C, FOUND AT HMV.

Part: STRINGER — CRACKED (WS 546)

DURING HMV, FOUND LT WING STRINGER 8 AT STA 546.5 CRACKED. REPAIRED PER M/M 57-13-0 PG 801.

Part: SKIN — DAMAGED (FS 480-680)

AT HMV, FOUND NUMEROUS TEMP REPAIRS ON FWD B/B LWR SKIN STA 480 TO 680. INSTALLED AND FABRICATED NEW SKIN PANELS PER SRM 53-30-3.

Part: INLET — CRACKED (NR 2 ENGINE)

NR 2 ENGINE INLET AFT LWR EDGE, BENT AND CRACKING IN SEVERAL PLACES. REPAIRED PER SRM 54-10-3.

Part: RIB — CRACKED (NR 4 LE SLAT)

AT HMV, FOUND NR 4 LE SLAT 4TH LE RIB FROM OB END IS CRACKED. DRILLED UP AND INSTALLED NEW DOUBLER PER MM 57-54-0 PG 806.

Part: RIB — CRACKED (NR 2 SLAT)

AT HMV, FOUND 2ND FROM IB RIB CRACKED IN THE NR 2 SLAT LE. REPAIRED PER MM 57-54-0 PG 819.

Part: RIB — CRACKED (NR 5 LE SLAT)

AT HMV, FOUND NR 5 LE SLAT 10TH RIB FROM IB END CRACKED. REPAIRED PER MM 52-54-0 PG 819.

Part: RIB — CRACKED (NR 4 LE SLAT)

AT HMV, FOUND NR 4 LE SLAT 11TH RIB FROM OB END CRACKED. INSTALLED NEW DOUBLER PER MM 57-54-00 PG 812.

Part: RIB — CRACKED (NR 2 LE SLAT)

AT HMV, FOUND NR 2 LE SLAT 3RD RIB FROM IB END IS CRACKED. REPAIRED PER MM 57-54-0 PG 819.

Part: FLOORBEAM — CORRODED (FS 328)

FOUND AT HMV, MOUNT HOLES CORRODED FLOOR SUPPORT ANGLE AT L-1 DOORWAY, STA 312 THROUGH 360. HOLE CORRODED FLOORBEAM STA 328, LBL 45. REPAIRED PER MM 53-20-11 FIG 804A.

Part: RIB — CRACKED (NR 7 LE SLAT)

AT HMV FOUND NR 7 L/E SLAT RIB IB OF TAI DUCT CRACKED. INSTALLED DOUBLERS PER MM 57-54-0 PG 819.

Part: RIB — CRACKED (NR 7 LE SLAT)

AT HMV FOUND NR 7 LE SLAT RIB CRACKED 2ND FROM OUTBOARD END. INSTALLED DOUBLER AND STOPPED DRILL CRACK PER M/M 57-40-0 PG 819.

Part: ANGLE — WORN (NR 2 COWL)

AT HMV, THE NR 2 ENGINE FWD COWLING CLOSEOUT RIM AT STA 1352 IS DAMAGED AND WORN FROM 5 TO 7 O'CLOCK POSITION. REPAIRED PER MM 53-11-0 PAGE 801.

Part: FRAME — CORRODED (FS1070)

AT HMV FOUND FORWARD LOWER FLANGE OF FRAME 1070 CORRODED LOC BETWEEN STR 30 AND 29R. INSTALLED NEW CLIP PER MM 53-11-0.

Part: FRAME — CORRODED (FS 970)

FRAME 970, CORROSION FWD SIDE BETWEEN STR 28R AND 27R. REPAIRED PER MM 53-11-0 PG 825.

Part: RIB — CRACKED (NR 7 LE SLAT)

RIB CRACKED, NR 7 L/E SLAT, 2ND RIB FROM I/B END. REPAIRED PER MM 57-54-0 PG 819, FOUND AT HMV.

Part: RIB — CRACKED (NR 3 LE SLAT)

RIB CRACKED NR 3 L/E SLAT. THE 7TH RIB I/E END SLAT IS CRACKD AT NUT LOCATION. INSTALLED REPAIR PER MM 57-54-0 PG 807, FOUND AT HMV.

Part: RIB — CRACKED (NR 3 LE SLAT)

AT HMV, FOUND NR 3 L/E SLAT 19TH RIB FROM IB END SLAT CRACKED. REPAIRED RIB PER M/M 57-40-0 PG 819.

Part: FRAME — CORROSION (FS 950)

FOUND AT HMV, FRAME 950C CORROSION LWR SIDE BETWEEN STR 30 AND 29R. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER MM 53-11-0 PG 825.

Part: STRINGER — CRACKED (FS 720)

DURING HMV, FOUND STR 15L CRACKED AT STA 720C. REPAIRED PER SRM 53-10-3 DETAIL 2 FIG 2.

Part: STRINGER — CRACKED (FS 720)

DURING HMV, FOUND STR 15L CRACKED AT STA 720B. REPAIRED PER SRM 53-10-3.

Part: FRAME — CRACKED (FS 560)

AT HMV, FOUND TOP OF FRAME CRACKED AT STA 560, 6 INCHES RBL ABOVE INTERCOSTAL. FABRICATED AND INSTALLED REPAIR PER ERA 301859-14.

Part: CLIP — CORRODED (FS 720)

SKIN CLIP CORRODED FS 720 FRAME FWD SIDE BETWEEN STR28L AND R. REPAIRED PER MM 53-11-0 FIG 815, FOUND AND REPAIRED AT HMV.

Part: FRAME — CRACKED (R1 DOORWAY)

AT HMV, FOUND R1 DOORWAY FWD FRAME CRACKED AT BOTTOM CORNER. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4 PG 23.

Part: STRINGER — CRACKED (WS 629)

AT HMV, FOUND RT WING UPPER STR TO RIB CRACKED AT WS 629.00 2ND STR AFT OF VENT BOX. INSTALLED REPAIR DOUBLER PER M/M 57-13-0 PG 801.

Part: FLANGE — DAMAGED (FS 950)

AT HMV TRANS FROM SCH MTC SHEET, PERM REPAIR SKIN FLANGE NEAR FS 950 STR 18A LT REM TEMP REPAIR INSTALLED NEW REPAIR PER M/M 53-12-0.

Part: FRAME — CRACKED (FS 312)

DURING HMV, FOUND FRAME AT STA 312 CRACKED AT STR 13R. REPAIRED PER SRM 53-10-4 FIG 1 DETAIL 3.

Part: DOUBLER — CRACKED (NR 3 MIDFLAP)

NR 3 MIDFLAP, NR 6447 DOUBLER CRACKED IN TWO PLACES AT AFT CHORD ANGLE 29 FROM I/B END. REPAIRED PER M/M 575200 FIG 802. REMOVED AND REPLACED DOUBLER. NR 6449 AFT LOWER SPAR ANGLE DOUBLER IMPROPERLY INSTALLED 40 FROM O/B END. REPAIRED PER M/M 575200 FIG 802, REMOVED AND REPLACED DOUBLER. NR 6421O/B CARRIAGE SUPPORT THRUST BEARING RETAINER, BOTH UPPER BOLT HOLES AND LOWER I/B BOLT HOLE CORRODED AND NR 6423 I/B THRUST BEARING RETAINER, BOTH UPPER BOLT HOLES CORRODED. REPAIRED PER SRM 575004, REAMED AND INSTALLED BUSHINGS. ACCOMPLISHED REPAIRS DURING SHOP VISIT.

Part: ACT BRACKET — CRACKED (NR 5 LE FLAP)

DURING HMV, FOUND NR 5 L/E FLAP O/B ACTUATOR SUPPORT BRACKET CRACKED. REPAIRED PER M/M 57-20-21 PG 811.

Part: RIB — CRACKED (NR 3 LE FLAP)

RIBS CRACKED, NR 3 L/E SLAT. NINTH RIB FROM I/B END OF SLAT IS CRACKED IN RADIUS, TENTH RIB SAME CONDITION. REPAIRED PER MM 57-54-0 PG 817.

Part: SKIN — CRACKED (NR 2 MIDFLAP)

NR 2 MIDFLAP, AFT CORD ANGLE CRACKED 21, 36, AND 55 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 FIG 802 SPLICED IN NEW SECTIONS, NR 6272/6273/6274. ART CORD ANGLE CRACKED 41 FROM O/B END OF FLAP. REPAIRED PER M/M 575200 FIG 802 SPLICED IN NEW SECTION, NR 6275/6526/6537. COVE SKIN CRACKED 32 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 FIG 809. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER, NR 6277. REPAIRS ACCOMPLISHED DURING SHOP VISIT.

Part: RIB — CRACKED (NR 4 MIDFLAP)

NR 4 MIDFLAP, NR 6354 O/B THRUST BEARING BORE CORRODED. REPAIRED PER SRM 575004, MACHINED BORE AND INSTALLED BUSHING. NR 6320 O/B THRUST BEARING UPPER I/B RETAINER BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14, MACHINED AND INSTALLED BUSHING. NR 6331 L/E WORN FROM I/B END APPROX 12. REPAIRED PER SRM 575200 FIG 803, INSTALLED FILLER AND DOUBLER. NR 6332 I/B RIB LOWER AFT CORNER CRACKED. REPAIRED PER M/M 575200 TRIMMED DAMAGE AND INSTALLED DOUBLER. REPAIRS ACCOMPLISHED AT SHOP VISIT.

Part: FLAP ASSY — CORROSION (NR 2 MIDFLAP)

THRUST BEARING BORE RETAINER BOLT HOLES AT I/B END CORRODED, ON NR 2 MIDFLAP ASSEMBLY. REPAIRED PER SRM 57-50-4.

Part: BRACKET — CRACKED (NR 2 LE FLAP)

AT HMV, FOUND UPPER/LOWER CORNERS CRACKED FOR NR 2 LE FLAP ACT MOUNT BRACKET. INSTALLED DOUBLER PER M/M 57-20-21 PG 811.

Part: SKIN — WORN (NR 4 FOREFLAP)

DURING SHOP INSPECTION, NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO THE L/E SKIN AT 12 FROM THE 0/B END. REPAIRED PER SRM 57-50-4.

Part: NOSE COWL — CRACKED (NR 3 ENGINE)

UPON MAINT INSPECTION, A CRACK WAS FOUND IN OUTER SKIN OF NR 3 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3.

Part: RIVET — MISSING (RT ELEVATOR)

DURING HMV, FOUND RIVET MISSING ON LOWER SURFACE OF RT ELEVATOR INBD TRAILING EDGE CORNER. REPAIRED PER SRM 55-20-3 FIG 2.

Part: PANEL — WORN (NR 2 TE FLAP)

DURING SHOP INSPECTION, FOUND NR 2 AFT FLAP PANEL L/E HAD WEAR DAMAGE AT 40 INCHES FROM O/B END. REPAIRED PER SRM 57-53-4.

Part: BEAM — CRACKED (BS 1273)

THE BS 1273 FRAME BEAM AND I/B UPPER CHORD OF THE RT TORQUE BOX AT THE AIRSTAIR ACTUATOR FITTING WERE FOUND CRACKED. REPAIRED PER S/B 53-0129. DAMAGE FOUND AT LETTER CHECK.