N294WA

Part: ACCESSORY UNIT — FAILED (E/E BAY) · airframe 63,872 hrs · 43,289 cycles

AFTER T/O AND GEAR RETRACTION WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION IT DID NOT CATCH IN THE DETENT. GEAR DISAGREE LIGHT AND DOORS LIGHT ILLUMINATED. GEAR WAS THEN CYCLED WITH A/C SPEED AT 230 KNOTS CAUSING OVERSPEED CONDITION ON GEAR. GEAR WAS RETRACTED AND ALL RETURNED TO NORMAL. REPLACED LANDING GEAR ACCESSORY MODULE. SWUNG LANDING GEAR, CHECKS OUT OK.

Part: SPAR — CRACKED (ELEVATOR) · airframe 63,684 hrs · 43,170 cycles

INSPECTION OF THE LT ELEVATOR REAR SPAR PER BAC S/B 727-55-0089 AND AD 96-06-05 REVEALED A TYPICAL CRACK EMANATING FROM A TAB HINGE SHEAR PLATE. THE CRACK WAS WITHIN LIMITS OF THE S/B AND WAS STOP DRILLED ON A TEMPORARY BASIS UNTIL THE SPAR MOD IS ACCOMPLISHED PER THE S/B. THE WORK WAS ACCOMPLISHED PER ER/A 382010-14AD.

Part: ELEVATOR — CRACKED (TAIL) · airframe 63,677 hrs · 43,167 cycles

1/4" CRACK AT RIVET UPPER SKIN OF R/H ELEVATOR APPROX. 14" FWD OF TAB CENTER HINGE. REPAIRED PER DRD 55-20-3D,AND RESTENCILED ELEVATOR

Part: FILTER HOUSING — CRACKED (HYD SYSTEM) · airframe 62,810 hrs · 42,584 cycles

LOST A-SYS HYDRAULICS ON LANDING GEAR RETRACTION PRESSURE AND QTY DECREASED TO ZERO. FOUND A-SYS FILTER MODULE CRACKED AT CHECK VALVE REPLACED SAME.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,284 hrs · 42,222 cycles

F/C SEAT ROWS EMER LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK. OPS CKS NML

Part: ANGLE — CRACKED (NR 8 SLAT) · airframe 62,219 hrs · 42,176 cycles

COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT NBR 8 SLAT. REPAIR PER MM 57-54-000-8

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,219 hrs · 42,176 cycles

THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 26 AND WL 169. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 380315-14.

Part: WINDOW — CRACKED (COCKPIT) · airframe 62,018 hrs · 42,039 cycles

UPON LANDING, NOTICED R-1 WINDOW CRACKED. REPLACED R-1 WINDOW AND WINDOW HEAT CONTROLLER.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 61,277 hrs · 41,529 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES.

Part: B-NUT — LOOSE (NR 1 PYLON) · airframe 61,005 hrs · 41,346 cycles

A-SYS HYD FAILURE. QTY WENT TO -0-, BOTH LOW PRESS LIGHTS ILLUM ON SHORT FINAL. FOUND B-NUT AT LOWER NR 1 PYLON LOOSE. TIGHTENED SAME. INSPECTED CASE DRAIN FILTERS AND SERVICED.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 61,005 hrs · 41,346 cycles

O2 MASK HEAD PIECE MISSING RUBBER STRIP. REPLACED MASK, OPS CHECK OK.

Part: ANGLE — CRACKED (TE FLAP) · airframe 60,475 hrs · 40,975 cycles

DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 32.5 INCH FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER 727 M/M 57-52-0 BY INSTALLING A NEW SECTION OF ANGLE AND A DOUBLER PER THE ABOVE M/M.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,436 hrs · 40,949 cycles

A CRACK WAS FOUND IN THE LBL 36.83 VERTICAL STIFFENER ON THE FORWARD SIDE OF THE 1183 BULKHEAD. THE CRACK WAS LOCATED BETWEEN WL 230 AND WL 254. THE DAMAGE WAS REPAIRED PER S/B 727-53-0192 AT MV2.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 60,436 hrs · 40,949 cycles

AT MV THE RT ELEVATOR UPPER SURFACE HAS A DENT WITH CRACK JUST O/B OF ELEV STA 136.5 6 IN FWD OF T/E. THE ELEVATOR WAS REPLACED PER NR 852. S/N OFF DL90136RH, S/N ON DL90091RH.

Part: ATTACH FITTING — CORRODED (NR 3 FLAP TRACK) · airframe 60,436 hrs · 40,949 cycles

AT MV THE NR 3 FLAP TRACK FWD ATTACH LUG WAS FOUND TO BE CORRODED. CORROSION WAS REMOVED PER MM 57-52-0. EDDY CURRENT INSP, NO INDICATIONS. AREA PEENED AND CAD PLATED PER MM 57-52-0. REPAIR COMPLETED PER MM 57-52-0.

Part: SKIN — DAMAGED (TE FLAP) · airframe 60,436 hrs · 40,949 cycles

DURING MV2 VISIT THE NR 4 MIDFLAP LEADING EDGE WAS FOUND WORN AT THE IB END. THE LEADING EDGE WAS REPAIRED BY TRIMMING OUT THE WORN AREA AND INSTALLING A DOUBLER AND FILLER PER 727 MM 57-52-0,FIG. 803. THIS REPAIR WAS ACCOMPLISHED IN THE SHOP PER SO B09707.

Part: TRANSCEIVER — INOPERATIVE (E/E BAY) · airframe 59,678 hrs · 40,456 cycles

NR 2 NAV INOP, SPECIFICALLY NR 2 VOR, LOC AND GS INOP. AND OFF FLAG IN VIEW. DME WORKS NORMALLY. NAV TUNED TO MULTIPLE FREQUENCIES AT VARIOUS DISTANCE BUT EQUIP STILL UNRELIABLE. REPLACED XCVR ATTENUATE TO-60 ON VOR -50 ON ILS, OPS CK NORMAL.

Part: CONNECTOR — DIRTY (SMOKE DETECTOR)

LAV SMOKE CAUTION LIGHT ILLUMINATED ON S/O PANEL AND CHIMES IN PAX CABIN. NO FIRE WAS LOCATED AND SYSTEM WAS DEACTIVATED BY PULLING CIRCUIT BREAKER. FOUND LEFT AFT LAV SMOKE DETECTOR WOULD NOT TEST AFTER RESETTING C/B. CLEANED CONNECTIONS AT CANNON PLUG AND SWITCH, OPS CKS GOOD. INSPECTED PLACARDS, EXTINGUISHERS, NO INDICATION OF EXCESS HEAT OR FIRE.

Part: SKIN — CRACKED (NR 6 LE SLAT)

A 1.125 INCH VISABLE CRACK ON AFT SKIN OF NR 6 SLAT AT O/B TRAILING EDGE. SPLICED SKIN PER M/M 57-54-0, NR 1.

Part: WEB — DAMAGED (WING REAR SPAR)

WHILE ACCOMPLISHING THE CENTER WING REAR SPAR WEB MOD PER BAC S/B 57A0182, SEVERAL FASTENER HOLE LOCATIONS WERE DAMAGED. THE MODIFICATION DOUBLERS AND FILLERS WERE EXTENDED TO REPAIR THE EXTRA DAMAGE PER ER/A 366706-14AD.

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

NR 1 LE FLAP ACT SUPPORT BOX CRACKED AT UPPER IB CORNER. REPAIRED PER MM 57-21-21.

Part: HEAT VALVE — FAILED (NR 3 ENGINE)

NR 3 ENGINE OIL TEMPERATURE ROSE TO YELLOW BAND RANGE. FOLLOWED POM PROCEDURES FOR HIGH OIL TEMPERATURE. SHUTDOWN NR 3 ENGINE ACCORDING TO CHECKLIST PROCEDURES. REPLACED NR 3 ENGINE FUEL HEAT VALVE. LEAK AND FUNCTION CHECKS OK. INSPECTED ENGINE FOR OIL TEMP CONDITION AND WINDMILL CONDITION. ALL OPERATIONS CHECKS OK PER MAINTENANCE MANUAL.

Part: LIGHT — INOPERATIVE (CABIN)

AFT LT O/W EMERG LIGHT INOP. REPLACED M955 RACK, OPS CKS GOOD.

Part: SKIN — CORRODED (BS 1060)

THE SKIN WAS FOUND CORRODED AT STRINGER 28R BETWEEN FS 1050 AND 1070. THE DAMAGE WAS CUTOUT OVER A 3 X 16 AREA. THE SKIN WAS REPAIRED WITH A DOUBLER PER THE GUIDLINES OF B727 SRM 53-30-3 AND DOCUMENTED PER ER/A 364236-14.

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

FOUND .125 INCH VISIBLE CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BOX I/B LOWER CORNER MARKED. REPAIRED PER MM 57020-21 P 811.

Part: WEB — CRACKED (BS 1303)

FOUND DURING B-2 LETTER CHECK, VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 CRACKS AT LT SIDE. ONE CRACK AT LWR CORNER AND ONE APPROX 6.5 INCHES ABOVE LWR CORNER. REPAIRED PER M/M 53-11-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT CROSS AISLE EMERGENCY EXIT LIGHTS FLASH WHEN TESTED. REPLACED BATTERY PACK, LIGHTS CK OK.

Part: CHANNEL — CRACKED (BS 1263)

DURING INSPECTION, FOUND CHANNEL AT FS 1263 TORQUE BOX CRACKED. CRACK LENGTH WAS APPROXIMATELY 1.5 INCH. REPLACED CHANNEL PER AD 94-07-08 AND B727 S/B 53-0129, R 4.

Part: ANGLE — CRACKED (NR 6 SLAT)

NR 6 SLAT LOWER COVE SKIN ANGLE CRACKED 1.5 INCH INBD OF ACTUATOR. REPAIRED PER M/M 57-54-0.

Part: WEB — CRACKED (BS 1223)

FOUND DURING A-1 LETTER CHECK, .125 INCH CRACK IN LWR TORQUE BOX VERT WEB LIGHTENING HOLE FS 1223 LEFT SIDE. REPAIRED PER M/M 53-11-0 PAR 15.

Part: ACTUATOR BRACKET — CRACKED (NR 2 LE FLAP)

FOUND ON A-1 LETTER CK, NR 2 LE FLAP O/B ACTUATOR BRACKET CRACKED. REPAIRED PER MM 57-20-21.

Part: DOUBLER — CRACKED (NR 7 LE FLAP)

PREVIOUS DOUBLER REPAIR CRACKED BENEATH NR 7 L/E SLAT I/B DOWN STOP PAD. CRACK WAS FOUND AT F-1 LTR CHECK. REPLACED DOUBLER PER MM 57-54-0.

Part: ELEMENT — SHORTED (LWR AFT BODY)

ON TAKEOFF OUT OF ORF, HAD THE LOWER/AFT BODY OVERHEAT ILLUM. FOLLOWED PROCEDURES, LIGHT STAYED ILLUM. ISOLATED THE NR 1, NR 2, NR 3 ENG PNEUMATICS, LIGHT REMAINED ILLUM. OFF-LANDED IN CAE. FOUND RT OVERHEAT DET M365 SEC 48 SHORTED. REPLACED SAME, RAN ENGINES, OPERATION NORMAL.

Part: SKIN — CORRODED (FS 720)

CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT ALONG THE AFT EDGE. REPAIRS WERE ACCOMPLISHED PER ERA 301584-14.

Part: SEAT TRACK — CORRODED (FS 1030-1136)

AT HMV, RT INBD SEAT TRACK CORRODED STA 1030 TO 1136, RT OUTBD TRACK CORRODED AT FS 1090 TO 1136 AND RT GALLEY TRACK CORRODED FS 1070 TO 1136. REPLACED SECTIONS OF TRACK PER SRM 53-10-5.

Part: FRAME — CRACKED (L2 DOOR)

THE L2 DOOR FRAME (ON DOOR) IS CRACKED AT UPPER HINGE, LWR O/B CORNER. REPAIRED PER SRM 52-40-2 PG13-15.

Part: SKIN — DAMAGED (RT ELEV)

DURING SHOP INSP, AN ELONGATED HOLE WAS DISCOVERED IN THE 4TH ACCESS PANEL FROM O/B. REPAIRED PER SRM 55-10-3. DURING SHOP INSP, AN UNIDENTIFIED REPAIR WAS DISCOVERED ON THE LWR SKIN 12 INCHES FROM I/B END. REPAIRED PER SRM 55-20-3 FOR RIGHT ELEVATOR ASSEMBLY.

Part: SKIN — DENTED (RT ELEV)

FOUND DURING SHOP INSP, RT ELEV UPPER I/B SURFACE DENTED. REPAIRED SKIN PER SRM 55-20-3.

Part: SEAT TRACK — CORRODED (FS 344-380)

DURING HMV, FOUND RT INBD SEAT TRACK CORRODED STA 344-380. REPLACED PER SRM 53-10-5 FIG 8.

Part: SEAT TRACK — CORRODED (FS 350)

DURING HMV, FOUND LT INBD SEAT TRACK CORRODED STA 350. REPAIRED PER SRM 53-10-5.

Part: FRAME — CRACKED (FS 1030)

AT HMV, FOUND FUSELAGE FRAME FS 1030 ABOVE STRINGER 25L CRACKED. CUT OUT DAMAGE SECTION AND REPAIRED PER DL ERA 301494-14.

Part: PANEL — DISBONDED (NR 12 SPOILER)

DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 12 SPOILER PANEL REPAIRED PER SRM 57-50-6.

Part: PANEL — DISBONDED (NR 11 SPOILER)

DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 11 SPOILER PANEL REPAIRED PER SRM 57-50-6.

Part: STRINGER — CRACKED (FS 720)

AT HMV, STRINGER 15R FOUND CRACKED AT AFT SIDE OF RT WING LEADING EDGE ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3.

Part: SKIN — CRACKED (NR 5 SLAT)

AT HMV, FOUND RT WING NR 5 L/E SLAT WITH CRACKS IN THE SKIN AT WING FENCE ATTACH HOLE. REPAIRED PER MM 57-54-0 PG 817.

Part: RIB — CRACKED (NR 2 LE SLAT)

RIB CRACKED NR 2 L/E SLAT NR 3 RIB CRACKED (MARKED). STOP DRILLED CRACK AS PER SRM 57-50-3. FABRICATED DOUBLER AS PER SRM 57-50-3 FIG 9 SHEET 1 AND 2.

Part: STRINGER — CRACKED (FS 720)

AT HMV, STRINGER 15R FOUND CRACKED AT FWD SIDE OF RT WING L/E ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3.

Part: SKIN — CRACKED (NR 4 LE SLAT)

SKIN CRACKED, NR 4 SLAT HAS 6 CRACKS AT FENCE ATTACH POINTS. REPAIRED PER MM 57-54-0 PG 817. FOUND AT HMV.

Part: RIB — CRACKED (NR 2 LE SLAT)

RIB CRACKED NR 2 L/E SLAT NR 4 RIB CRACKED (MARKED). STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 57-50-3 FIG 9.

Part: RIB — CRACKED (NR 2 LE SLAT)

RIB CRACKED NR 2 L/E SLAT NR 5 RIB FROM INBD END CRACKED FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9. FOUND AT HMV.

Part: FITTING — CORROSION (LT WING)

LMG SUPPORT BEAM OB FITTING AT REAR SPAR HAS CORROSION IN BORE OF FWD SUPPORT FITTING. REPAIRED PER SRM 57-40-00 FIG 1. FOUND AT HMV.

Part: INTERCOSTAL — CRACKED (FS 348-60)

INTERCOSTAL AT STA 348 TO 360 STR 16L IS CRACKED. REPAIRED PER SRM 53-10-4 FIG 28. FOUND AT HMV.

Part: ATTACH FITTING — ELONGATED HOLES (LT MLG)

DURING HMV, FOUND HOLES ELONGATED LMLG SUPPORT BEAM ATTACH FITTING. REPAIRED PER SRM 57-40 PG. 3.

Part: SKIN — CORRODED (FS 1050)

AT HMV, FOUND FUSELAGE SKIN WITH CORROSION DAMAGE AT FS 1050 AT STRINGER 28L. REPAIRED PER SRM 53-30-3 FIG 3.

Part: FLOOR BEAM — CORRODED (FS 400)

FLOOR BEAM CORRODED AT FS 400 FROM LBL 20 TO RBL 36. REPAIRED PER SRM 53-10-8 FIG 3.

Part: BLKHD SUPPORT — WORN (FS 720)

DURING HMV, FOUND SUPPORT WORN LT BULKHEAD, FS 720D. REPAIRED PER SRM 53-10-9 FIG 8.

Part: SUPPORT — WORN (FS 720)

AT HMV, FOUND SUPPORT WORN RT BULKHEAD. FS 720D RBL 24. REPAIRED PER SRM 53-10-9 FIG 8.

Part: FLOORBEAM — CORRODED (FS 344)

FLOORBEAM CORRODED STA 344 RBL 22 TO LBL 54 AT FASTENER HOLES. REPAIRED PER SRM 53-10-8 FIG 8. FOUND AT HMV.

Part: FLOORBEAM — CORRODED (FS 380)

FLOORBEAM CORRODED STA 380 RBL 12 TO 44, FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 1.

Part: RIB — CRACKED (NR 5 LE SLAT)

NR 5 SLAT RIB CRACKED, OB RIB OF OB TRACK ATTACH POINT IS CRACKED AT SCREW HOLE 2 INCHES UP FROM LOWER SKIN. REPAIRED PER SRM 57-50-3 FIG 9.

Part: RIB — CRACKED (NR 3 LE SLAT)

NR 3 SLAT RIB CRACKED IB RIB AT ACT ATTACH POINT IS CRACKED AFT LOWER CORNER. REPAIRED PER MM 57-54-00 PG 806-807.

Part: ANGLE — CRACKED (NR 8 LE SLAT)

NR 8 SLAT ANGLE CRACKED, ANGLE IS CRACKED UNDER IB UPSTOP FITTING NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812. FOUND AT HMV, INSPECTION.

Part: RIB — CRACKED (NR 5 LE SLAT)

RIB CRACKED NR 5 SLAT, FWD TOP CORNER OF RIB MARKED 119IB RIB AT ACT IS CRACKED. REPAIRED PER MM 57-54-0 PG 815 TO 815A. FOUND AT HMV.

Part: WEB — CRACKED (BS 1303)

WEB CRACKED, TWO 1 INCH CRACKS IN STA 1303 UPPER WEB ABOVE AND TO RT SIDE OF 'S' DUCT (MARKED). FABRICATED REPAIR PLATE PER SRM 51-40-2 FIG 1.

Part: STRINGER — CORRODED (FS 990)

AT HMV, FOUND FUSELAGE FRAME AND STRINGER CORRODED AT FS 990 AT STRINGER 29L. REPAIRED FRAME PER MM 53-11-0 PG 825.

Part: SKIN — CRACKED (BS 1100)

FUSELAGE SKIN CRACKED 1 INCH BOTH SIDES OF C/L AT STA 1100. CUT OUT DAMAGE PER SRM 53-30-3. INSP OF DAMAGED AREA STA 1100 LT AND RT SHOWED CRACKS REMOVED. INSTALLED REPAIR PER SRM 53-30-3. FOUND AT HMV.

Part: FRAME — CORRODED (FS 1010)

CORROSION ON BOTTOM LEG OF FORMER AT STA 1010 BETWEEN S30 AND S29R. REPAIRED PER SRM 53-10-4 FIG 4. FOUND AT HMV.

Part: STRINGER — CORRODED (FS 1050)

STA 1050 STR 28L HEAVY CORROSION BETWEEN SKIN AND STR BELOW FRAME AND INSIDE STRINGER. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV.

Part: STRINGER — CORROSION (FS 720)

DURING HMV, FOUND CORROSION IN S27R AT STA 720F. REPAIRED PER SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (FS 706)

AT HMV, FOUND STRINGER 26R CORRODED AT STA 706. REPAIRED PER SRM 53-10-3.

Part: ELEVATOR — DAMAGED (RT ELEV)

AT HMV, FOUND RT ELEVATOR LOWER SKIN WITH DAMAGED SKIN AT FASTENER HOLE AT FOURTH ACCESS PANEL FROM O/B END. ELEVATOR WAS SENT TO SHOP FOR REPAIRS.

Part: SUPPORT BEAM — CORRODED (FS 848-870)

BEAM CORRODED. STA 848-870 RBL-10 SUPPORT BEAM CORRODED AT PNL 3455R HINGE LOCATIONS, LOWER FUSELAGE ACCESS PANELS. FOUND AT HMV.

Part: STRINGER — CORRODED (FS 700)

AT HMV, FOUND STRINGER 28L WITH CORROSION DAMAGE AT FS 700. REMOVED SECTION OF STRINGER FROM STA 680 TO 720 AND INTERCOSTAL FROM 700 TO 720. FABRICATED REPAIR AS PER SRM 53-10-3. INSTALLED STRINGER, REPAIR, AND INTERCOSTAL.

Part: STRINGER — CORRODED (FS 700)

AT HMV, STRINGER 27L WAS FOUND CORRODED JUST AFT OF FS 700. REMOVED CORROSION PER SRM 51-10-6. REMOVED SECTION OF STRINGER AND REPAIRED PER SRM 53-10-2.

Part: STRINGER — CORRODED (FS 640)

AT HMV, FOUND STRINGER 26R CORRODED AFT OF FS 640. INSTALLED REPAIR AS PER ERA 301574-14.

Part: BLKHD ANGLE — CORRODED (FS 740)

STA 740 SKIN TO BULKHEAD CLOSEOUT ANGLE CORRODED BETWEEN STR 28R AND 27R. DAMAGE FOUND AND REPAIRED AT HMV. REPAIRED PER SRM 53-11-0 FIG 826, TREATED AND PAINTED.

Part: STRINGER — CORRODED (FS 740)

DURING HMV, FOUND STRINGER 27R CORRODED AT END, FWD OF STA 740. REPAIRED PER SRM 53-10-3 FIG 1.

Part: FITTING — HOLE CORRODED (NR 3 TE MIDFLAP)

I/B CARRIAGE SUPPORT FITTING WAS FOUND TO HAVE LOWER O/B RETAINER BOLT HOLE CORRODED, IN NR 3 MIDFLAP. FOUND AT SHOP INSP, THE HOLE WAS REAMED AND BUSHED PER SRM 57504.

Part: STRINGER — CRACKED (FS 720)

AT HMV, STRINGER 15L WAS FOUND CRACKED AT ITS END AT FS 72OC LEFT WING ICE LIGHT HOUSING. REPAIRED PER SRM 53-10-3 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE)

REMOVED FASTENERS AND STOP DRILLED CRACK IN STRINGER 15L. INSTALLED REPAIR PER SRM 53-10-3 NR 2.

Part: BOW — FRETTED (FAIRING NR 9705)

AT HMV, FOUND BOW FRETTED ON BOTH SIDES AT FWD END OF FAIRING NR 9705. REPAIRED PER SRM 51-40-3.

Part: FLOORBEAM — CORRODED (FS 700)

STA 700 FRAME CORRODED ON TOP IB OF RT FIXED FLOOR AND STA 700 FRAME CRACKED/BENT ON TOP IB OF LT FIXED FLOOR AT Z ANGLE ATTACH. REPAIRED PER SRM 53-10-1 PG 1.

Part: FRAME — CRACKED (BS 913.5)

DURING HMV, THE LT MLG UPLOCK ASSEMBLY ATTACH FRAME IN LT WHEEL WELL FS 913.5 HAD TIME LIMITED REPAIR. REPLACED WITH PERMANENT REPAIR PER MM 53-11-0 PG 814.

Part: COWL FRAME — WORN (NR 2 ENG)

AT HMV, FS 1353 FRAME AT RBL 11 WAS FOUND WORN BEYOND LIMITS FROM WEAR BY NR 2 ENGINE AFT COWL PANELS. REPAIRED PER MM 53-11-0 PG 801.

Part: STRINGER — CORRODED (FS 490-500)

AT HMV, FOUND STRINGER 28L CORRODED AT FS 490 TO 500. REPAIRED PER SRM 53-10-3 FIG 1.

Part: STRINGER — CORRODED (FS 700)

AT HMV, FOUND STRINGER 28R WITH CORROSION DAMAGE AT FS 700. FABRICATED STRINGER SPLICE REPAIR PER SRM. INSTALLED REPAIR PER SRM 53-10-3 FIG 1.

Part: FITTING — CORRODED (NR 4 TE FLAP)

NR 4 MID FLAP, O/B CARRIAGE SUPPORT FITTING UPPER I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. ALSO, I/B SUPPORT FITTING HAS LOWER I/B THRUST BEARING BOLT HOLE CORRODED. REPAIRED PER SRM 57-50-04 PG33. REAMED OVERSIZE AND INSTALLED BUSHINGS. FOUND AND REPAIRED DURING HMV SHOP INSPECTION.

Part: SKIN — CRACKED (NR 3 AFT FLAP)

LOWER L/E SKIN HAS CRACK APPROX 61 INCHES FROM I/B END. THIS WAS REPAIRED PER SRM 57-50-4 FIG 9, FOR NR 3 AFT FLAP AT HVM SHOP INSPECTION.

Part: FITTING — PITTED (RT TE FLAP)

NR 4 MID FLAP, O/B THRUST BEARING BORE PITTED. REPAIRED PER SRM 57-50-04 PG 37. OVERSIZED BORE AND INSTALLED BUSHING. FOUND AND REPAIRED AT HMV, SHOP INSPECTION.

Part: RIB — CRACKED (NR 4 MID FLAP)

NR 4 MID FLAP, I/B AFT CLOSE-OUT RIB CRACKED. REPAIRED PER M/M 57520 FIG 808, MFG'D AND INSTALLED DOUBLER. FOUND AND REPAIRED DURING SHOP INSPECTION.

Part: SKIN — CRACKED (NR 2 TE FLAP)

ON INITIAL SHOP INSPECTION, MAINTENANCE FOUND A CRACK ON LEADING EDGE SKIN AT CLEARENCE CUTOUT APPROX 47 INCHES FROM OUTBOARD END. REPAIRED DAMAGED AREA PER SRM 57-50-4 FOR L/WING NR 2 FOREFLAP.

Part: SKIN — CRACKED (NR 6 LE FLAP)

DURING SHOP INSPECTION RIGHT WING NR 6 SLAT WAS FOUND WITH A CRACK IN THE LOWER SKIN AT 19 INCH FROM THE INBOARD END OF SLAT AND 13 INCH FROM THE OUTBOARD END OF SLAT. REPAIRED PER SRM 57-54-0.