N93875

Part: POWER SUPPLY — INOP (CABIN)

INSPECTION FOUND CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND OPERATION CHECKED GOOD IAW MM 33-53-00.

Part: ACTUATOR — INOP (LT MLG DOOR)

THE LT MLG SHOWED RED UNSAFE LIGHT WITH DOOR LIGHT OUT AFTER GEAR RETRACTION. THE GEAR WAS RECYCLED IAW CHECKLIST AND GEAR INDICATED NORMAL. THE LT GEAR ACTUATING CYLINDER WAS REMOVED AND REPLACED IAW MM 32-32-02. THE LT MLG DOOR ACTUATING CYLINDER AND DOOR LATCH MECHANISM WERE ADJUSTED IAW MM 32-32-04 AND MM 32-31-04, STEPS 6-20. THE DOOR LATCH WAS TESTED IAW MM 32-31-04 AND THE GEAR WAS SWUNG SEVERAL TIMES WITH NO FAULTS FOUND.

Part: SPAR CAP — CRACKED (LT TE FLAP)

INSPECTION FOUND A 3.5 INCH CRACK IN LT WING FLAP TRAILING EDGE CAP JUST O/B OF FLEX JOINT ASSEMBLY. REPAIRED IAW SRM 57-03, FIGURE 9 AND MM 51-00-00.

Part: PANEL — CRACKED (RT HORIZ STAB)

INSPECTION FOUND A 1.5 CRACK IN RT HORIZONTAL STABILIZER PANEL NR 3804 L/E. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 55-01, 51-30-2, 55-01, FIGURE 4, AND 55-12.

Part: TIE STRAP — CORRODED (BS 1136)

INSPECTION FOUND TIE STRAP CORRODED AT LEFT AFT SERVICE DOOR CUTOUT, FS 1136, LONGERON 27R. THE TIE STRAP WAS REMOVED AND A NEW TIE STRAP WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.

Part: SKIN — DENTED (LT LE SLAT)

INPECTION FOUND LEFT WING 0 SLAT DENTED. THE SLAT WAS REPAIRED IAW ECRA 5720-01120.

Part: DOUBLER — CRACKED (LT MLG DOOR)

INSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR LOWER LT CORNER DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.

Part: PAN — GOUGED (CARGO DOOR)

INSPECTION FOUND AFT CARGO DOOR GOUGED ON PAN AROUND DOOR STOPS. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, 51-10-4, 52-03, FIGURE 8 AND EA 5233-2-A0495.

Part: SUPPORT — BENT (BS 1007)

INSPECTION FOUND AFT PIT FORWARD BULKHEAD CENTER VERTICAL SUPPORT BENT AT FS 1007, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-10-4, 51-10-2, 51-30-2, 51-30-5, AND 51-10-3.

Part: SLAT — DENTED (RT LE SLAT)

INSPECTION FOUND RT WING 0 SLAT DENTED. REPAIRED SLAT IAW ECRA 5720-01170.

Part: PANEL — CRACKED (RT WING)

INSPECTION FOUND A 3 INCH CRACK IN RT WING TRAILING EDGE PANEL NR 1610. THE PANEL WAS REPAIRED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1338)

INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, RBL 54.5 AND RBL 35-45. THE CORRODED AREAS WERE CUT OUT AND REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3, 51-30-2, 51-30-5 AND ECRA 5310-03899.

Part: ANGLE — CRACKED (BS 875)

INSPECTION FOUND 3 CRACKS IN CENTER WING TO BODY FAIRING SUPPORT ANGLES(3) AT STA 875, BL 0. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-30-4, AND 51-30-5.

Part: LONGERON — CRACKED (BS 256)

INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-14-02, FIGURE 3, 53-02, FIGURE 18, 51-30-02, AND 51-30-05.

Part: FLOOR — CORRODED (BS 1138)

INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1138, LBL 42. INSTALLED NEW SKIN AND SUPPORTS IAW SRM 51-30-2, 51-30-3, AND 51-30-5.

Part: SUPPORT — CORRODED (BS 1330-1338)

INSPECTION FOUND AFT LT SERVICE DOOR LOWER CUTOUT FLOOR LEVEL SUPPORT CORRODED AT FS 1330-1338, LBL 14. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: ANGLE — CORRODED (BS 148-160)

INSPECTION FOUND L-ANGLE ABOVE LONGERON 18R AT STA 148-160 CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: DOUBLER — CORRODED (BS 484-503)

INSPECTION FOUND LOWER FUSELAGE EXTERNAL CUTOUT FOR NR 2 AD ANTENNA CORRODED BETWEEN SKIN AND INTERNAL DOUBLER AND MATING SURFACE AT FS 484-503, LONGERON 29L AND 30. THE INTERNAL DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — CRACKED (RT COCKPIT)

INSPECTION FOUND A 2 INCH CRACK IN RT COCKPIT SLIDING WINDOW CUTOUT UPPER AFT CORNER INSIDE DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1.

Part: SUBFLOOR — CORRODED (BS 200)

INSPECTION FOUND SUBFLOOR CORRODED AT STA 200, LBL 40 AND LBL 18 TO RBL 30. THE SUBFLOOR AREAS WERE REPAIRED IAW SRM 51-30-2, 53-05, FIGURE 25, 51-30-5, AND 53-01, FIGURE 4.

Part: SUPPORT — CORRODED (BS 1155)

INSPECTION FOUND LT FLOOR SUPPORT CORRODED AT FS 1155, JUST O/B OF I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.

Part: SKIN — CRACKED (RT SPOILER)

INSPECTION FOUND A 2.2 INCH CRACK IN RT I/B SPOILER FIXED SUPPORT PANEL. THE CRACKED AREA OF SKIN WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.

Part: FLOOR — CORRODED (BS 1183)

INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1183, LBL 42. REMOVED FORWARD AND AFT FRAME FITTINGS TORQUE BOX DOUBLER AND VERTICAL STIFFENER IAW SRM 51-30-1 AND 51-30-5. A REPAIR WEB WAS INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5. THE FITTINGS, FRAME AND STRAPS WERE INSTALLED IAW SRM 53-01-2.

Part: SKIN — DENTED (BS 140)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 140, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 22, VIEW I.

Part: SEAT TRACK — CORRODED (BS 1022-1243)

INSPECTION FOUND AFT RIGHT O/B SEAT TRACK CORRODED AT STA 1022-1041, RBL 54.5 AND STA 1092-1243, RBL 54.5. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-05, FIGURE 4.

Part: SEAT TRACK — CRACKED (BS 1309)

INSPECTION FOUND A 3 INCH CRACK IN LT CENTER SEAT TRACK AT FS 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-3, AND 53-05, FIGURE 4A.

Part: SUBFLOOR — CORRODED (BS 218)

INSPECTION FOUND SUBFLOOR CORRODED AT STA 218, LBL 42-44. THE SUBFLOOR WEB AND STIFFENERS WERE REMOVED AND A NEW WEB AND STIFFENERS WERE INSTALLED IAW SRM 53-10-4, 51-30-2, 51-30-4, AND 51-30-8.

Part: FLOOR — CORRODED (BS 148)

INSPECTION FOUND COCKPIT RT FLOOR SKIN CORRODED AT FS 148, RBL 6. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3 AND 51-30-2.

Part: SUPPORT — CORRODED (BS 157-200)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157-200, BL 0 AND STA 200, BL 0 TO RBL 40. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-30-5.

Part: SUPPORT — CORRODED (BS 157-180)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 157-180, RBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-10-3.

Part: TAB — DISBONDED (RUDDER)

INSPECTION FOUND RUDDER TRIM TAB METAL TAB DISBONDED ON RT SIDE OF TAB. THE RUDDER TAB WAS REMOVED AND THE METAL TAB WAS REMOVED AND REPLACED. THE RUDDER TAB WAS REINSTALLED AND RIGGED IAW MM 27-20-02.

Part: WEB — CRACKED (BS 195)

INSPECTION FOUND A 2 INCH CRACK IN SUBFLOOR CUSP WEB AT STA 195, RBL 9. THE SUBFLOOR CUSP WEB WAS REPAIRED IAW SRM 53-01, FIGURE 4, SHEET 3.

Part: FRAME — CORRODED (BS 1269)

INSPECTION FOUND FRAME LOWER LOBE AND WEB CORRODED AT FS 1269, LONGERON 28L-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 53-05, FIGURE 4A.

Part: PANEL — CORRODED (BS 864-870)

INSPECTION FOUND KEEL ACCESS PANEL BETWEEN BOTH MLG DOORS CORRODED ON ONE END AT FS 864-870. A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-00-60.

Part: PANEL — CRACKED (VERT STAB)

INSPECTION FOUND CRACKS IN VERTICAL STABILIZER PANEL NR 6404. THE CRACKS WERE 1-2 INCHES LONG. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1333)

INSPECTION FOUND FALSE BULKHEAD LOWER ATTACH ANGLE CORRODED AT FS 1333, LONGERON 28L-28R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-10-4 AND 53-01, FIGURE 2, SHEET 4.

Part: FITTING — CRACKED (NR 5 LE SLAT)

INSPECTION FOUND A .25 INCH CRACK IN RT WING NR 5 SLAT O/B FITTING. THE FITTING WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-30-2, 51-30-8, AND ECRA 5750-03276.

Part: SUPPORT — CORRODED (BS 200)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, BL 0 TO LBL 12 AND LBL 40. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 53-14-1, 51-10-3, 51-30-4, AND 51-30-5.

Part: WEB — PUNCTURED (BS 1050)

INSPECTION FOUND A SMALL HOLE PUNCTURED IN CUSP WEB AT FS 1050, RBL 59. THE PUNCTURED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND ECRA 5310-03907.

Part: SKIN — PUNCTURED (VERT STAB)

INSPECTION FOUND A HOLE THROUGH SKIN AND RIB OF VERTICAL STABILIZER AFT UPPER STRINGER TIP FAIRING. THE RIB AND SKIN WERE REPAIRED IAW SRM 55-01, FIGURES 2 & 4.

Part: POWER SUPPLY — INOP (EMER EXIT)

INSPECTION FOUND EMERGENCY OVERWING AFT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-22.

Part: FLOORBEAM — CORRODED (BS294 & 328)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, BL 0 TO RBL 50 AND STA 328, BL 0 TO RBL 50. NEW FLOORBEAM SECTIONS WERE INSTALLED IAW SRM 53-10-51.

Part: PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 2 CRACK IN FORWARD CARGO DOOR PAN ON LOWER SIDE OF DOOR NEAR NR 2 FRAME. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-4, 51-30-02, AND 51-30-7.

Part: ANGLE — CORRODED (BS 541)

INSPECTION FOUND LOWER ANGLES CORRODED AT BOTH SIDES OF FALSE BULKHEAD AT FS 541. THE SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-3, 51-01, FIGURE 1, SHEET 3, 53-20-0, AND 53-24-0.

Part: SEAT TRACK — CORRODED (BS 1112-1309)

INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1112-1309, LBL 54. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-10-3, AND 53-05, FIGURE 1A.

Part: SUPPORT — CORRODED (BS 218)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 218, LBL 6. A NEW SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — CREASED (NLG DOOR)

INSPECTION FOUND RT FORWARD NLG DOOR CREASED ON OUTER FORWARD UPPER CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 4 AND 51-10-3.

Part: SKIN — CRACKED (WS 257)

INSPECTION FOUND A 2.25 INCH CRACK IN LT WING LOWER LEADING EDGE SKIN AT STA XRS 257(NR 8 SLAT TRACK). A DOUBLER WAS INSTALLED IAW ECRA 5730-01667, SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1174)

INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1174, RBL 22. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 1 AND 51-10-3.

Part: SUPPORT — CORRODED (BS 168)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 168, BL 0 TO RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-5.

Part: SUPPORT — CRACKED (WS 189)

INSPECTION FOUND A 2 CRACK INCH LT WING REAR SPAR WEB LOWER SUPPORT JUST O/B OF FLAP I/B HINGE, XRS 189. THE ANGLE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2.

Part: SUPPORT — CORRODED (BS 1155)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155, LONGERON 28R-29R. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: TRACK — CORRODED (BS 1137-1155)

INSPECTION FOUND RT FORWARD CARGO FLOOR TRACK CORRODED AT STA 1137-1155, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-30-1, AND 51-30-2.

Part: SUPPORT — CRACKED (BS 446)

INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT AT FS 446, LONGERON 23L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.

Part: FITTING — CRACKED (BS 1338)

INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT FITTING AT STA 1338, RBL 54.5. THE FITTING WAS REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1332)

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1332, LBL 34 TO 42.5. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 20A.

Part: ANGLE — CORRODED (BS 160)

INSPECTION FOUND LOWER FLOOR SUPPORT ANGLE CORRODED AT STA 160, LBL 18-44. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-1.

Part: SKIN — CORRODED (BS 200)

INSPECTION FOUND FORWARD ENTRANCE DOOR CUTOUT CORRODED ON LOWER FORWARD CORNER AT FS 200, LONGERON 18L. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5310-03900 AND EA 9-5314-2-A0486.

Part: TRACK — CORRODED (BS 1170-1271)

INSPECTION FOUND LT AFT CARGO TRACK CORRODED AT SAT 1170-1271, LBL 24. A NEW CARGO TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 4C.

Part: SEAT TRACK — CORRODED (BS 1009-1079)

INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AROUND CLIP NUTS AT STA 1009-1079. THE SEAT TRACK WAS REPLACED IAW ECRA 5310-03904.

Part: SEAT TRACK — CORRODED (BS 478-1079)

INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 478-788, RBL 58 AND LT O/B SEAT TRACK CORRODED AT STA 1060-1079, LBL 58. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 53-05, FIGURES 4F AND 16, 51-30-5, AND 51-30-2.

Part: LONGERON — CRACKED (BS 160)

INSPECTION FOUND A 0.7 CRACK IN LONGERON 3L AT STA 160 AND A 0.6 CRACK IN LONGERON 4L AT STA 160. THE LONGERONS WERE REPLACED IAW SRM 53-02, FIGURE 18, 51-30-2 AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1338)

INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, LBL 54.5. THE CORRODED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4.

Part: SUPPORT — CORRODED (BS 1320)

INSPECTION FOUND RT AFT LAV FLOOR PAN CENTER SUPPORT CORRODED AT FS 1320, RBL 40. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1338)

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1338. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 200-237)

INSPECTION FOUND SEAT TRACKS CORRODED AT STA 200-237, RBL 22 AND STA 218-234, LBL 22. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-30-05, 53-24-0, AND 53-05, FIGURE 4F.

Part: SUPPORT — CORRODED (BS 157-200)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157, BL 0 - LBL 10 AND STA 157-200, LBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-14-1, 51-30-2, 51-30-5, 51-30-1, AND 51-30-3.

Part: FITTING — CORRODED (BS 1174)

INSPECTION FOUND FLOORBEAM LT END FITTING CORRODED AT STA 1174. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 AND 51-10-3.

Part: FLOOR — PUNCTURED (BS 148)

INSPECTION FOUND COCKPIT RT FLOOR SKIN PUNCTURED AT FS 148, RBL 14. THE PUNCTURED AREA WAS REMOVED AND TWO DOUBLERS WERE INSTALLED IAW SRM 53-10-1, FIGURE 12, SHEET 2.

Part: WEB — CRACKED (BS 636-655)

INSPECTION FOUND A 10 CRACK IN RT CUSP WEB BETWEEN STA 636 AND 655, RBL 44-54.5. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3.

Part: SKIN — CRACKED (PAX DOOR)

INSPECTION FOUND A .75 INCH CRACK IN FORWARD ENTRY DOOR INNER SKIN AT STA 207, LONGERON 15L. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5310-03891 AND EA 9-5314-2-A0482.

Part: SUPPORT — CORRODED (BS 1174)

INSPECTION FOUND FLOOR SPPORT CORRODED AT FS 1174, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.

Part: WEB — CRACKED (BS 1250)

INSPECTION FOUND A 4 CRACK IN LT CUSP WEB AT STA 1250, LBL 58. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.

Part: SUPPORT — CORRODED (BS 484)

INSPECTION FOUND CENTER FLOORBOARD SUPPORT AT STA 484, RBL 10 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-10-14.

Part: BRACKET — CORRODED (BS 1287-1307)

INSPECTION FOUND TWO FLOOR SUPPORT BRACKETS CORRODED AT FS 1287-1307, LBL 22. ONE BRACKET WAS CLEANED OF CORROSION AND THE OTHER BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2.

Part: POWER SUPPLY — INOP (CABIN)

INSPECTION FOUND MID CABIN AND SECOND SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE POWER SUPPLIES FOR EACH LOCATION WERE REMOVED AND REPLACED IAW MM 33-53-00.

Part: BATTERY — DISCHARGED (TAIL CONE)

TAIL CONE CEILING EMERGENCY LIGHTS FOUND INOP. REPLACED BATTERY PACK PER MM 33-53-00.

Part: BALLAST — INOPERATIVE (CABIN)

AN ELECTRICAL ODOR WAS REPORTED IN MAIN CABIN IN THE VICINITY OF ROW 15 WHILE AIRCRAFT WAS ON THE GROUND IN TPA. MAINTENANCE FOUND BALLAST FOR OVERHEAD LIGHTS AT ROW 15 AT FAULT. THE BALLAST WAS REPLACED AND OPERATION CHECKED GOOD.

Part: SHOCK STRUT — LOW PRESSURE (NLG)

THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE FOUND THE NOSE STRUT X-DIMENSION LOW. A FULL NOSE STRUT SERVICE WAS PERFORMED AND SET X-DIMENSION IAW MM 32-21-02, PAGE 301. THE NOSE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD.

Part: SENSOR — MALFUNCTIONED (NLG)

THE L/H MLG SHOWED UNSAFE AFTER GEAR WAS RETRACTED LEAVING EWR. THE GEAR WAS CYCLED, BUT THEN THE NOSE GEAR SHOWED UNSAFE. WHEN THE GEAR WAS EXTENDED FOR RETURN TO EWR ALL THREE GEAR SHOWED SAFE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AN EXTENSION/RETRACTION TEST WAS PERFORMED PER MM 32-30-00 AND ALL GEAR INDICATIONS CHECKED GOOD. THE FAILURE COULD NOT BE DUPLICATED. THE NOSE GEAR UP/DOWN LOCK PROXIMITY SENSOR AND CONNECTOR WERE REPLACED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT HAS FLOWN OVER FIVE FLIGHTS WITHOUT A REPEAT OF THIS PROBLEM.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION FOUND FUSELAGE SKIN CORRODED IN OPENING FOR NR 3 ADF CONNECTOR FITTING. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02556 AND SRM 53-04, FIGURE 12B.

Part: ANGLE — CRACKED (DORSAL FIN)

INSPECTION FOUND A .375 INCH CRACK IN LOWER DORSAL FIN INNER ATTACH ANGLE ON RT SIDE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 297)

INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 297. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38.

Part: STATOR SUPPT — BROKEN (NR 2 ENGINE)

THE NR 2 ENGINE SURGED WHILE AT CRUISE. THE ENGINE WAS BROUGHT BACK TO IDLE AND THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT ARRIVED WITHOUT FURTHER PROBLEM. THE NR 2 ENGINE WAS REMOVED AND REPLACED. AN ENGINE TRIM AND POWER RUN WAS PERFORMED AND ALL PARAMETERS CHECKED GOOD. *S/D* SHOP FINDINGS REVEALED THE 8TH STAGE STATOR SUPPORT HAD BROKEN.

Part: APU — MALFUNCTIONED (A/C TAIL)

SMOKE ENTERED THE COCKPIT AND CABIN AFTER TAKEOFF. THE LEFT PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE FLIGHT WAS CONTINUED TO FLL WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE VERIFIED THAT WHEN EITHER PACK WAS RUN WITH APU AIR SMOKE WAS CREATED. THE APU INLET AREA WAS INSPECTED AND OIL SEEPAGE FROM FIRST STAGE IMPELLER INLET AREA WAS NOTED. THE APU WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: STRUT — FLAT (NLG)

THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE LANDING GEAR HANDLE WOULD NOT RAISE AND AIRCRAFT REMAINED IN GROUND MODE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG STRUT AT FAULT. A FULL SERVICE OF THE NLG STRUT WAS PERFORMED. IN ADDITION, THE STRUT UPPER VALVE WAS REPLACED, A NLG SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD.

Part: HYD LINE — LEAKING (RT TAIL COMPT)

THE AIRCRAFT LOST FLUID FROM THE RT HYDRAULIC SYSTEM WHILE EN ROUTE TO EWR. THE RT SYSTEM WAS SECURED AT 7 QUART LEVEL. THE RT SYSTEM WAS TURNED ON FOR LANDING AND THE HYDRAULIC FLUID DROPPED TO A FINAL LEVEL OF THREE QUARTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT CASE DRAIN FILTER IN RT TAIL COMPARTMENT LEAKING. THE LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: STATOR VANE — FAILED (NR 1 ENGINE)

THE NR 1 ENGINE QUIT RUNNING AT FL 280 WHILE EN ROUTE FROM EWR TO MCO. THE ENGINE FAILURE WAS ACCOMPANIED BY A MUFFLED BANG. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO JAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED A FRACTURED C-8 STATOR VANE.

Part: STRUT — REQ'D SERVICE (NLG)

FLT NR 1862 - DEN - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND WAS ACCOMPANIED BY NOSE GEAR VIBRATION. THE GEAR WAS EXTENDED FOR RETURN TO DEN AND THERE WAS A LOUD THUMP WHEN NOSE GEAR LOCKED DOWN. A TOWER FLY-BY WAS CONDUCTED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPACKED AND SERVICED THE NLG IAW MM 32-21-02. THE UPPER AND LOWER BEARINGS AND INNER AND OUTER CYLINDERS WERE INSPECTED WITH NO ABNORMALITIES FOUND. A GEAR SWING WAS PERFORMED AND OPERATION AND INDICATIONS WERE GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT NR 0743 - IAH - PRIOR TO DEPARTURE, AISLE LIGHTING COMES ON WHEN SWT IN ARM POSITION. REMOVED BATTERY PACK AND REPLACED, OPS CHECKS NORMAL. (M)

Part: SUPPORT SHELF — BROKEN (NR 1 ENGINE)

FLT NR 477 - RDU - THE NR 1 ENGINE COMPRESSOR BEGAN TO STALL AT FL 310 WHILE EN ROUTE FROM EWR TO TPA. THE STALL WAS ACCOMPANIED BY A LOUD BANGING IN REAR OF AIRCRAFT. THE NR 1 ENGINE WAS BROUGHT TO IDLE AND THE STALLING CEASED. THE AIRCRAFT WAS DIVERTED TO RDU WHERE IT LANDED WITHOUT INCIDENT. A BOROSCOPE OF THE NR 1 ENGINE FOUND THE 6TH AND 7TH STAGE COMPRESSOR DAMAGED. THE NR 1 ENGINE WAS REMOVED AND REPLACED. A POWER ASSURANCE/TRIM RUN WAS PERFORMED IAW MM 71-00-00 AND ALL PARAMETERS WERE NORMAL. INVESTIGATION REVEALED AN 8TH STAGE STATOR SUPPORT SHELF HAD BROKEN OUT AND WAS THE PRIMARY CAUSE OF ENGINE FAILURE. (M)

Part: CLIPS — OUT OF ADJUST (TAILCONE)

HOU - THE INTERIOR TAILCONE RELEASE REQUIRED EXCESSIVE FORCE TO PULL FROM CLIPS. THE RELEASE HANDLE CLIPS WERE ADJUSTED TO WITHIN SPECIFICATION PER MM 53-53-00. (M)

Part: EEL POWER SUPPLY — FAILED (CABIN)

FLT NR 0302 - DCA - OVERHEAD EMERGENCY LIGHTS ROW 28 AND 29 INOP. REPLACED POWER SUPPLY. OPERATION OF OVERHEAD LIGHTING RESTORED. (M)

Part: VALVE — FAILED (RT PACK)

FLT NR 5392 - BOS - SMOKE APPEARED IN THE CABIN ON APPROACH TO BOS WITH THE ENGINE AND AIRFOIL ANTI-ICE ON. THE SAME PROBLEM HAD OCCURRED ON THE PREVIOUS FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED DIAPHRAGM IN THE RT WATER SEPARATOR TEMPERATURE CONTROL VALVE. THE CONTROL VALVE WAS REMOVED AND REPLACED. IN ADDITION, THE RT ACM WAS REPLACED AS A PRECAUTIONARY MEASURE, AND THE RT COALESCER BAG WAS REPLACED. A FUNCTIONAL CHECK WAS PERFORMED AND NO LEAKAGE WAS PRESENT IN THE RT PACK SYSTEM. BURNOUT PROCEDURES WERE COMPLETED IAW MM 21-20-02, PAGE 209, PARAGRPAH C AND NO FURTHER SMOKE OR ODORS WERE PRESENT. (Z)

Part: SENSOR — SHORTED (LT WW)

FLT NR 0683 - IAH - WHEN WING ANTI-ICE SYSTEM WAS TURNED ON THE PRESSURE ABNORMAL LIGHT ILLUMINATED STEADILY AND THE PROTECTION TEMP LOW LIGHTS REMAINED ON. THE AIR CONDITIONING AIR BEGAN TO SMELL HOT AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED SAFELY AT IAH. MAINTENANCE FOUND THE 180 DEGREE DUCT BLOWN SENSOR SHORTED IN THE LEFT WHEEL WELL. THE SENSOR WAS REPLACED AND OPERATION CHECKED GOOD WITH NO SMOKE DETECTED. (Z)