N14840

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,738 hrs · 23,126 cycles

INSPECTION FOUND A 1/2 INCH CRACK IN CANTED FRAME CAP AT STA 1446, L3R. REMOVED AND REPLACED CAP IAW SRM 51-30-2.

Part: LONGERON — CRACKED (STA 1410) · airframe 47,738 hrs · 23,126 cycles

INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT STA 1410. A REPAIR SECTION AND SPLICE WERE INSTALLED IAW ECRA 5311-01132.

Part: TORQUE LINK — CRACKED (NLG) · airframe 45,685 hrs · 22,070 cycles

INSPECTION FOUND A 1.5" CRACK IN NLG UPPER TORQUE LINK. THE UPPER TORQUE LINK WAS REMOVED AND REPLACED IAW MM 32-21-04.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 43,820 hrs · 21,094 cycles

THE FORWARD ENTRY PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EMERGENCY LIGHT WAS REMOVED AND REPLACED IAW MM 33-53-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT FS 200 - 243. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-10-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FUSELAGE SKIN CREASED AT FS 133, LONGERON 18L. A DOUBLER AND SKIN FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-34, FIGURE 1.

Part: DOUBLER — CORRODED (ANTENNA) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND NR 1 RAD ALT ANTENNA DOUBLER CORRODED. THE ANTENNA DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 1 ENGINE PYLON O/B TRAILING EDGE BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 788 - 1258. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3, AND 53-05, FIGURE 4F.

Part: SUPPORT BRACKET — CRACKED (TAIL BAY) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 2 INCH CRACK IN AFT END OF TAIL COMPARTMENT LT SIDE WALL SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 51-10-1.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FORWARD CARGO DOOR JAMB CORRODED AROUND RIVET NUTS. THE DOOR JAMB WAS REMOVED AND A NEW DOOR JAMB WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4.

Part: SKIN — DENTED (SLAT) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT WING 0 SLAT DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-06, FIGURE 1. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-7.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND AFT CARGO DOOR OUTER SKIN CHAFED AT BOTTOM FORWARD CORNER. THE DOUBLER WAS REMOVED IAW SRM 51-30-2 AND 51-10-4. A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED ON O/B EDGE AT STA 389 - 427, LONGERON 18R. THE CORRODED SECTION OF WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 53-01, FIGURE 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 280 BETWEEN LONGERON 23L AND 24L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 6 INCH CRACK IN EXTERNAL FUSELAGE LOWER FILLET FAIRING T-FITTING AT FS 880. THE T-FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: RIB — CRACKED (FAIRING) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT MOST LEFT RIB AT FASTENER HOLE OF VERTICAL STABILIZER SADDLE FAIRING. THE RIB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 55-01. A DOUBLER AND RIB WERE INSTALLED IAW SRM 55-01, 51-30-2, AND 51-30-5.

Part: ANGLE — CRACKED (RT PYLON) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK IN RIGHT PYLON PANEL 8212C L-ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND RT CUSP WEB CORRODED AT STA 503 - 598. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-14-2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND MID CARGO DOOR LOWER EDGE PAN CHAFED AND GOUGE AROUND ALL DOOR STOPS. DOUBLERS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-30-2, AND 51-30-3.

Part: PAN — DENTED (RT MLG DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND RIGHT MLG DOOR UPPER DOOR PAN DENTED AT DOOR HINGE. THE PAN WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND MID CARGO DOOR PAN AFT EDGE CHAFED AND GOUGED AROUND DOOR STOPS NR 6, 9 AND 10. REPAIRED IAW ECRA 5330-02819.

Part: STRAP — CORRODED (DOOR CUTOUT) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND MID CARGO DOOR CUTOUT REPAIR STRAP CORRODED. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-5, 53-05, FIGURE B, AND 51-10-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CUSP WEB CORRODED IN LT AFT BAG PIT AT FS 1174 - 1193, S18L. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK AT AFT UPPER CORNER OF INTERCOSTAL BETWEEN FS 1022 AND 1041, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM FITTING AT FS 294, BL 0. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND EXTERNAL FUSELAGE LOWER FILLET FAIRING STRUCTURE T-FITTINGS CRACKED AT FS 850 AND 865. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, 51-10-4, AND 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND RT CUSP WEB CORRODED AT FS 598 - 712. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-10-4.

Part: SUPPORT BRACKET — CRACKED (RT TAIL BAY) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND AN 8 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT BELOW RT WATER SEPARATOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-3, AND 51-30-1.

Part: SKIN — CHIPPED (PAX DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND THE L-1 DOOR SKIN CHIPPED IN FORWARD LOWER CORNER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.

Part: PANEL — CRACKED (RT WING) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN RT WING L/E PANEL 1222C. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 57-01, FIGURE 3, AND 51-30-2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND MID CARGO DOOR PAN CHAFED AND GOUGED AT DOOR STOPS NR 1, 2, AND 5. REPAIR DOUBLERS AND SHIMS WERE INSTALLED AT EACH DOOR STOP LOCATION IAW ECRA 5330-02819 AND SRM 51-10-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CORROSION ON I/B EDGE OF CUSP WEB AT FS 1222 AT SEAT TRACK SPLICE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-02.

Part: SPACER — CORRODED (DOOR FRAME) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND AFT CARGO LOWER DOOR JAMB SPACER CORRODED. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 140 - 200, LBL 7. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND BOTH R-1 DOOR GIRT BAR MOUNT FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-3, 51-10-4, 51-10-3, AND 51-30-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT FASTENER HOLE, STA 1322, LBL 40. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-3 AND 53-05, FIGURE 20A.

Part: DOUBLER — WORN (MLG DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT MLG DOOR AFT EDGE LOWER CHAFE STRIP WORN. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 52-05, FIGURE 28.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT CUSP WEBS CORRODED AT FS 503 - 598 AND FS 598 - 712. THE CUSP WEBS WERE REMOVED AND NEW CUSP WEBS WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1109. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT FS 146 - 200, LBL 44 AND AT FS 200, LBL 55. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-10-4, 51-30-05, AND 51-30-08.

Part: FITTING — CRACKED (TORQUE BOX) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK AT L-1 DOOR JAMB AFT TORQUE BOX LOWER AND UPPER LUGS, STA 207. THE CRACKED SECTIONS WERE REMOVED AND A DOUBLER AND FILLER REPAIR WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND EA 9-5314-2-A0797.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LT CUSP WEB CORRODED IN MID CARGO COMPARTMENT AT FS 737 - 756. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-2, 51-30-3, AND 51-30-4.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FORWARD CARGO DOOR PAN GOUGED AT DOOR STOP NR 5. THE GOUGED AREA WAS REMOVED AND A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-3.

Part: BRACKET — CORRODED (SERV DOOR SILL) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND AFT LT SERVICE DOOR THRESHOLD PAN MOUNTING BRACKET CORRODED. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-30-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND G-4 GALLEY ATTACH FITTING CORRODED AT FS 1174, LBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-5, AND 51-10-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND NUT PLATE AND FASTENER HOLE OF LT AFT CABIN FLOORBEAM CORRODED AT STA 1309, LBL 24. REPAIR ANGLES AND FILLER WERE INSTALLED IAW SRM 53-05, FIGURE 20A.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1079 - 1271. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-5, 51-10-3, AND 53-05, FIGURE 4F.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 146 - 200, RBL 55. THE COVER PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-30-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN GALLEY SUPPORT FITTINGS CORRODED AT FS 146, RBL 45 AND AT RBL 51. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT FS 200, LBL 14 AND AT FS 146 - 200, LBL 55. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-5 AND 51-30-02.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FORWARD CARGO DOOR PAN GOUGED AT DOOR STOP NR 7. A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-3.

Part: ANGLE — CRACKED (LT PYLON) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND A 1 INCH CRACK AT EACH END OF LT PYLON PANEL NR 8111C ATTACH SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FORWARD ENTRY AREA FLOOR SUPPORT WEB CORRODED AT STA 146, RBL 45 - 51. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-1, FIGURE 11, AND 51-10-3.

Part: PAN — GOUGED (CARGO DOOR) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND FORWARD CARGO DOOR PAN GOUGED AT STOP NR 6 AND NR 10. THE GOUGED AREA WAS REMOVED. A REPAIR DOUBLER AND SHIM WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 180, LBL 53. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT FS 200 - 246. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05 AND 51-30-1.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND THE L-1 DOOR JAMB CUSP WEB CORRODED AT STA 180 - 200. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-01, 51-10-3, 51-30-2, AND 53-14-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 198, LBL 50. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-10-4 AND 51-10-3.

Part: LONGERON — BENT (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND LONGERON 17L BENT AT FS 229. THE DAMAGED SECTION OF LONGERON WAS CUT OUT AND A NEW SPLICE WAS INSTALLED IAW SRM 51-30-2 AND 53-02, FIGURE 18.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 148, LBL 53. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND GALLEY FITTING CORRODED AT FS 146, RBL 10. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2.

Part: FITTING — CORRODED (GALLEY) · airframe 43,239 hrs · 20,765 cycles

INSPECTION FOUND GALLEY MOUNT FITTING CORRODED AT FS 218, RBL 12. THE FITTING WAS REMOVED AND REPLACED IAW SRM 53-10-3 AND 51-10-4.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,239 hrs · 20,765 cycles

INSPECION FOUND LEFT FLOOR SUPPORT ANGLE CORRODED ON UPPER SURFACE AROUND FASTENER HOLE AT FS 1183. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: BATTERIES — DISCHARGED (L1&R1 DOOR)

INSPECTION FOUND EMERGENCY LIGHTS ABOVE L-1 AND R-1 DOORS INOPERATIVE. THE BATTERIES IN FORWARD BATTERY PACK WERE REMOVED AND REPLACED.

Part: ANGLE — CRACKED (LT VERT STAB)

INSPECTION FOUND A .25 INCH CRACK IN AFT FUSELAGE LEFT VERTICAL STABILIZER ATTACH ANGLE. THE ANGLE WAS REPLACED IAW EA 5340-01012.

Part: SLIDING BLOCKS — INOPERATIVE (TAILCONE)

THE TAILCONE HUNG UP DURING RELEASE CHECK, HANDLE PULL WAS GOOD. BOTH UPPER SLIDING BLOCKS WERE REPLACED. A TAILCONE DROP/FUNCTIONAL CHECK WAS PERFORMED IAW MM 53-53-01 AND OPERATION CHECKED GOOD.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A 1 CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: UPLOCK SENSOR — INOPERATIVE (RT MLG)

AIRCRAFT HAD A BRIEF HISTORY OF THE RT MLG RED UNSAFE LIGHT REMAINING ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE RT MLG UPLOCK SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05, PAGE 207. THE GEAR WAS SWUNG AND GEAR OPERATION AND INDICATIONS WERE GOOD.

Part: T-4 BLADE — FAILED (NR 2 ENGINE)

CREW REPORTED A LOUD BANG WITH NR 2 ENGINE HIGH EGT AND EPR 1.44 WHILE EN ROUTE FROM LGA TO IAH. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED T-4 BLADE FAILURE AS PRIMARY CAUSE.

Part: SKIN — DENTED (BS 340-400)

THE FUSELAGE SKIN WAS DENTED AT STA 340-400 BETWEEN LONGERON 22R AND CUSP. A REPAIR WAS INSTALLED IAW ECRA 5330-02433.

Part: SKIN — DAMAGED (BS 265)

INSPECTION FOUND IMPACT DAMAGE TO LEFT FUSELAGE SKIN AT STA 265, LONGERON 15L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5330-02431.

Part: SUBFLOOR — CORRODED (BS 1136-1174)

INSPECTION FOUND CORROSION ON SUBFLOOR AT STA 1136-1174. THE CORRODED SECTION OF SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 946)

INSPECTION FOUND A .50 INCH CRACK IN KEEL STRUCTURE VERTICAL INTERCOSTAL AT STA 946, SIX INCHES RIGHT OF AIRCRAFT CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5.

Part: ANGLE — CRACKED (BS 946)

INSPECTION FOUND A .25 INCH CRACK IN KEEL STRUCTURE VERTICAL ANGLE AT STA 946, SIX INCHES LEFT OF AIRCRAFT CENTERLINE. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 946)

INSPECTION FOUND A .75 INCH CRACK IN KEEL STRUCTURE HORIZONTAL INTERCOSTAL AT STA 946, SIX INCHES RIGHT OF AIRCRAFT CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 946)

INSPECTION FOUND A .25 INCH CRACK IN KEEL STRUCTURE VERTICAL INTERCOSTAL AT STA 946, SIX INCHES LEFT OF AIRCRAFT CENTERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5.

Part: DOOR PAN — CRACKED (MAIN BAG BIN)

INSPECTION FOUND A 1 INCH CRACK AT FORWARD LATCH AREA OF MAIN BAGGAGE BIN DOOR PAN. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05.

Part: SUPPORT — CORRODED (BS 148-200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 148-200, LEFT OF CENTERLINE. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (PAX DOOR)

INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-3.

Part: CABLES — OUT OF ADJUST (TAILCONE)

THE TAILCONE WOULD NOT DROP WHEN RELEASE HANDLE WAS PULLED. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00.

Part: CLIPS — OUT OF ADJUST (TAILCONE)

THE TAILCONE EXTERIOR RELEASE HANDLE PULLED TOO LIGHT OUT OF CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00.

Part: PROX SENSOR — INOPERATIVE (RT MLG DOOR)

FLT NR 1896 - IAH - THE GEAR DOOR OPEN LIGHT ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM PHX. THE AIRCRAFT WAS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOOR PROXIMITY SENSOR IAW MM 32-60-05, PAGE 212. OPERATION OF THE GEAR DOOR OPEN LIGHT WAS RESTORED TO NORMAL. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

FLT NR 0340 - EWR - THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-15 WERE FOUND INOPERATIVE. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-15 WERE REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M)

Part: APU — INOPERATIVE (TAIL)

FLT NR 356 - EWR - THE APU WAS IN USE PRIOR TO TAKEOFF FROM EWR, BUT WAS SHUT DOWN BEFORE TAKING THE RUNWAY. SMOKE ENTERED THE CABIN MOMENTARILY AFTER TAKEOFF. THE SMOKE DISSIPATED AND THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. THE APU WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M)

Part: ACM — FAILED (LEFT)

FLT NR 0206 - CLE - A FLIGHT ATTENDANT NOTICED HAZE IN THE CABIN ON APPROACH TO CLE JUST BEFORE TOUCHDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT AIR CYCLE MACHINE BLOWING OIL. THE LEFT AIR CYCLE MACHINE WAS REMOVED AND REPLACED AND THE WATER SEPARATOR BAG WAS REPLACED. THE APU WAS RUN WITH PACK OPERATING AND OPERATION CHECKED GOOD WITH NO HAZE OBSERVED. (Z)