N319UA

Part: ACTUATOR — FAILED (NLG) · airframe 45,492 hrs · 25,385 cycles

ON GEAR RETRACTION NOSE GEAR RED AND GREEN LIGHTES REMAINED ON WITH GRINDING SOUND. ALSO AIR NOISE AS IF GEAR DID NOT FULLY RETRACT. FOUND NOSE GEAR LOCK ACTUATOR LEAKING. REPLACED ACTUATOR. ACCOMPLISHED SEVERAL GEAR SWING AND MANUAL EXTENSION. NO SYSTEM FAULT NOTED. ALL INDICATIONS FOUND NORMAL.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

STRINGER CLIP CRACKED AT BS 597, STR 2L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

CABIN FLOORBEAM CLIP CRACKED AT BS 328, RBL 32, WL 200. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

LT MID CABIN UPPER T-CHORD CRACKED LATERALLY IN VERTICAL LEG, JUST BELOW UPPER RADIUS FILLER, AT BS 520, LBL 24. ACCOMPLISHED ANGLE REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BULKHEAD WEB HAS OIL CANNING AND DENTED AND PUCKERED FASTENER HOLES, AT BS 178. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

STRINGER-FRAME CLIP CRACKED AT BS 663.75, STR 10R. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

AFT GALLEY DOORWAY STOP FITTING, 2 LOWER AFT FASTENER HOLES OF DOOR ASSIST HANDLE HAVE CRACKS. ACCOMPLISHED FRAME SPLICE STRAP REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BULKHEAD WEB EXTERIOR SURFACE CRACKED AT FASTENER, AT BS 178, WL 234, LBL 12. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BS 178 BULKHEAD WEB HAS WEAR DAMAGE AT WL 218 O/B EDGE, AND OIL CANNING AT WL 203, RBL 21 ABOVE ACCESS HOLE. ACCOMPLISHED DOUBLER AND TRIPLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

STRINGER-FRAME CLIP CRACKED AT BS 663.75, STR 11L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

STRINGER CLIP CRACKED AT BS 597, STR 3L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BULKHEAD WEB HAS CRACK AT 4 RADAR ANTENNA MOUNTS, AT BS 178, WL 207, BL 0. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

AFT ENTRY DOORWAY ASSIST HANDLE FITTING AFT 2 FASTENER HOLES ARE CRACKED. ACCOMPLISHED REPAIR STRAP AND FRAME SPLICE STRAP. MAJOR REPAIR ACCOMPLISHED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

LT VERTICAL WEB FRAME CRACKED AT BS 188. INSTALLED WEB REPAIR ANGLE. EXTENDED SKIN DOUBLER TO REPAIR THE SKIN CUTOUT. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BULKHEAD WEB HAS EXCESSIVE MATERIAL LOSS AT BS 178, LBL 28, WL 216. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — FRETTED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

FUSELAGE BHD WEB IS FRETTED WORN AT RADOME BRACKET AT BS 178, LBL 27, WL 203. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: DENTED (OUTER SKIN) · airframe 40,493 hrs · 22,207 cycles

FWD CARGO DOOR HAS NUMEROUS DENTS BEYOND LIMITS. CUT OUT DENTED AREAS AND INSTALLED EXTERNAL DOUBLER. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

WEAR DAMAGE ON OUTBOARD WEB AT BS 178, RBL 21, WL 203. ACCOMPLISHED REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

CABIN FLOORBEAM WEB HAS EXCESSIVE MATERIAL LOSS AT BS 1016, LBL 28. ACCOMPLISHED REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 40,493 hrs · 22,207 cycles

VERTICAL STABILIZER ATTACH LUGS CORRODED. MAJOR REPAIR ACCOMPLISHED. OVERSIZED BORES AND INSTALLED NEW BUSHINGS.

Part: FRAME — MISDRILLED · airframe 40,493 hrs · 22,207 cycles

FRAME SHEAR TIE HAS MISDRILLED HOLE. STA 967, OB OF STR 4R. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND NEW SHEAR TIE.

Part: FRAME — DAMAGED · airframe 40,493 hrs · 22,207 cycles

FWD PIT FRAME DAMAGED. STA 500, STR 25R TO STR 26R. MAJOR REPAIR ACCOMPLISHED.INSTALLED J-ANGLE REINFORCEMENT REPAIR.

Part: FRAME — DAMAGED · airframe 40,493 hrs · 22,207 cycles

FRAME WEB DAMAGED. STA 616, RBL 64. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW WEB AND DOUBLER.

Part: KEELBEAM — WORN (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

KEEL BEAM LT LOWER CHORD OUTBOARD FLANGE, TWO HOLES WORN STA 712 - 720. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR AND FREEZE PLUGS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

INTERCOSTAL CRACKED STA 178, WL 207, RBL 24. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

CREASE BEAM WEB CORRODED STA 635, LBL 69, WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

FLOORBEAM CORRODED STA 1016. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM UPPER CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

FLOORBEAM CORRODED AT BS 1006, RBL 15 TO RBL 30. REPLACED FLOORBEAM UPPER T-CAP SECTION. MAJOR REPAIR ACCOMPLISHED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

FWD GALLEY DOOR AFT CUTOUT FRAME CRACKED. INSTALLED REPAIR ANGLE DOUBLER. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

BULKHEAD WEB CRACKED AT BS 178, WL 184, RBL 1. ACCOMPLISHED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

WEB CRACKED AT BS 178, WL 234, RBL 12. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,493 hrs · 22,207 cycles

STRINGER CLIP CRACKED AT BS 639, STR 8L. REPLACED CLIP. MAJOR REPAIR ACCOMPLISHED.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 38,317 hrs · 21,046 cycles

AIRFRAME VIBRATION. *S/D* LEFT ELEVATOR TAB INBOARD HINGE FITTING BEARING AND HARDWARE HAVE EXCESSIVE WEAR. REMOVED TAB, REPLACED MOST INBOARD HINGE BUSHINGS AND BOLT.

Part: FAIRNG — NOT SEALED (BS 580)

VIBRATION AND HUM ADJACENT TO ROW 9. THE REPORTED VIBRATION THAT WAS HEARD FROM ROW 9 (LEFT) WAS A RESULT OF DETERIORATED SEALANT ON THE UPPER WING TO BODY FAIRING AT THAT SAME LOCATION. THE FAIRING WAS RESEALED AT THE IMC AND THE AIRCRAFT RELEASED.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT FLOOR LIGHT STRIP AT ROW 12 IS INOP. *S/D* REPLACED TWO EEL STRIPS AND A SECTION OF TRACK. LIGHTS OPS CHECK GOOD.

Part: NR 3 BEARING — FAILED (COMPRESSOR)

OIL BURNING ODOR NOTICED ON CLIMB-OUT IN COCKPIT AND IN CABIN. THREE SELF-LOCKING SHANK NUTS HAD DAMAGED THREADS GIVING FALSE READING WHEN THE BOLTS WERE TORQUED. THIS CAUSED AN IMPROPER SEAL BETWEEN THE NR 3 BEARING AIR/OIL SEAL AND THE FAN FRAME. AIR VAPORS MIXED WITH THE PRIMARY AIR FLOW AND EXITING AT THE 5TH STAGE BLEED VALVE ALLOWING THE SMELL TO PROGRESS INTO THE CABIN. ENGINE WAS REPLACED.

Part: COALESCER BAG — DIRTY (CABIN)

AIR CONDITIONING ODOR IN ALL CABINS DURING CLIMB ON BOTH PACKS. ACCOMPLISHED CHRONIC REVIEW OF BOTH PACKS. COALESCER BAGS WERE REPLACED. ODOR WENT AWAY. REPLACED AIR CYCLE MACHINE FOR PRECAUTION. OPS CHECK GOOD.