N720AX

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 86,155 hrs · 21,579 cycles

LANDING GEAR HANDLE WOULD NOT COME UP. FOLLOWED QRH PROCEDURE, RETURNED TO DEPARTURE. JACK ACFT IAW MM-07-11, PERFORM EXTENSION & RETRACTION OF ALL MLG'S. OPS CKS NORMAL AIW MM 32-30 DOWN JACK ACFT IAW MM 07-11.

Part: FLOORBEAM — CORRODED (BS 1941) · airframe 82,794 hrs · 21,039 cycles

BS1941, RBL40 CORROSION ON FLOORBEAM. DAMAGED FLOORBEAM REMOVED. FABRICATED NEW FLOORBEAM IAW SRM VOL 3, 53-16-01 FIG 8 GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,794 hrs · 21,039 cycles

EMERGENCY LIGHT WOULD NOT PASS TEST. EMERG LIGHT BATTERY PACK POS "OVERWING" REPLACED AND TESTED IAW AMM 33-50-00, PASSED OK.

Part: SEAT TRACK — CORRODED (BS 1887-1941) · corrosion level 2 · airframe 82,794 hrs · 21,039 cycles

BS 1887-1941, LBL 27, CORROSION ON SEAT TRACK. DAMAGED SEAT-TRACK PORTION REMOVED, REINFORCED AREA WITH NEW PORTION OF SEAT-TRACK AND SPLICE. IAW SRM VOL 1, 53-70-00, FIG 1. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: SKIN — CORRODED (NR 2 SLAT) · airframe 82,794 hrs · 21,039 cycles

LT WING, SLAT 2, OTBD GAP STRAP HAS SURFACE CORROSION AND MISSING RIVETS. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH NEW SLAT SEAL REPAIR IAW SRM VOL 1, 57-10-00, FIG 32. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOOR SUPPORT — CORRODED (BS 457-515) · airframe 82,794 hrs · 21,039 cycles

B/T STA 457 AND STA 515 BL-0 CORROSION ON FLOOR SUPPORT. DAMAGED FLOOR SUPPORT AND NEW PART INSTALLED USING FASTENERS IAW SRM VOL 2, 51-31-01 NAS 517-2-6 B/N: 749-19-03, MS21032L3, B/N: 513300459.

Part: FLOOR SUPPORT — CORRODED (BS 1964) · airframe 82,794 hrs · 21,039 cycles

BS 1964, LBL 62 CORROSION ON FLOOR SUPPORT. GMM 4.45 AND INSTALLED WITH FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOORBEAM — CORRODED (BS 1256) · airframe 82,794 hrs · 21,039 cycles

BS1256, RBL 28-46, THERE IS A CRACK ON THE FLOORBEAM. DAMAGED FLOORBEAM REMOVED, NEW FABRICATED IAW SRM VOL 3, 53-14-01 FIG 5 AND GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOORBEAM — CRACKED (BS 1239) · airframe 82,794 hrs · 21,039 cycles

BS 1239 LBL 29-46 THERE IS A CRACK ON THE FLOORBEAM. DAMAGED FLOORBEAM REMOVED, NEW FABRICATED IAW SRM VOL 3. 53-14-01 FIG 5 AND GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 2. 51-21-01.

Part: SUPPORT — CORRODED (BS 1941) · airframe 82,794 hrs · 21,039 cycles

STA 1941, RBL 52 CORROSION ON GALLEY SUPPORT AROUND NUT PLATES. DAMAGED GALLEY SUPPORT REMOVED AND NEW FASTENERS INSTALLED IAW SRM VOL 2, 51-31-01,

Part: FLOORBEAM — TORN (BS 1871) · airframe 82,794 hrs · 21,039 cycles

BS1871, RBL45, FLOORBEAM IS TORN. TORN FLOORBEAM REMOVED FABRICATEDNEW FLOORBEAM IAW SRM VOL 3, 53-14-01 FIG 5 AND GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 3, 51-31-01.

Part: FLOOR SUPPORT — CORRODED (BS 1964) · airframe 82,794 hrs · 21,039 cycles

STA 1964, RBL 62 CORROSION ON FLOOR SUPPORT. CORRODED FLOOR SUPPORT REMOVED NEW FABRICATED PN: OAI-53-0017 IAW SRM VOL.3 53-16-01 FIG 8 AND GMM 4.45 AND INSTALLED WITH FASTENERS IAW SRM VOL 2 51-31-01.

Part: FLOORBEAM — CRACKED (BS 1239) · airframe 82,794 hrs · 21,039 cycles

BS1239, LBL 48-74 THERE IS A CRACK ON THE FLOORBEAM. DAMAGED FLOORBEAM REMOVED, NEW FABRICATED. IAW SRM VOL 3, 57-14-01 FIG 5 AND OMNI GMM 4.45. INSTALLED FASTENERS IAW SRM VOL.2. 51-31-01.

Part: FLOOR SUPPORT — CORRODED (BS 401-428) · airframe 82,794 hrs · 21,039 cycles

B/T STA 401 AND STA 428, RBL 20 CORROSION ON FLOOR SUPPORT. DAMAGED FLOOR SUPPORT REMOVED, NEW FLOOR SUPPORT INSTALLED. INSTALLED FASTENERS IAW SRM VOL 2 51-31-01.

Part: FLOORBEAM — TORN (BS 1821) · airframe 82,794 hrs · 21,039 cycles

STA 1821, BL-0 UPPER FLANGE OF FLOORBEAM IS TORN (UNDER CENTER RAIL). DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH ANGLES AND E FILLERS IAW SRM 53-00-01 FIG 2. INSTALLED FASTENERS IAW SRM VOL 2 51-31-01.

Part: WEB — CORRODED (CARGO DOOR) · airframe 82,794 hrs · 21,039 cycles

CORROSION ON CTR CARGO DOOR WEB NEAR LATCHES. DAMAGED AREA TRIMMED-OUT. REINFORCED AREA WITH DOUBLER AND FILLERS IAW SRM VOL 1, 53-00-01, FIG 10 AND INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOORBEAM — CORRODED (BS 1964) · airframe 82,794 hrs · 21,039 cycles

BS 1964, RBL 43-46 CORROSION ON FLOORBEAM. DAMAGED FLOORBEAM REMOVED, AND NEW FABRICATED IAW SRM VOL 3, 53-16-01 FIG 8 AND GMM 4-45. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOOR SUPPORT — CORRODED (BS 401-428) · airframe 82,794 hrs · 21,039 cycles

B/T STA 401 AND STA 428 LBL 20 CORROSION ON FLOOR SUPPORT. DAMAGED FLOOR SUPPORT REMOVED AND NEW PN:ABA7-334-1 INSTALLED FASTENERS IAW SRM VOL.2.

Part: FRAME — CORRODED (BS 879) · airframe 82,794 hrs · 21,039 cycles

STA 879, RBL 50 CORROSION AND DENT ON WEB OF FRAME. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLER AND FILLER PN: N720AX-NRC361-11-2 IAW SRM VOL 1, 53-00-01, FIG 10 USING FASTENERS IAW SRM VOL 2, 51-31-01.

Part: SUPPORT — CORRODED (BS 1900-1964) · airframe 82,794 hrs · 21,039 cycles

BS 1900-1964, LBL 52, CORROSION ON GALLEY SUPPORT. DAMAGED GALLEY SUPPORT REMOVED AND NEW INSTALLED USING FASTENERS, IAW SRM VOL 2, 51-31-01.

Part: TRACK — CORRODED (BS 457-475) · airframe 82,794 hrs · 21,039 cycles

B/T STA 457 AND STA 475, LBL 58, CORROSION ON TRACK. (HOLE AREA) DAMAGED AREA TRIMMED-OUT. REINFORCED AREA WITH DOUBLERS AND FILLERS IAW SRM VOL 1, 53-00-01 FIG, 2 INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: FLOORBEAM — CORRODED (BS 878) · airframe 82,794 hrs · 21,039 cycles

STA 878, B/T LBL28 AND LBL60 DEEP CORROSION ON FLOORBEAM. DAMAGED FLOORBEAM REMOVED, NEW FABRICATED IAW SRM VOL 3, 53-13-01 FIG 24 AND GMM 4.45. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: SUPPORT ANGLE — CORRODED (BS 832) · airframe 82,794 hrs · 21,039 cycles

STA 832, LBL 12 DEEP CORROSION ON SUPPORT ANGLE. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE IAW SRM VOL1, 53-00-01 FIG 8. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.

Part: COMPRESSOR — DAMAGED (ENGINE) · airframe 77,557 hrs · 20,073 cycles

NR 2 ENGINE FAILED ON TAKEOFF ROLL AT 70KTS TAKEOFF ABORTED. N1 WAS 103.0 EGT PEGGED. RAN ENGINE FIRE SEVERE DAMAGE CHECK LIST NO FIRE. R & R NR 2 ENGINE IAW 10UN-201. ENGINE S/N 517-533 INSPECTION REVEALED NO SIGNS OF FOD TO THE COMPRESSOR SECTION BUT HEAVY IMPACT DAMAGE EXTENDING TO STG 4 LPT. 5 EA STAGE 1 NOZZLE SEGMENTS HAD LOST RETENTION AND HAD GONE IN CONTACT WITH THE STAGE 1 ROTOR BLADES.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 76,223 hrs · 19,750 cycles

LAV -A- SMOKE DETECTOR ACTIVATED IN FLIGHT, NO SMOKE OBSERVED. INSPECTED, NO DEFECTS NOTED. REPLACED LAVATORY SMOKE DETECTOR PRECAUTIONARY IAW SMM 26-14. UNIT REPAIRED FRONT DAMAGED REPLACED FRONT.

Part: SLIDE — FAILED (L-3 DOOR) · airframe 78,008 hrs · 19,317 cycles

L-3 SLIDE/RAFT DID NOT FULLY DEPLOY DURING ACCOMPLISHMENT OF OMNI AIR WORKCARD 101C-744 (FUNCTIONAL CHECK OF SLIDE/RAFT FOR C-CHECK REQUIREMENTS) SLIDE/RAFT ASPIRATOR PART NUMBER 31002-201 SEPARATED FROM RAFT DUE TO IMPROPER INSTALLATION OF RETAINING RING.

Part: BATTERY PACK

EMERG. LITES WILL NOT GIVE GREE LITE DURING TEST-ALL LIGHTS OPERATEFOUND MID CABIN EMERG LITES POWER SUPPLY INOP R/R MIDCABIN PWR SUPPLY OPS CKD NORMALLY PER M/M 33-51

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS DO NOT TEST. REPLACED MID CABIN BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

L1 AND R1 DOOR EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY. REPLACED BOTH L1 AND R1 EMERGENCY LIGHT BATTERY PACKS.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT TEST FAILED. REPLACED NR 4 EMERGENCY LIGHTING POWER SUPPLY AND BATTERY.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,981 hrs · 17,228 cycles

NR 1 AIR CONDITION BAY INTERCOSTAL ATTACH ANGLE AT FS 585 CORRODED AFT OF NR 1 PACK EXHAUST DUCT. REMOVED INTERCOSTAL, TREATED AND PRIMED. FABRICATED NEW ATTACH ANGLE AND INSTALLED INTERCOSTAL IAW SRM 51-31-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,981 hrs · 17,228 cycles

LOWER CENTER CARGO COMPARTMENT FLOOR SUPPORT BEAM HAS A 13 INCH CRACK. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-60-01.