N720AX

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
OMNI AIR INTERNATIONAL LLC (CNMA)Operator2008-05-19 – 2008-05-19Operator named in NTSB report
Omni Air InternationalOperator2008-05-19 – 2008-05-19Operator named in NTSB report

Accident & incident history

Acc · 2008-05-19 Operator named in NTSB report
MCDONNELL DOUGLAS DC10 Serious injury Part 121OMNI AIR INTERNATIONAL LLC
Source: NTSB case DCA08FA062

Maintenance disclosures

B · 2011-04-11 Matched by certificate designator
ATA 2170

OILY BURNING ODOR THROUGHOUT CABIN AND FLIGHT DECK. AFTER REPLACEMENT OF NR 1 PACK & COALESER BAGS, RAN ENGINES AT MPA ONE AT A TIME & ISOLATED PNEUMATICS, NO OBVIOUS ODOR ON FLT DECK, CABIN OR LOWER GALLEY AREA.

Source: SDR CNMA20110010 · FAA SDRS
F · 2010-07-02 Matched by certificate designator
ATA 3234

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.

Source: SDR CNMA20100027 · FAA SDRS
L · 2009-02-02 Matched by certificate designator
ATA 3350

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

Source: SDR CNMA20090124 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5347

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.

Source: SDR CNMA20090119 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090114 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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

Source: SDR CNMA20090120 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5754

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.

Source: SDR CNMA20090107 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090115 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5314

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.

Source: SDR CNMA20090123 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090116 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090117 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090118 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5311

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.

Source: SDR CNMA20090103 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090104 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090105 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090106 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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,

Source: SDR CNMA20090110 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5230

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.

Source: SDR CNMA20090109 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA20090108 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090121 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090111 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090112 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090113 · FAA SDRS
O · 2009-02-02 Matched by certificate designator
ATA 5315

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.

Source: SDR CNMA20090122 · FAA SDRS
R J · 2007-01-03 Matched by certificate designator
ATA 7230

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.

Source: SDR CNMA20070001 · FAA SDRS
N · 2006-05-29 Matched by certificate designator
ATA 2611

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.

Source: SDR CNMA20060013 · FAA SDRS
L · 2004-10-15 Matched by certificate designator
ATA 2565

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.

Source: SDR 2004000014 · FAA SDRS
P · 2001-12-14 Matched by certificate designator
ATA 3350

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

Source: SDR CNMA200100037 · FAA SDRS
L · 2001-04-26 Matched by certificate designator
ATA 3350

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

Source: SDR CNMA200100023 · FAA SDRS
L · 2001-04-16 Matched by certificate designator
ATA 3350

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

Source: SDR CNMA200100022 · FAA SDRS
L · 2001-04-10 Matched by certificate designator
ATA 3350

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

Source: SDR CNMA200100021 · FAA SDRS
O · 2000-12-13 Matched by certificate designator
ATA 5320

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.

Source: SDR CNMA200100010 · FAA SDRS
O · 2000-12-11 Matched by certificate designator
ATA 5315

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

Source: SDR CNMA200100009 · FAA SDRS