# N973NA: Aerospatiale/Aeritalia ATR 42-300, registration cancelled 2013-09-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 12, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Aerospatiale/Aeritalia ATR 42-300](https://openairdocs.org/model/aerospatiale-aeritalia-atr-42-300) (registry code 8680920)
- Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114)
- Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 065
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 8, 1987
- Certificate issued: November 19, 2001
- Last registry action: December 3, 2004
- Mode S code: AD8FF7
- Owner when cancelled: [International Airline Support Group Inc](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIRLINE%20SUPPORT%20GROUP%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.8885° N, 84.2895° W: Placed by OpenAirDocs at the center of ZIP code 30341, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N973NA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=973NA
- Page: https://openairdocs.org/deregistered/N973NA-2013-09-12

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Aerospatiale/Aeritalia ATR 42-300: https://openairdocs.org/model/aerospatiale-aeritalia-atr-42-300.md

## Service difficulty reports (19)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 99ZZZM666](https://openairdocs.org/sdr/99ZZZM666), Jun 3, 1999: FRAME. CORRODED. FRAME 27A LT CORRODED INBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-5
- [SDR 99ZZZM665](https://openairdocs.org/sdr/99ZZZM665), Jun 3, 1999: BULKHEAD WEB. CORRODED. FORWARD BULKHEAD BONDING STRIP AT 11:00 O'CLOCK POSITION HAS CORROSION PITTING. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND B
- [SDR 99ZZZM664](https://openairdocs.org/sdr/99ZZZM664), Jun 3, 1999: FITTING. CORRODED. FUSELAGE ATTACH FITTING FOR SPLICE CONNECTING FRAMES 27A RT AND LT CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYO
- [SDR 99ZZZM663](https://openairdocs.org/sdr/99ZZZM663), Jun 3, 1999: STRINGER. CORRODED. SPECIAL STRINGER ON LOWER KEEL BEAM, RIGHT SIDE HAS CORROSION BETWEEN FRAMES 24A RT AND 27A RT. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLE
- [SDR 99ZZZM662](https://openairdocs.org/sdr/99ZZZM662), Jun 3, 1999: STRINGER. CORRODED. SPECIAL STRINGER ON LOWER KEEL BEAM, LEFT SIDE HAS CORROSION BETWEEN FRAMES 24A LT AND 27A LT. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLEN
- [SDR 99ZZZM661](https://openairdocs.org/sdr/99ZZZM661), Jun 3, 1999: FRAME. CORRODED. FOUND FRAMES 28A RT CORRODED INBOARD AND OUTBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LI
- [SDR 99ZZZM660](https://openairdocs.org/sdr/99ZZZM660), Jun 3, 1999: INTERCOSTAL. CORRODED. FOUND INTERCOSTAL BETWEEN FRAMES 27A RT AND 28 RT BELOW STRINGER 16R CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BE
- [SDR 99ZZZM659](https://openairdocs.org/sdr/99ZZZM659), Jun 3, 1999: INTERCOSTAL. CORRODED. INTERCOSTAL BETWEEN FRAMES 27A LT AND 28A LT BELOW STRINGER 19 CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION REMOVED AND FOUND BEYOND L
- [SDR 99ZZZM658](https://openairdocs.org/sdr/99ZZZM658), Jun 3, 1999: FRAME. CORRODED. FOUND UPPER CHORD ON FRAME 27A RT CORRODED INBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION REMOVED AND FOUND BEYOND L
- [SDR 99ZZZM657](https://openairdocs.org/sdr/99ZZZM657), Jun 3, 1999: INTERCOSTAL. CORRODED. FOUND INTERCOSTAL BETWEEN FRAMES 27A RT AND 28A RT BELOW STRINGER 19 CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION REMOVED AND FOUND BE
- [SDR 99ZZZM656](https://openairdocs.org/sdr/99ZZZM656), Jun 3, 1999: FRAME. CORRODED. FOUND FORWARD CARGO DOOR INNER STRUCTURE HAS CORROSION AFT OF PRESSURE DOOR. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION REMOVED AND FOUND BEYO
- [SDR 99ZZZM655](https://openairdocs.org/sdr/99ZZZM655), Jun 3, 1999: FRAME. CORRODED. FOUND FRAME 27A RT CORRODED INBOARD AND OUTBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL CORROSION BLENDED AND FOUND BEYOND LIMI
- [SDR 99ZZZM654](https://openairdocs.org/sdr/99ZZZM654), Jun 3, 1999: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOORBEAM FRAME 41 CENTER AREA BY FITTING. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SR
- [SDR 98ZZZM357](https://openairdocs.org/sdr/98ZZZM357), Feb 23, 1998: SPAR. CORRODED. DURING ACCOMPLISHEMENT OF SB ATR 42-57-0044R2 AD 97-26-11, FOUND CORROSION DAMAGE ON THE LEFT WING REAR SPAR LOWER EXTRUSION FOUND OUT OF LIMITS. THE MANUFACTUR
- [SDR 98ZZZX2406](https://openairdocs.org/sdr/98ZZZX2406), May 14, 1997: SEAT TRACK. CORRODED. DURING A CPCP-4 CHECK PERFORMED AT AMR REGIONAL AIRCRAFT MAINTENANCE CENTER, SEAT TRACK FROM FRAMS 39 TO 41 HAVE CORRROSION IN LAVATORY. REMOVED AND REPLACED IA
- [SDR 98ZZZM541](https://openairdocs.org/sdr/98ZZZM541), May 14, 1997: SUPPORT. CORRODED. DURING A CPCP 4 CHECK PERFORMED AT AMR REGIONAL AIRCRAFT MAINTENANCE CENTER, CORROSION WAS FOUND ON THE SUPPORT BEAM THAT RUNS IN THE MIDDLE OF FRAME 39 AND 40 
- [SDR 98ZZZM540](https://openairdocs.org/sdr/98ZZZM540), May 14, 1997: SUPPORT. CORRODED. DURING A CPCP 4 CHECK PERFORMED AT AMR REGIONAL AIRCRAFT MAINTENANCE CENTER, CORROSION WAS FOUND ON THE SUPPORT BEAM THAT RUNS IN THE MIDDLE OF FRAME 39 AND 40 
- [SDR 96ZZZM1282](https://openairdocs.org/sdr/96ZZZM1282), Jul 14, 1996: TRANSFER TUBE. LOOSE. DURING CLIMB, CREW RECEIVED FIRE INDICATION ON THE LEFT ENGINE AND FIRE BOTTLE WAS DISCHARGED. FOUND NR 14 SECONDARY FUEL NOZZLE TRANSFER TUBE LOOSE WITH FUEL L
- [SDR 96ZZZM608](https://openairdocs.org/sdr/96ZZZM608), Jan 27, 1995: FITTING. CRACKED. DURING PHASE NR 4 INSPECTION, FOUND NR 2 ENGINE LEFT AFT LATERAL ENGINE MOUNT ATTACHMENT FITTING CRACKED WITH NO VIBRATION OR DISCREPANCY REPORTED DURING FLIGHT

## Other aircraft with N973NA

- [Registered now](https://openairdocs.org/aircraft/N973NA): Bell 206B, S/N 3884

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