# N648AW: 1997 Airbus Industrie A320-232, registration cancelled 2017-04-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 13, 2017
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-232](https://openairdocs.org/model/airbus-industrie-a320-232) (registry code 3930326)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 770
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 17, 1998
- Certificate issued: March 10, 2015
- Last registry action: March 10, 2015
- Mode S code: A88308
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N648AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=648AW
- Page: https://openairdocs.org/deregistered/N648AW-2017-04-13

From the FAA registry file of October 29, 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 Airbus Industrie A320-232: https://openairdocs.org/model/airbus-industrie-a320-232.md

## Service difficulty reports (138, newest 50)

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

- [SDR USAA2014081400004](https://openairdocs.org/sdr/USAA2014081400004), Aug 13, 2014: LENS. BROKEN. DOOR 1L EMER EXIT LIGHT LENS COVER BROKEN. REPLACED DOOR 1L EMER EXIT LIGHT LENS.
- [SDR USAA2014012100002](https://openairdocs.org/sdr/USAA2014012100002), Jan 19, 2014: LENS. MISSING. DOOR L2 EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED DOOR L2 EMERGENCY EXIT LIGHT LENS IAW AMM 25-60-00.
- [SDR USAA2014011300014](https://openairdocs.org/sdr/USAA2014011300014), Jan 12, 2014: HANDLE. DIRTY. INFLIGHT DOOR L2 ARM LEVER STANDS OUT ABOUT 1/8 INCH CAUSING THE RED CABIN PRESS LIGHT ON THE DOOR TO FLASH OFF & ON WITH THE ECAM PAGE SHOWING DOOR L2 DISARMED
- [SDR USAA2013100900002](https://openairdocs.org/sdr/USAA2013100900002), Oct 8, 2013: FLASHLIGHT. INOPERATIVE. FORWARD F/A OTBD FLASHLIGHT BATTERY INDICATION INOPERATIVE AND SAFETY STRAP DAMAGED. REPLACED FORWARD FLASHLIGHT AND SAFETY STRAP.
- [SDR USAA2013032200004](https://openairdocs.org/sdr/USAA2013032200004), Mar 21, 2013: SOLENOID VALVE. FAILED. COMPRESSOR STALL ON TAKEOFF. COMPRESSOR VANE FAULT NR 1 ENGINE. ENGINE BORESCOPED, NO DEFECTS NOTED IN AREAS SURVEYED. REMOVED AND REPLACED HIGH PRESSURE COMPRE
- [SDR USAA2012121900007](https://openairdocs.org/sdr/USAA2012121900007), Dec 18, 2012: WIRE HARNESS. CONTAMINATED. ON ENGINE NR 2 START, EGT OVERLIMIT AND AUTO SHUTDOWN. MAINTENANCE FOUND EXCESSIVE MOISTURE IN EGT HARNESS CONNECTORS AND JUNCTION BOX. DRIED AREA WITH NITROGEN
- [SDR USAA2012112900023](https://openairdocs.org/sdr/USAA2012112900023), Nov 27, 2012: LENS. MISSING. 3C LOW LEVEL EMERGENCY LIGHT PUSHED IN AND LENS COVER IS MISSING. REPLACED 3C EMERGENCY LIGHT LENS COVER.
- [SDR USAA2012051500004](https://openairdocs.org/sdr/USAA2012051500004), May 14, 2012: CONNECTOR. NOT SEATED. C11 C HECK - EPSU INTERNAL LOAD EMERGENCY LIGHT COMES UP ON CIDS DURING EMERGENCY LIGHTING TEST. RESEATED CONNECTOR ON EPSU BATTERY PACK AND PERFORMED OPERATION
- [SDR USAA2012051400001](https://openairdocs.org/sdr/USAA2012051400001), May 10, 2012: LENS. CRACKED. C11 CHECK - CRACKED LENSES ON EMERGENCY EXIT LIGHTS AT ROWS 10ABC AND 11ABC. REPLACED EMERGENCY EXIT LIGHT LENSES AT ROWS 10ABC AND 11ABC IAW A320 AMM 33-51-400
- [SDR USAA2012051600015](https://openairdocs.org/sdr/USAA2012051600015), May 8, 2012: FRAME. CRACKED. C11 CHECK - CRACK ON AFT FRAME SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR AT STA 1792. REPLACED AFT FRAME SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228.
- [SDR USAA2012051600014](https://openairdocs.org/sdr/USAA2012051600014), May 8, 2012: FRAME. CRACKED. C11 CHECK - CRACK ON FORWARD FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT STA 1738. REPLACED FORWARD FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR IAW EO 
- [SDR USAA2012051600013](https://openairdocs.org/sdr/USAA2012051600013), May 8, 2012: FRAME. CRACKED. C11 CHECK - CRACK ON AFT FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT STA 1738. REPLACED AFT FRAME SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228
- [SDR USAA2012051400031](https://openairdocs.org/sdr/USAA2012051400031), May 5, 2012: SKIN. SATURATED. C11 CHECK - NUMEROUS AREAS OF FLUID INGRESS ON RIGHT ELEVATOR UPPER SURFACE APPROX 26 INCHES FROM INBOARD EDGE THRU 1105 INCHES FROM INBOARD EDGE. REPAIRED RIGH
- [SDR USAA2011120900007](https://openairdocs.org/sdr/USAA2011120900007), Dec 7, 2011: UNKNOWN. ODOR. AFTER TAKEOFF CLIMBING OUT, STRONG DIRTY SOCK SMELL STARTED IN THE CABIN AND PROGRESSED INTO THE COCKPIT. DUE TO TOXIC FUMES, RETURNED FOR OVERWEIGHT LANDING. R
- [SDR USAA2011102100003](https://openairdocs.org/sdr/USAA2011102100003), Oct 20, 2011: BATTERY. DISCHARGED. "A" FLIGHT ATTENDANT REPORTED FORWARD GALLEY FLASHLIGHT FAILED TO TEST - BLINKING LIGHT DID NOT ILLUMINATE. MAINTENANCE REPLACED BATTERY IN FLASHLIGHT.
- [SDR USAA2011102100002](https://openairdocs.org/sdr/USAA2011102100002), Oct 19, 2011: DOOR. CONTAMINATED. WHILE EN ROUTE PHX-JFK, FLIGHT ATTENDANTS REPORTED AMMONIA TYPE FUMES NEAR THE L1 DOOR. CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. MAINTENANCE FOUND EXCESS
- [SDR USAA2011081100007](https://openairdocs.org/sdr/USAA2011081100007), Aug 10, 2011: OXYGEN MASK. DEFECTIVE. FIRST OFFICER'S O2 MASK LENS RETENTION CLIPS NOT SECURED. MAINTENANCE REMOVED AND REPLACED F/O'S O2 MASK IAW AIRBUS MAINTENANCE MANUAL 35-12-41-000-002.
- [SDR USAA2011071800014](https://openairdocs.org/sdr/USAA2011071800014), Jul 15, 2011: DIAPHRAGM. LEAKING. R-1 DOOR EMERGENCY CYLINDER LOW 1300 PSI. SERVICED R-1 DOOR EMERGENCY CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-10-00. MAINTENANCE REPLACED DIAPHRAGM AND SEALS 
- [SDR USAA2011051391844](https://openairdocs.org/sdr/USAA2011051391844), May 11, 2011: BOTTLE. LOW PRESSURE. FLT 63 - BOS-CLT - EMERGENCY EGRESS SYSTEM - R1 DOOR BOTTLE NEEDS SERVICE. SERVICED R1 DOOR ASSIST BOTTLE PER AMM 52-10-00. OPERATIONAL CHECK WAS GOOD.
- [SDR USAA2011042091558](https://openairdocs.org/sdr/USAA2011042091558), Apr 19, 2011: CIDS. MALFUNCTIONED. FLT 430 - LAS - EEL - EMERGENCY EXIT LIGHTS FAIL BITE CHECK. MAINTENANCE RESET CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) IAW AIRBUS MAINTENANCE MANUAL 23-73-0
- [SDR USAA2011040991393](https://openairdocs.org/sdr/USAA2011040991393), Apr 8, 2011: CYLINDER. LOW PRESSURE. FLT 83 - PHX-SEA - EMERGENCY EGRESS SYSTEM - DOOR R1 EMERGENCY CYLINDER PRESSURE IS LOW. SERVICED DOOR R1 EMERGENCY CYLINDER AS REQUIRED PER AMM 52-10-00-614-00
- [SDR USAA2011012190310](https://openairdocs.org/sdr/USAA2011012190310), Jan 20, 2011: BOTTLE. LOW PRESSURE. FLT 307 - LAS - EES - R-1 DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED R-1 DOOR ASSIST BOTTLE TO PROPER PRESSURE.
- [SDR USAA2011011890240](https://openairdocs.org/sdr/USAA2011011890240), Jan 15, 2011: BATTERY. DISCHARGED. FLT 172 - PHX - EEL - FORWARD FLIGHT ATTENDANT JUMPSEAT INBOARD "C" POSITION BREAKWAY FLASHLIGHT OFF MOUNT. MAINTENANCE REPLACED FLASHLIGHT BATTERY AS REQUIRED.
- [SDR USAA2011010590051](https://openairdocs.org/sdr/USAA2011010590051), Jan 4, 2011: ACCUMULATOR. LOW PRESSURE. FLT 76 - SEA - EES - R-1 DOOR ASSIST ACCUMULATOR PRESSURE IS LOW. MAINTENANCE SERVICED R-1 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-00
- [SDR USAA2010111792615](https://openairdocs.org/sdr/USAA2010111792615), Nov 16, 2010: CYLINDER. LOW PRESSURE. FLT 74 - SEA - EES - R1 DOOR ASSIST ACCUMULATOR PRESSURE IS LOW. MAINTENANCE SERVICED R1 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.
- [SDR USAA2010102992441](https://openairdocs.org/sdr/USAA2010102992441), Oct 28, 2010: BOTTLE. LOW PRESSURE. FLT 614 - ATL - EES - R-1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED R-1 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001-0.
- [SDR USAA2010082391742](https://openairdocs.org/sdr/USAA2010082391742), Aug 20, 2010: LIGHT. INOPERATIVE. FLT 74 - SEA - EEL - EMERGENCY LIGHT AT ROW 17C IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT AT ROW 17C.
- [SDR USAA2010082391741](https://openairdocs.org/sdr/USAA2010082391741), Aug 20, 2010: LENS. MISSING. FLT 74 - SEA - EEL - RED EMERGENCY LIGHT LENS IS MISSING AT ROW 9C. MAINTENANCE INSTALLED NEW LENS AT ROW 9C.
- [SDR USAA2010081691670](https://openairdocs.org/sdr/USAA2010081691670), Aug 13, 2010: LENS. MISSING. FLT 504 - PHX - EEL - EMERGENCY EXIT LIGHT LENS MISSING AT ROW 9 LEFT. MAINTENANCE INSTALLED LENS AT ROW 9 LEFT.
- [SDR USAA2010021790389](https://openairdocs.org/sdr/USAA2010021790389), Feb 16, 2010: BATTERY PACK. FAILED. FLT 430 - LAS - EEL - RIGHT MID CABIN EMERGENCY BATTERY PACK FAILS TEST. MAINTENANCE REPLACED RIGHT MID CABIN EMERGENCY LIGHT BATTERY PACK.
- [SDR USAA2010021190339](https://openairdocs.org/sdr/USAA2010021190339), Feb 10, 2010: CYLINDER. LOW PRESSURE. FLT 77 - SEA - EES - DOOR ASSIST PRESSURE LOW AT 1 RT. MAINTENANCE SERVICED PRESSURE AT DOOR 1 RT CYLINDER.
- [SDR USAA2009121593343](https://openairdocs.org/sdr/USAA2009121593343), Dec 14, 2009: BATTERY. DISCHARGED. FLT 343 - FLIGHT ATTENDANT REPORTS FLASHLIGHT AT JUMPSEAT C INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT JUMPSEAT C FLASHLIGHT.
- [SDR USAA2009061991514](https://openairdocs.org/sdr/USAA2009061991514), Jun 18, 2009: LENS. MISSING. INSP - DFW - EEL - ROW 4 OVERHEAD HAS EMERGENCY LIGHT LENS MISSING. MAINTENANCE REPLACED MISSING LENS.
- [SDR USAA2009022790452](https://openairdocs.org/sdr/USAA2009022790452), Feb 21, 2009: MECHANISM. FAULTY. SAL - C8 - EES - FAULT PROXIMITY SWITCH RELEASE MECHANISM EMERGENCY ESCAPE AT PASSENGER/CREW DOOR 832. REPLACED PROXIMITY SWITCH RELEASE MECHANISM EMERGENCY ESC
- [SDR USAA2009022090397](https://openairdocs.org/sdr/USAA2009022090397), Feb 6, 2009: SPLICE. CORRODED. SAL - C8 - MAJOR REPAIR - CORROSION ON SPLICE COUPLING AT FR64, Y765. REPLACED SPLICE COUPLING AT FR64, Y765 IAW A320 SRM 51-72-11.
- [SDR USAA2009021390337](https://openairdocs.org/sdr/USAA2009021390337), Feb 6, 2009: SILL. CORRODED. SAL C8 MAJOR REPAIR NR 6180803. GALVANIC CORROSION ON LOWER SILL AT BULK CARGO DOOR FR60 TO FR62. REPAIRED LOWER SILL AT BULK CARGO DOOR FR60 TO FR62 IAW A320 S
- [SDR USAA2009022390420](https://openairdocs.org/sdr/USAA2009022390420), Feb 4, 2009: SILL. CORRODED. SAL - C8 - MAJOR REPAIR - CORROSION ON R2 LOWER DOOR SILL AT FR67 +17 INCHES, -Y1460. REPAIRED R2 LOWER DOOR SILL AT FR67 +17 INCHES, -Y1460 IAW A320 SRM 53-41-
- [SDR USAA2009020690294](https://openairdocs.org/sdr/USAA2009020690294), Feb 2, 2009: SEAT TRACK. CORRODED. SAL - C8 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46 +17 INCHES, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46 +17 INCHES, -Y1292 IAW A320 
- [SDR USAA2009021690348](https://openairdocs.org/sdr/USAA2009021690348), Feb 1, 2009: SEAT TRACK. CORRODED. SAL - C8 - MAJOR REPAIR - NR 6171206 - CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A320 SRM 51-72-1
- [SDR USAA2009022390421](https://openairdocs.org/sdr/USAA2009022390421), Jan 31, 2009: SEAT TRACK. CORRODED. SAL - C8 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, Y1292 IAW A320 SRM 51-72-11.
- [SDR USAA2009021990385](https://openairdocs.org/sdr/USAA2009021990385), Jan 29, 2009: FITTING. CORRODED. SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FORWARD CORNER FITTING OF L1 DOOR AT FR16, Y1853. REPLACED FORWARD CORNER FITTING OF L1 DOOR AT FR16, Y1853 IAW 
- [SDR USAA2009022090392](https://openairdocs.org/sdr/USAA2009022090392), Jan 28, 2009: SHEAR PLATE. CORRODED. SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1360. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1360 IAW A320 SRM 51-72-1
- [SDR USAA2009021890369](https://openairdocs.org/sdr/USAA2009021890369), Jan 28, 2009: FLOOR SUPPORT. CORRODED. SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR16 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR16 TO FR24, -Y254 IAW A320 SRM 51-72
- [SDR USAA2009021390338](https://openairdocs.org/sdr/USAA2009021390338), Jan 28, 2009: SILL. CORRODED. SAL C8 MAJOR REPAIR NR 6171575 GALVANIC CORROSION ON R2 DOOR LOWER SILL AT FR68, -Y1732. REPAIRED R2 DOOR LOWER SILL AT FR68, -Y1732 IAW A320 SRM 53-41-14.
- [SDR USAA2009021290323](https://openairdocs.org/sdr/USAA2009021290323), Jan 28, 2009: FLOORBEAM. CORRODED. SAL - C8 MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR69, -Y1262. REPAIRED BEAM BETWEEN FR67 TO FR69, -Y1262 IAW A320 SRM 51-72-11.
- [SDR USAA2009021290322](https://openairdocs.org/sdr/USAA2009021290322), Jan 28, 2009: FLOORBEAM. CORRODED. SAL - C8 MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, Y765 IAW A320 S
- [SDR USAA2009022390419](https://openairdocs.org/sdr/USAA2009022390419), Jan 27, 2009: SILL. CORRODED. SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON BULK CARGO LOWER DOOR SILL BETWEEN FR60 TO FR62. REPAIRED BULK CARGO LOWER DOOR SILL BETWEEN FR60 TO FR62 IAW A3
- [SDR USAA2009022090390](https://openairdocs.org/sdr/USAA2009022090390), Jan 26, 2009: BEARING. EXCESS PLAY. SAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BEARING NR 3 VERTICAL STABILIZER. REPLACED ATTACH FITTING HINGE ARM BEARING NR 3 OF VERTICAL STABIL
- [SDR USAA2009022090389](https://openairdocs.org/sdr/USAA2009022090389), Jan 26, 2009: BEARING. EXCESS PLAY. SAL - C8 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM BEARING NR 5 VERTICAL STABILIZER. REPLACED ATTACH FITTING HINGE ARM BEARING NR 5 OF VERTICAL STABIL
- [SDR USAA2009021990386](https://openairdocs.org/sdr/USAA2009021990386), Jan 26, 2009: SEAT TRACK. CORRODED. SAL - C8 - MAJOR REPAIR - CORROSION ON SEAT TRACK RAIL BETWEEN FR46 +17 INCHES TO FR64, -Y765. REPLACED SEAT TRACK RAIL BETWEEN FR46 +17 INCHES TO FR64, -Y765 I

All 138: https://openairdocs.org/deregistered/N648AW-2017-04-13/reports.md

## Other aircraft with N648AW

- [Registered now](https://openairdocs.org/aircraft/N648AW): DJI AGRAS T100, S/N 1581F8ZLC258N0027866

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.