# N622AW: 1989 Airbus Industrie A320-231, registration cancelled 2015-10-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 28, 2015
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (registry code 3930325)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 054
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 1989
- Certificate issued: June 19, 2015
- Last registry action: September 23, 2015
- Mode S code: A81DC0
- Owner when cancelled: [Global Aircraft Support Group LLC](https://openairdocs.org/faa-owner/GLOBAL%20AIRCRAFT%20SUPPORT%20GROUP%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N622AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=622AW
- Page: https://openairdocs.org/deregistered/N622AW-2015-10-28

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 A320-231: https://openairdocs.org/model/airbus-industrie-a320-231.md

## Service difficulty reports (277, newest 50)

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

- [SDR USAA2014090200027](https://openairdocs.org/sdr/USAA2014090200027), Aug 30, 2014: SLIDE RAFT. UNSERVICEABLE. THE PAX ENTRY DOOR L1 GUST LOCK STICKS. FOUND THE SLIDE RAFT HAD EXPANDED CAUSING SLIDE COVER TO COME IN CONTACT WITH FUSELAGE WITH DOOR OPEN. R & R L1 DOOR SLI
- [SDR USAA2014072800009](https://openairdocs.org/sdr/USAA2014072800009), Jul 25, 2014: LENS. MISSING. EMERGENCY LIGHT LENS MISSING AT SEAT 24C. INSTALLED EMER LIGHT LENS AT SEAT 24C.
- [SDR USAA2014042400004](https://openairdocs.org/sdr/USAA2014042400004), Apr 23, 2014: PUMP. INOPERATIVE. RETURN TO FIELD FOR BLUE HYD SYS OVERHEAT MULTIPLE TIMES, 8, SHUT OFF BLUE HYD PUMP IAW ECAM. REPLACED BLUE HYD PUMP 2075GJ & CASE DRAIN FILTER 2084GM IAW AMM 2
- [SDR USAA2014042100007](https://openairdocs.org/sdr/USAA2014042100007), Apr 17, 2014: LENS. MISSING. SEAT 1R MISSING EMERGENCY EXIT LIGHT LENS. REPLACED EMERGENCY EXIT LIGHT LENS AT SEAT 1R.
- [SDR USAA2014041700013](https://openairdocs.org/sdr/USAA2014041700013), Apr 17, 2014: RAM AIR TURB. DEPLOYED. RAT OUT ECAM MSG AFTER TAKEOFF. FOUND RAT DEPLOYED ON ARRIVAL INTO PHX. PERFORMED JOB CARD 26T21029003. NO DISCREPANCIES NOTED, PERFORMED SEVERAL EXTENSIONS.
- [SDR USAA2014041400007](https://openairdocs.org/sdr/USAA2014041400007), Apr 13, 2014: LIGHT. LOOSE. EMERGENCY EXIT LIGHT AT ROW 5 LT IS LOOSE. SECURED EMERGENCY EXIT LIGHT AT ROW 5 LT.
- [SDR USAA2014040700019](https://openairdocs.org/sdr/USAA2014040700019), Apr 6, 2014: LENS. DETACHED. EXIT LIGHT COVER AT DOOR 2L FELL OFF. INSTALLED EXIT LIGHT COVER AT DOOR 2L.
- [SDR USAA2014031400015](https://openairdocs.org/sdr/USAA2014031400015), Mar 11, 2014: LIGHT. MALFUNCTIONED. CAPTAIN`S MAP LIGHT STARTED ELEC ARCING & SMOKING INFLIGHT. REPLACED CAPTAIN`S READING MAP LIGHT IAW AMM 33-12-12-0401.
- [SDR USAA2014012700008](https://openairdocs.org/sdr/USAA2014012700008), Jan 26, 2014: MECHANISM. OUT OF ADJUST. RIGHT FWD OVERWING EMERGENCY EXIT ECAM ARMING MESSAGE DURING CRUISE. ADJUSTED LATCH MECHANISM OF RT FWD OVERWING EMERGENCY EXIT.
- [SDR USAA2014012700009](https://openairdocs.org/sdr/USAA2014012700009), Jan 24, 2014: LENS. MISSING. EMERGENCY EXIT LIGHT LENS MISSING AT SEAT 9D. INSTALLED EMERGENCY EXIT LIGHT LENS AT SEAT 9D.
- [SDR USAA2014010600022](https://openairdocs.org/sdr/USAA2014010600022), Jan 4, 2014: LENS. MISSING. SEAT MOUNTED EMERGENCY LIGHT LENS MISSING AT ROW 19 LT. INSTALLED SEAT MOUNTED EMERGENCY LIGHT LENS AT ROW 19 LT.
- [SDR USAA2013122600006](https://openairdocs.org/sdr/USAA2013122600006), Dec 25, 2013: LENS. MISSING. SEAT 9C MISSING EMERGENCY LIGHT LENS. INSTALLED NEW LENS ON EMERGENCY LIGHT AT 9C IAW A320 CMM 25-25-01.
- [SDR USAA2013120900017](https://openairdocs.org/sdr/USAA2013120900017), Dec 2, 2013: SKIN. SATURATED. C2 CHECK, AREA OF WATER INGRESS ON UPPER SURFACE OF RT ELEVATOR AT APPROXIMATELY 17 INCHES FWD OF TE & 1.13 INCHES FROM INBD EDGE. REPAIRED RT ELEVATOR UPPER SU
- [SDR USAA2013100100003](https://openairdocs.org/sdr/USAA2013100100003), Oct 1, 2013: FLOOR PANEL. DELAMINATED. FLOOR PANEL SOFT AT CENTER AISLE ROW 8 AREA BETWEEN FRAMES 32 - 35 & BETWEEN S23L TO S23R, BL 0. REPLACED FLOOR PANEL IAW AMM 53-12-12.
- [SDR USAA2013090300022](https://openairdocs.org/sdr/USAA2013090300022), Aug 31, 2013: LENS. MISSING. RED EXIT ROW EMERGENCY LIGHT LENS IS MISSING FROM LIGHT AT 9L. INSTALLED RED LENS TO EMERGENCY LIGHT AT EXIT ROW 9L.
- [SDR USAA2013082300012](https://openairdocs.org/sdr/USAA2013082300012), Aug 22, 2013: FLOOR PANEL. DELAMINATED. DELAMINATION ON FLOOR PANEL BETWEEN FRAMES 64 TO 66 & S21L TO S21R. REPLACED FLOOR PANEL IAW AMM 53-42-12-400-002-A.
- [SDR USAA2013082300011](https://openairdocs.org/sdr/USAA2013082300011), Aug 22, 2013: FLOOR PANEL. DELAMINATED. FOUND DELAMINATION ON FLOOR PANEL 251WF BETWEEN FRAMES 62 TO 64 & S21L TO S21R. REPLACED FLOOR PANEL IAW AMM 53-42-12-400-001-A.
- [SDR USAA2013081300006](https://openairdocs.org/sdr/USAA2013081300006), Aug 12, 2013: SLIDE. BULGED. L1 DOOR GUST LOCK, HARD TO LATCH AND UNLATCH. FOUND SLIDE RAFT BULGING CAUSING GUST LOCK NOT TO ENGAGE. R & R L1 SLIDE IAW TASK CARD 26L00025011.
- [SDR USAA2013070800034](https://openairdocs.org/sdr/USAA2013070800034), Jul 6, 2013: TRU. INOPERATIVE. THE COCKPIT CREW DETECTED SMOKE IN THE COCKPIT DURING CRUISE ALTITUDE. MX REPLACED THE NR ONE TRANSFORMER RECTIFIER.
- [SDR USAA2013070500012](https://openairdocs.org/sdr/USAA2013070500012), Jul 3, 2013: SKIN PANEL. DELAMINATED. RUDDER LT SKIN PANEL DELAMINATED 15" FROM TIP AND 8" FWD OF T/E. R & R RUDDER IAW AMM 27-21-41.
- [SDR USAA2013062700009](https://openairdocs.org/sdr/USAA2013062700009), Jun 25, 2013: SLIDE RAFT. UNSECURE. LEFT REAR PAX DOOR SLIDE MECHANISM CAME OFF OF DOOR. REPLACED L2 DOOR SLIDE RAFT.
- [SDR USAA2013051300003](https://openairdocs.org/sdr/USAA2013051300003), May 11, 2013: WIRE HARNESS. DISCONNECTED. EMERGENCY LIGHT 7A INOPERATIVE. RECONNECTED LOOSE WIRE.
- [SDR USAA2013050600007](https://openairdocs.org/sdr/USAA2013050600007), May 4, 2013: GUST LOCK. LACK OF LUBE. GUST LOCK ON DOOR 1L DIFFICULT TO OPERATE. LUBRICATED L-1 GUST LOCK.
- [SDR USAA2013031400013](https://openairdocs.org/sdr/USAA2013031400013), Mar 13, 2013: FLASHLIGHT. INOPERATIVE. EMERGENCY FLASHLIGHT AT JUMP SEAT 1L DOES NOT FLASH. REPLACED FLASHLIGHT AS REQUIRED.
- [SDR USAA2013021900003](https://openairdocs.org/sdr/USAA2013021900003), Feb 17, 2013: WIRE. BROKEN. EMERGENCY LIGHT ON SEAT ROW 26 LEFT INOP (WIRE BROKEN). REPAIRED WIRE PER ELECTRICAL STANDARD PRACTICE MANUAL 20-43-12, ELECTRICAL STANDARD PRACTICE MANUAL 20-4
- [SDR USAA2013021300026](https://openairdocs.org/sdr/USAA2013021300026), Feb 11, 2013: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT BY 2R DOOR INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT LENS COVER NEAR 2R DOOR.
- [SDR USAA2012122400016](https://openairdocs.org/sdr/USAA2012122400016), Dec 22, 2012: BRACKET. LOOSE. EMERGENCY FLOOR LIGHTING SEAT 17C BROKEN. RE-SECURED EMERGENCY FLOOR LIGHT BRACKET. OPS CHECKED GOOD.
- [SDR USAA2012120700009](https://openairdocs.org/sdr/USAA2012120700009), Dec 5, 2012: BOTTLE. LOW PRESSURE. L2 DOOR ASSIST BOTTLE CHARGE IS LOW. SERVICED L2 DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001-A.
- [SDR USAA2012070500025](https://openairdocs.org/sdr/USAA2012070500025), Jul 2, 2012: CYLINDER. LOW PRESSURE. L2 DOOR ASSIST NEEDS SERVICING. SERVICED L2 DOOR TO PROPER PRESSURE. OPS CHECKED GOOD.
- [SDR USAA2012051100001](https://openairdocs.org/sdr/USAA2012051100001), May 10, 2012: LIGHT. BROKEN. C1 CHECK - BROKEN EMERGENCY EGRESS LIGHTS BROKEN AT ROW 17ABC & 11FED. RE-SECURED EMERGENCY LIGHT ASSEMBLY AT ROW 17ABC & 11FED IAW A320 AMM 33-51-19.
- [SDR USAA2012051000021](https://openairdocs.org/sdr/USAA2012051000021), May 9, 2012: ANGLE. CRACKED. BC1 CHECK - 5 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON FORWARD LEFT EMERGENCY EXIT DOOR 833. REPLACED SEGMENT ANGLE ON FORWARD LEFT EMERGENCY EXI
- [SDR USAA2012051000020](https://openairdocs.org/sdr/USAA2012051000020), May 9, 2012: ANGLE. CRACKED. BC1 CHECK - 10 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON AFT RIGHT EMERGENCY EXIT DOOR 844. REPLACED SEGMENT ANGLE ON AFT RIGHT EMERGENCY EXIT DOO
- [SDR USAA2012050800019](https://openairdocs.org/sdr/USAA2012050800019), May 7, 2012: DAMPER. LEAKING. C1 CHECK - LEFT AFT ENTRY L2 DOOR EMERGENCY ASSIST ACTUATOR BOTTLE BLEED DOWN AFTER CHARGE AND DOOR OPENS SLOWLY. REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM
- [SDR USAA2012051100002](https://openairdocs.org/sdr/USAA2012051100002), May 2, 2012: HINGE PIN. BENT. BC1 CHECK - NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN IS BENT. REPLACED NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN IAW JOB CARD 26C71032003.
- [SDR USAA2012032800004](https://openairdocs.org/sdr/USAA2012032800004), Mar 27, 2012: LENS. MISSING. EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 9R. INSTALLED EMERGENCY AISLE LIGHT LENS AT ROW 9R.
- [SDR USAA2012031600006](https://openairdocs.org/sdr/USAA2012031600006), Mar 15, 2012: COMPUTER. FAILED. CREW RECEIVED ECAM MESSAGE FOR AVIONICS SMOKE AFTER LANDING WITH SMOKE IN GEN LINE 1 SWITCH. CAPTAIN REQUESTED PRIORITY TAXI AND FIRE TRUCK. MAINTENANCE MET AIR
- [SDR USAA2012030100008](https://openairdocs.org/sdr/USAA2012030100008), Feb 29, 2012: CONNECTOR. LOOSE. SEAT MOUNTED EMERGENCY LIGHT AT ROW 11 RIGHT INOPERATIVE. SECURED WALL CONNECTOR AT ROW 12 - SYSTEM OPERATIONAL CHECK GOOD.
- [SDR USAA2012012400019](https://openairdocs.org/sdr/USAA2012012400019), Jan 22, 2012: BATTERY. DISCHARGED. RT EMERGENCY EXIT LIGHT POWER SUPPLY UNIT BATTERY FAULTS. REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-
- [SDR USAA2011112800018](https://openairdocs.org/sdr/USAA2011112800018), Nov 27, 2011: BOTTLE. LOW PRESSURE. DOOR L2 OPEN ASSIST BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.
- [SDR USAA2011090600028](https://openairdocs.org/sdr/USAA2011090600028), Sep 2, 2011: PUMP. DEFECTIVE. CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INS
- [SDR USAA2011090600025](https://openairdocs.org/sdr/USAA2011090600025), Sep 2, 2011: PRESSURE SWITCH. DEFECTIVE. CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INS
- [SDR USAA2011080900006](https://openairdocs.org/sdr/USAA2011080900006), Aug 5, 2011: PUMP. LEAKING. DURING DESCENT, PACKS STILL EMITTING DIRTY SOCK, FOUL ODOR. FOUND HYDRAULIC FLUID FROM BLUE ELECTRIC PUMP CONTAMINATING ENVIRONMENTAL SYSTEM. REMOVED AND REPLAC
- [SDR USAA2011053100014](https://openairdocs.org/sdr/USAA2011053100014), May 29, 2011: LIGHT. LOOSE. PHX - EEL - EMERGENCY PATH LIGHT LOOSE A/C LEFT FORWARD BULKHEAD PANEL. REMOVED AND REPLACED LIGHT ASSEMBLY.
- [SDR USAA2011031491044](https://openairdocs.org/sdr/USAA2011031491044), Mar 10, 2011: ACTUATOR. STALLED. FLT 88 - CREW REPORTED NR 1 ENGINE COMPRESSOR STALL ON CLIMB WITH MAX EGT 720+ FOR ONE MINUTE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MA
- [SDR USAA2011022590860](https://openairdocs.org/sdr/USAA2011022590860), Feb 24, 2011: CYLINDER. LOW PRESSURE. FLT 77 - SEA - EES - R-2 DOOR ASSIST CYLINDER PRESSURE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.
- [SDR USAA2011012590325](https://openairdocs.org/sdr/USAA2011012590325), Jan 24, 2011: BOTTLE. LOW PRESSURE. FLT 77 - SEA - EES - L-2 DOOR ASSIST BOTTLE CHARGE IS LOW. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.
- [SDR USAA2011012590324](https://openairdocs.org/sdr/USAA2011012590324), Jan 24, 2011: BOTTLE. LOW PRESSURE. FLT 77 - SEA - EES - R-2 DOOR ASSIST BOTTLE CHARGE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.
- [SDR USAA2010120992935](https://openairdocs.org/sdr/USAA2010120992935), Dec 8, 2010: CYLINDER. LOW PRESSURE. FLT 94 - PHX - EES - R-2 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE TO PROPER PRESSURE.
- [SDR USAA2010100792211](https://openairdocs.org/sdr/USAA2010100792211), Oct 5, 2010: DOOR FRAME. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON FORWARD & AFT TRANSMITTING PROFILE OF FORWARD RIGHT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AT BEAM 2. REPAIRED FORWARD & AFT
- [SDR USAA2010100792210](https://openairdocs.org/sdr/USAA2010100792210), Oct 5, 2010: DOOR FRAME. CRACKED. SAL - S5 - MAJOR REPAIR - CRACK ON AFT TRANSMITTING PROFILE OF AFT LEFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE. REPAIRED AFT TRANSMITTING PROFILE OF AFT LEFT EM

All 277: https://openairdocs.org/deregistered/N622AW-2015-10-28/reports.md

## Other aircraft with N622AW

- [Registered now](https://openairdocs.org/aircraft/N622AW): Air Tractor AT-602, S/N 602-1343, built 2022

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