# N602AW: 1996 Airbus Industrie A320-232, registration cancelled 2016-04-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 21, 2016
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-232](https://openairdocs.org/model/airbus-industrie-a320-232) (registry code 3930326)
- Engine: [IAE V2527-A5](https://openairdocs.org/engine/iae-v2527-a5) (registry code 34604)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM), [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Serial number: 565
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard
- Airworthiness date: May 5, 2009
- Certificate issued: February 20, 2013
- Last registry action: October 30, 2015
- Mode S code: A7CEC2
- Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N602AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=602AW
- Page: https://openairdocs.org/deregistered/N602AW-2016-04-21

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 (192, newest 50)

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

- [SDR AALA201512219004](https://openairdocs.org/sdr/AALA201512219004), Dec 20, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT WAS GNDED. DURING TAKEOFF, TAKEOFF INHIBITED, TURNED RED. TAKEOFF ABORTED AT APPROX 70 KTS. ACCOMPLISHED A GROUND SCAN OF CENTRAL WARNING SYS & FWC SYS
- [SDR AALA201510119003](https://openairdocs.org/sdr/AALA201510119003), Oct 10, 2015: LENS. MISSING. LENS COVER MISSING FROM EMER LIGHT ON L2 DOOR. INSTALLED LENS COVER AS REQUIRED.
- [SDR AALA201509049001](https://openairdocs.org/sdr/AALA201509049001), Sep 3, 2015: BATTERY. DISCHARGED. FORWARD FLIGHT ATTENDANT FLASHLIGHT, OTBD POSITION, NOT CHARGING. REPLACED BATTERY.
- [SDR AALA201506119003](https://openairdocs.org/sdr/AALA201506119003), Jun 10, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE AT ROW 09 RT. REPLACED THE EMER ESCAPE PATH LIGHT AT SEAT ROW 9 RT.
- [SDR USAA2015010700003](https://openairdocs.org/sdr/USAA2015010700003), Jan 6, 2015: BATTERY PACK. DISCHARGED. EXIT SIGN OVER RT PLUG DOORS AT SEAT ROWS 10 & 11 INOPERATIVE. REPLACED BATTERY PACKS AT FLOOR LEVEL ROW 10L & 11R. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.
- [SDR USAA2015010700002](https://openairdocs.org/sdr/USAA2015010700002), Jan 6, 2015: LENS. MISSING. SEAT 1C SEAT EMER LIGHT LENS MISSING. REPLACED 1C EMER LIGHT LENS. OK FOR SERVICE.
- [SDR USAA2015010200006](https://openairdocs.org/sdr/USAA2015010200006), Dec 31, 2014: HANDLE. OUT OF ADJUST. FLIGHT ATTENDANT UNABLE TO ARM DOOR 2L. ADJUSTED ESCAPE SLIDE HANDLE IAW AMM 52-11-22-820-11 & LUBED CABLE. REMOVED & INSTALLED SLIDE IAW AMM 25-62-44.
- [SDR USAA2014122400006](https://openairdocs.org/sdr/USAA2014122400006), Dec 22, 2014: RIB. CRACKED. NUMBER 1 ENG PYLON RIB 4 IS CRACKED ON INNER & OUTER SIDE OF RADIUS AT LOWER END. REMOVED, WELDED & REINSTALLED PYLON RIB NR 4 IAW SRM 51-42-11 & 54-30-00-101.
- [SDR USAA2014121500009](https://openairdocs.org/sdr/USAA2014121500009), Dec 14, 2014: SIGN. NOT SEATED. EXIT SIGN IS BURNT OUT. RESEATED EXIT SIGN 1L DOOR OPERATIONS NORMAL.
- [SDR USAA2014092200004](https://openairdocs.org/sdr/USAA2014092200004), Sep 20, 2014: LENS. MISSING. EMERGENCY LIGHT LENS COVER MISSING FROM SEAT ROW 7 LT. INSTALLED EMER LIGHT LENS AT SEAT ROW 7 LT.
- [SDR USAA2014082700001](https://openairdocs.org/sdr/USAA2014082700001), Aug 26, 2014: WARNING SYSTEM. FALSE ACTIVATION. EN ROUTE CREW RECEIVED STATUS MSG INOP SYS. REVERSER 1 ENG 1 THRUST, FLIGHT DIVERTED. FOUND NO FAULTS ON PFR OR MSG. PERFORMED OPERATIONAL TEST OF NR 1 ENG THRU
- [SDR USAA2014081900003](https://openairdocs.org/sdr/USAA2014081900003), Aug 18, 2014: WARNING SYSTEM. FALSE ACTIVATION. IN CRUISE FLIGHT AT FL 350 STATUS MSG APPEARED. WHEN SLATS OUT ENG 1 AT IDLE ON GND ENG 1 MAX PWR, IDLE " $ INOP SYS REVERSER NR 1 ENG 1 THRUST. PERFORMED BITE 
- [SDR USAA2014080100009](https://openairdocs.org/sdr/USAA2014080100009), Jul 31, 2014: BATTERY. DISCHARGED. AFT EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN AFT EMER FLASHLIGHT.
- [SDR USAA2014032400018](https://openairdocs.org/sdr/USAA2014032400018), Mar 21, 2014: LENS. MISSING. SEAT MOUNTED EMERGENCY EXIT LIGHT MISSING LENS AT ROW 9 LT. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT LENS AT ROW 9 LT.
- [SDR USAA2014022400005](https://openairdocs.org/sdr/USAA2014022400005), Feb 23, 2014: MEGAPHONE. DAMAGED. AFT MEGA PHONE DAMAGED. REPLACED AFT MEGA PHONE, OPERATIONS CHECKED GOOD.
- [SDR USAA2014013000007](https://openairdocs.org/sdr/USAA2014013000007), Jan 29, 2014: LENS. LOOSE. EXIT SIGN LENS AT DOOR 2R BY FLOOR HAS COVER LOOSE. REPLACED EXIT SIGN LENS AT DOOR 2R.
- [SDR USAA2013121600014](https://openairdocs.org/sdr/USAA2013121600014), Dec 13, 2013: PRESSURE SWITCH. INOPERATIVE. SHORTLY AFTER TAKEOFF GOT GREEN HYD ENG 1 PUMP FAULT. REPLACED NR 1 ENG HYD PUMP PRESS SWITCH IAW A320 AMM 29-11-17.
- [SDR USAA2013103100003](https://openairdocs.org/sdr/USAA2013103100003), Oct 30, 2013: LIGHT. UNSECURE. CREW REPORTED THE EMERGENCY LIGHT IN REAR GALLEY BROKEN. MAINTENANCE SECURED REAR GALLEY EMERGENCY LIGHT.
- [SDR USAA2013103000004](https://openairdocs.org/sdr/USAA2013103000004), Oct 29, 2013: BRACKET. UNSECURE. CREW REPORTED SEAT 9D FLOOR LIGHT DANGLING. MX SECURED SEAT MOUNTED EXIT LIGHT BRACKET ON SEAT 9D. OPS CHECKED GOOD IAW CMM 25-27-35.
- [SDR USAA2013091300006](https://openairdocs.org/sdr/USAA2013091300006), Sep 11, 2013: BATTERY PACK. INOPERATIVE. LEFT FORWARD EMERGENCY LIGHT FAILED TEST. R & R LT FORWARD EMERGENCY BATTERY.
- [SDR USAA2013081900003](https://openairdocs.org/sdr/USAA2013081900003), Aug 16, 2013: LENS. BROKEN. R2 DOOR EXIT LIGHT LENS BROKEN. INSTALLED NEW EXIT LIGHT LENS AT R2 DOOR.
- [SDR USAA2013072900008](https://openairdocs.org/sdr/USAA2013072900008), Jul 25, 2013: LENS. MISSING. L2 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED L2 DOOR EMERGENCY LIGHT LENS.
- [SDR USAA2013071800001](https://openairdocs.org/sdr/USAA2013071800001), Jul 17, 2013: WIRE HARNESS. FAULTY. MX REPORTED THE EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. MX REPLACED EMERGENCY LIGHT HARNESS AT SEAT 26L. OPS CHECKED GOOD. IAW ESPM 20-33-22.
- [SDR USAA2013060700009](https://openairdocs.org/sdr/USAA2013060700009), Jun 6, 2013: LENS. BROKEN. EXIT ROW LIGHT BROKE OFF AT 1C. REPLACED LENS AT 1C EMERGENCY LIGHT.
- [SDR USAA2013042900007](https://openairdocs.org/sdr/USAA2013042900007), Apr 27, 2013: WIRE HARNESS. DAMAGED. SEAT ROW 22L EMERGENCY CONNECTOR PLUG PULLED OUT FROM SPLICES. REMOVED AND REPLACED SEAT HARNESS.
- [SDR USAA2013031800009](https://openairdocs.org/sdr/USAA2013031800009), Mar 15, 2013: LENS. MISSING. RIGHT REAR EXIT DOOR EMERGENCY LIGHT CASING MISSING. REPLACED MISSING LENS AT RIGHT REAR DOOR.
- [SDR USAA2013012800014](https://openairdocs.org/sdr/USAA2013012800014), Jan 25, 2013: LENS. MISSING. EXIT LIGHT COVER 2L DOOR MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS COVER AT DOOR 2L.
- [SDR USAA2012101900003](https://openairdocs.org/sdr/USAA2012101900003), Oct 18, 2012: BATTERY. DISCHARGED. AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY NEEDS REPLACING. REPLACED AFT F/A FLASHLIGHT BATTERY - OPERATIONAL CHECK NORMAL.
- [SDR USAA2012091000044](https://openairdocs.org/sdr/USAA2012091000044), Sep 9, 2012: WIRE. DISCONNECTED. EMERGENCY EXIT LIGHT AT ROW 10 RIGHT IS INOPERATIVE. FOUND WIRE DISCONNECTED FROM LIGHT. RECONNECTED TERMINAL FITTING TO LIGHT. OPS CHECKED GOOD.
- [SDR USAA2012071700004](https://openairdocs.org/sdr/USAA2012071700004), Jul 15, 2012: LIGHT. MISSING. OVERWING EMERGENCY EXIT LIGHT MISSING ROW 10 AIRCRAFT RIGHT LOWER SIDE PANEL. RE-INSTALLED EMERGENCY LIGHT ASSEMBLY AND APPLIED TAPE TO DAMAGED AREA OF PANEL. E
- [SDR USAA2012070200020](https://openairdocs.org/sdr/USAA2012070200020), Jun 29, 2012: ATTACH FITTING. CORRODED. 3S CHECK - CORROSION ON FORWARD LUG OF RIGHT WING BOX MAIN LANDING GEAR ATTACHMENT FITTING RIB 5 GEAR SUPPORT WS 2508. REPAIRED FORWARD LUG OF RIGHT WING BOX MA
- [SDR USAA2012062600006](https://openairdocs.org/sdr/USAA2012062600006), Jun 25, 2012: DOOR. OUT OF ADJUST. 3S CHECK - OUT OF ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER AND FINGER AT PASSENGER DOOR 842 (R2). PERFORMED ADJUSTMENT OF DIMENSION "A" BETWEEN STRIKER LE
- [SDR USAA2012062100004](https://openairdocs.org/sdr/USAA2012062100004), Jun 20, 2012: SLIDE. BULGED. 3S CHECK - DURING A DVI OF THE LEFT OFF WING SLIDE ENCLOSURE DOOR FOUND IT NOT FLUSH WITH THE OUTER SURFACE OF THE LEFT OFF WING SLIDE ENCLOSURE. REPACKED LEFT 
- [SDR USAA2012062800007](https://openairdocs.org/sdr/USAA2012062800007), Jun 11, 2012: DOOR FRAME. CORRODED. 3S CHECK - CORROSION ON FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (834) AT FR40. REPLACED FORWARD CURVE EDGE OF THE LEFT AFT EMERGENCY EXIT DOOR (8
- [SDR USAA2012062600011](https://openairdocs.org/sdr/USAA2012062600011), Jun 11, 2012: DOOR FRAME. CORRODED. 3S CHECK - CORROSION ON CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) AT FR39, BEAM 4. REPLACED CURVED EDGE OF LEFT FORWARD EMERGENCY EXIT HATCH (833) 
- [SDR USAA2012062100022](https://openairdocs.org/sdr/USAA2012062100022), Jun 9, 2012: FITTING. CORRODED. 3S CHECK - CORROSION ON RIGHT PYLON SPIGOT FITTING BETWEEN PYLON STA 4697 TO STA 4954, & BETWEEN RIB 5 TO RIB 4. REPLACED RIGHT PYLON SPIGOT FITTING IAW A320 SR
- [SDR USAA2012061200002](https://openairdocs.org/sdr/USAA2012061200002), Jun 2, 2012: FLOOR PANEL. DELAMINATED. 3S CHECK - DELAMINATION ON FLOOR PANEL 232PF BETWEEN FR24 TO FR28, BETWEEN Y-1732 TO Y-1292. REPLACED FLOOR PANEL 232PF IAW A320 SRM 53-02-00, TABLE 103 AND IRM
- [SDR USAA2012062100021](https://openairdocs.org/sdr/USAA2012062100021), Jun 1, 2012: SHEAR PLATE. CORRODED. 3S CHECK - CORROSION ON SHEAR PLATE ASSEMBLY BETWEEN FR58 TO FR59, S38R. REPLACED SHEAR PLATE ASSEMBLY BETWEEN FR58 TO FR59, S38R IAW A320 SRM 51-72-11AND DRAWI
- [SDR USAA2012061200010](https://openairdocs.org/sdr/USAA2012061200010), Jun 1, 2012: COUPLING. ELONGATED. 3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR 23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D534742
- [SDR USAA2012061200009](https://openairdocs.org/sdr/USAA2012061200009), Jun 1, 2012: COUPLING. ELONGATED. 3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR 23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D534742
- [SDR USAA2012061200008](https://openairdocs.org/sdr/USAA2012061200008), Jun 1, 2012: COUPLING. ELONGATED. 3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D5347425
- [SDR USAA2012061200006](https://openairdocs.org/sdr/USAA2012061200006), Jun 1, 2012: COUPLING. ELONGATED. 3S CHECK - ELONGATED HOLE ON FRAME COUPLING AT FR66, STR23R, -Y1732. REPLACED FRAME COUPLING AT FR66, STR 23R, -Y1732 IAW A320 SRM 51-72-11 AND DRAWING D5347425
- [SDR USAA2012060800012](https://openairdocs.org/sdr/USAA2012060800012), Jun 1, 2012: WEB. CRACKED. 3S CHECK - CRACK IN WEB BETWEEN FR8 TO FR11, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110285.
- [SDR USAA2012070300007](https://openairdocs.org/sdr/USAA2012070300007), May 31, 2012: SILL. CORRODED. 3S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LOWER DOOR SILL OF BULK CARGO COMPARTMENT AT FR 61+19 INCHES, S38R. REPLACED LOWER DOOR SILL OF BULK CARGO COMPART
- [SDR USAA2012070200019](https://openairdocs.org/sdr/USAA2012070200019), May 31, 2012: DOOR FRAME. CRACKED. 3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EX
- [SDR USAA2012070200018](https://openairdocs.org/sdr/USAA2012070200018), May 31, 2012: DOOR FRAME. CRACKED. 3S CHECK - CRACK ON INNER FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT OF EMERGENCY EX
- [SDR USAA2012070200017](https://openairdocs.org/sdr/USAA2012070200017), May 31, 2012: WEB. CORRODED. 3S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR65 TO FR66, S23L. REPLACED WEB BETWEEN FR65 TO FR66, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5344742
- [SDR USAA2012070200016](https://openairdocs.org/sdr/USAA2012070200016), May 31, 2012: WEB. CORRODED. 3S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR65 TO FR66, S23R. REPLACED WEB BETWEEN FR65 TO FR66, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5348050
- [SDR USAA2012062900015](https://openairdocs.org/sdr/USAA2012062900015), May 31, 2012: ANGLE. CORRODED. 3S CHECK - CORROSION ON T-SECTION ANGLE OF FORWARD LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 AND EDG
- [SDR USAA2012062900014](https://openairdocs.org/sdr/USAA2012062900014), May 31, 2012: ANGLE. CORRODED. 3S CHECK - CORROSION ON T-SECTION ANGLE OF AFT LOWER VERTICAL FRAME OF LEFT FORWARD EMERGENCY EXIT HATCH (833) BETWEEN FR38 TO FR39 & BETWEEN BEAM 4 & EDGE CURV

All 192: https://openairdocs.org/deregistered/N602AW-2016-04-21/reports.md

## Other aircraft with N602AW

- [Registered now](https://openairdocs.org/aircraft/N602AW): Air Tractor AT-602, S/N 602-1319, built 2021
- [Cancelled 1990-06-15](https://openairdocs.org/deregistered/N602AW-1990-06-15): British Aerospace BAE 146 SERIES 200, S/N E2014. N-number assigned, not yet registered

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