# N460AT: Boeing 737-214, registration cancelled 2000-07-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 6, 2000
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-214](https://openairdocs.org/model/boeing-737-214) (registry code 138446R)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 20158
- Type of aircraft: Fixed wing multi engine
- Certificate issued: April 11, 1998
- Last registry action: June 29, 1998
- Mode S code: A599AD
- Owner when cancelled: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%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/N460AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=460AT
- Page: https://openairdocs.org/deregistered/N460AT-2000-07-06

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 Boeing 737-214: https://openairdocs.org/model/boeing-737-214.md

## Service difficulty reports (88, newest 50)

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

- [SDR AT9900611](https://openairdocs.org/sdr/AT9900611), Aug 27, 1999: CONNECTOR. LOOSE. ONCE IN FLIGHT, EMERGENCY EXIT LIGHTS AND AISLE PATH LIGHTING CAME ON IN FLIGHT WITH SWITCH IN ARMED POSITION. CYCLED AIRCRAFT POWER, TESTED OK. INSPECTED AND F
- [SDR AT9900538](https://openairdocs.org/sdr/AT9900538), Jul 28, 1999: BATTERY PACK. DISCHARGED. R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT (SLIDE) WILL NOT ILLUMINATE. REMOVED AND REPLACED R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT BATTERY PACK IAW B737 MM 33-51-71.
- [SDR AT9900121](https://openairdocs.org/sdr/AT9900121), Jan 21, 1999: SKIN. MISREPAIRED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THREE EXISTING REPAIRS RIGHT FORWARD FUSELAGE AT COCKPIT NOT REPAIRED IAW SB 737-53-111. CUT OUT EXISTING REPAIRS, 
- [SDR AT9900056](https://openairdocs.org/sdr/AT9900056), Jan 20, 1999: SKIN. MISREPAIRED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HORIZONTAL STABILIZER STA 166 SKIN REPAIR HAS NO EDGE DISTANCE ON FILLER. REMOVED EXISTING REPAIR AND FABRICA
- [SDR AT9900039](https://openairdocs.org/sdr/AT9900039), Jan 17, 1999: SKIN. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAINS FWD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SCREW. FABRICATED DOUBLER FROM 2024-T3 .0125 THO
- [SDR AT99000039](https://openairdocs.org/sdr/AT99000039), Jan 17, 1999: SKIN. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAIN'S FORWARD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SCREW. FABRICATED DOUBLER FROM 2024-T3 .012
- [SDR AT9900186](https://openairdocs.org/sdr/AT9900186), Jan 16, 1999: ANGLE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE LAVATORY WALL HAT SECTION AT BS 300 LBL 35-50 HEAVY EXFOLIATION. MECHANICALLY REMOVED CORROSION, REMOVED HAT
- [SDR AT9900124](https://openairdocs.org/sdr/AT9900124), Jan 15, 1999: STRUCTURE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLIGHT DECK FLOOR BULGING AND RIVETS PULLING THROUGH. ALSO, THE NOSE WHEEL WELL AT STA 243, STRINGER 28R FRAME 
- [SDR AT9900122](https://openairdocs.org/sdr/AT9900122), Jan 14, 1999: STRUCTURE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL AREAS CORRODED. THE FORWARD CARGO DOOR FRAME AT STRINGER 25R, INTERCOASTAL FRAME AT STA 500 TO 520 RBL 25 I
- [SDR AT9900040](https://openairdocs.org/sdr/AT9900040), Jan 14, 1999: SKIN. DAMAGED. SCHEDULED INSPECTION AT AERO CORP, FL. STA 847 STR 22R HAS RIPPED SKIN. FABRICATED DOUBLER AND INSTALLED REPAIR IAW B737 SRM'S 53-30-3, 51-30-2, AND AIRTRAN RES
- [SDR AT9900120](https://openairdocs.org/sdr/AT9900120), Jan 11, 1999: DOOR. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT TURBO FAN EXHAUST LOUVER DOOR HAS CORROSION AND PULLING THRU FASTENERS AT STA 685. REMOVED AND REPLACED R
- [SDR AT9900118](https://openairdocs.org/sdr/AT9900118), Jan 11, 1999: SKIN. DAMAGED. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND RIGHT SIDE FUSELAGE SKIN HAS A PREVIOUS .5 BY .75 CUT OUT, WITH FILLER INSTALLED AT FORWARD LOWER CORNER OF FORWARD
- [SDR AT9900185](https://openairdocs.org/sdr/AT9900185), Jan 10, 1999: ANGLE. CORRODED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AND A CRACK ABOVE SIDE WALL AND FLOOR ATTACHMENT AT BS 420-440. MECHANICALLY CLEAN CORROSION, FABRICATED 
- [SDR AT9900123](https://openairdocs.org/sdr/AT9900123), Jan 10, 1999: SEAT TRACK. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT DIFFERENT LOCATIONS. FIRST, THE LAVATORY WALL HAT SECTION AT STA 300 L-35 TO 50, SECONDLY THE SEAT TRA
- [SDR AT9900117](https://openairdocs.org/sdr/AT9900117), Jan 5, 1999: PANEL. DAMAGE. SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PANEL 6403R HAS LEADING EDGE SCREW HOLE DAMAGE FROM WIND EROSION. PANEL HAS 15 PERCENT FLAME SPRAY MISSING. CLEANED
- [SDR AT9900119](https://openairdocs.org/sdr/AT9900119), Jan 4, 1999: STRINGER. CRACKED. SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING UPPER STRINGER NR 13 HAS 3 CRACK AT RIB AT WBL 135.00. REMOVED TEMPORARY REPAIR, FABRICATED NEW REPAIR PA
- [SDR VJ9800381R1](https://openairdocs.org/sdr/VJ9800381R1), Sep 11, 1998: BRAKE. FIRE. NR 3 BRAKE CAUGHT ON FIRE AFTER HIGH SPEED TAXI TEST WAS PERFORMED; TEST COMMENCED AT 100 KNOTS AND AT 80 KNTS LOST PRESSURE AND WENT TO STOP ON RIGHT BRAKES. A
- [SDR VJ9800316](https://openairdocs.org/sdr/VJ9800316), Sep 1, 1998: POWER SUPPLY. INOPERATIVE. RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.
- [SDR VJ0900298](https://openairdocs.org/sdr/VJ0900298), Aug 26, 1998: BATTERY CHARGER. INOPERATIVE. RT OVERWING EMERGENCY LIGHTS INOP. REPLACED THE LIGHT BATTERY CHARGER ASSY.
- [SDR VJ9800296](https://openairdocs.org/sdr/VJ9800296), Aug 23, 1998: BATTERY PACK. DISCHARGED. RT FUSELAGE EXTERNAL OVERWING EMERGENCY LIGHT FOUND INOPERATIVE DURING LAYOVER CHECK. REPLACED BATTERY PACK.
- [SDR VJ9800227](https://openairdocs.org/sdr/VJ9800227), Jul 16, 1998: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTING BATTERY PACK INOP. REPLACED BATTERY PACK.
- [SDR VJ9800198](https://openairdocs.org/sdr/VJ9800198), Jun 19, 1998: GEARBOX. LEAKING. ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND OIL QTY WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. FOUND THAT THE NR 2 ENGINE HAD A BANJO FITTI
- [SDR VJ9800197](https://openairdocs.org/sdr/VJ9800197), Jun 18, 1998: LIGHT. INOPERATIVE. FOUND EMERGENCY EXIT LIGHT INOP AT L-2 DOOR DURING THE LAYOVER CHECK. REPLACED THE LIGHT ASSY.
- [SDR VJ9800009](https://openairdocs.org/sdr/VJ9800009), Feb 9, 1998: SWITCH. FAILED. EMERGENCY EXIT LIGHT WILL NOT ARM, ON FLIGHT CREW PRE FLIGHT. REMOVED AND REPLACED MICRO SWITCH IAW MM 33-51-121; OPS CHECKED GOOD.
- [SDR 98ZZZM160](https://openairdocs.org/sdr/98ZZZM160), Jan 6, 1998: LAMP. MISSING. DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (
- [SDR 98ZZZM159](https://openairdocs.org/sdr/98ZZZM159), Jan 6, 1998: LENS. MISSING. DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMPED AND REPLACED LENS, OPS CHECKED GOOD. (
- [SDR ZZDA5324297](https://openairdocs.org/sdr/ZZDA5324297), Nov 3, 1997: ANGLE. CRACKED. DURING C-CHECK AT AERO CORP, FOUND CRACK AT AFT CARGO COMPARTMENT OF APPROXIMATELY 1 INCH IN STRINGER TO FRAME REINFORCEMENT ANGLE AT STA 907, RIGHT, STR 26 UND
- [SDR ZZDA3325297](https://openairdocs.org/sdr/ZZDA3325297), Oct 31, 1997: LAMP. INOPERATIVE. DURING LAYOVER CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT INOPERABLE, ROW 15. RELAMPED ROW 15 FLOOR TRACK EMERGENCY LAMP IAW MM 33-51-00. OPS CHECK GOOD. (X)
- [SDR ZZDA3325097](https://openairdocs.org/sdr/ZZDA3325097), Oct 31, 1997: POWER SUPPLY. FIRE. RIGHT OVERWING EXTERIOR LIGHT INOPERABLE. INSPECTED POWER SUPPLY ASSY. REMOVED C/P, CHECKED CIRCUIT BOARD. INSTALLED IN RT POWER SUPPLY AND OPS CHECKED GOOD. LT
- [SDR ZZDA5721197](https://openairdocs.org/sdr/ZZDA5721197), Oct 10, 1997: SKIN. DENTED. DURING C-CHECK AT AERO CORP, FOUND RIGHT WING INBOARD FLAP L/E HAS 1.0 INCH BY 2.0 INCH DENT AT WBL 80.0 OUT OF LIMITS. CUT OUT DENT AREA IAW B 737 57-50-4 FIG 
- [SDR ZZDA5322197](https://openairdocs.org/sdr/ZZDA5322197), Sep 30, 1997: SKIN. CORRODED. DURING C-CHECK AT AERO CORP, AT AFT CARGO PIT FROM STA 727B TO STA 767, FOUND CORROSION AROUND NUTPLATES (30 EACH) AT UNDERSIDE OF THE LT TRANSITION PANEL TO BE
- [SDR ZZDA5326897](https://openairdocs.org/sdr/ZZDA5326897), Sep 19, 1997: SKIN. MISDRILLED. DURING C-CHECK AT AERO CORP, FOUND BELLY SKIN HAS DOUBLER DRILLED HOLES AT STA 328 BETWEEN STR 25 - STR 26. FABRICATED DOUBLER FROM 2024 T3 .050 INCH 12 INCHES 
- [SDR ZZDA5327097](https://openairdocs.org/sdr/ZZDA5327097), Sep 14, 1997: SUPPORT. CORRODED. DURING C-CHECK AT AERO CORP, FOUND CABIN BS 344 - BS 380 RBL 15 FLOOR SUPPORT UPPER SURFACE CORRODED BS 350 - BS 354. FABRICATED SUPPORT FROM 7075 T6 .060 INCH 
- [SDR ZZDA5321697](https://openairdocs.org/sdr/ZZDA5321697), Sep 12, 1997: SUPPORT. CORRODED. DURING C-CHECK AT AERO CORP, FOUND FORWARD CABIN CORRODED ON FLOOR SUPPORTS WL 208.1 FROM STA 251.6 TO STA 328 BL AND BL 12R. REMOVED THE CORRODED FLOOR SUPPORT
- [SDR ZZDA5327697](https://openairdocs.org/sdr/ZZDA5327697), Sep 10, 1997: SEAT TRACK. BROKEN OFF. DURING C-CHECK AT AERO CORP, LT INBD SEAT TRACK LUGS AT STATIONS 480-520, AND STATIONS 540-597 ARE BROKEN OFF. FABRICATED SEAT TRACKS FROM BAC 1500-841 44.50 IN
- [SDR ZZDA5322097](https://openairdocs.org/sdr/ZZDA5322097), Sep 9, 1997: SKIN. CRACKED. DURING C-CHECK AT AERO CORP, FOUND 5 EACH FASTENERS WITH CRACK INDICATIONS W/HFEC RT SECTION 41 SKIN. REMOVED COCKPIT SIDE PANELS AND INSULATION FOR ACCESS. REM
- [SDR ZZDA5323197](https://openairdocs.org/sdr/ZZDA5323197), Sep 5, 1997: SEAT TRACK. CORRODED. DURING C-CHECK AT AERO CORP, FOUND OUTBOARD SEAT TRACK HAS CORROSION OUT OF LIMITS FROM BS 360 TO BS 480. REMOVED SEAT TRACK AND REPLACED WITH NEW TRACK (1A-240
- [SDR ZZDA5321997](https://openairdocs.org/sdr/ZZDA5321997), Sep 5, 1997: CHORD. CORRODED. DURING C-CHECK AT AERO CORP, FOUND T-CHORD FROM BS 324 - BS 360 STR 28R CORRODED BEYOND LIMITS. FABRICATED ANGLE REPAIR FROM 301 1/2 CRES STAINLESS STEEL .050 I
- [SDR ZZDA5321897](https://openairdocs.org/sdr/ZZDA5321897), Sep 5, 1997: CHORD. CORRODED. DURING C-CHECK AT AERO CORP, FOUND T-CHORD HAS HEAVY CORROSION FROM STA 360 - STA 294.5, STR 28L. FOUND TO BE BEYOND LIMITS. REMOVED DAMAGED T-CHORD FROM STA 29
- [SDR ZZDA5326797](https://openairdocs.org/sdr/ZZDA5326797), Sep 4, 1997: SKIN. CORRODED. DURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOV
- [SDR ZZDA5323497](https://openairdocs.org/sdr/ZZDA5323497), Sep 4, 1997: SUPPORT. CORRODED. DURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY LONGITUDINAL FLOOR SUPPORT AT BS LBL 14 HAS CORROSION. BLENDED CORROSION MATERIAL LOSS 50 PERCENT BEYOND LIMITS 
- [SDR ZZDA5321597](https://openairdocs.org/sdr/ZZDA5321597), Sep 4, 1997: FLOORBEAM. CORRODED. DURING C-CHECK AT AERO CORP, AFT LAVATORY FLOOR BEAM UPPER CHORD BS 1006 HAS CORROSION AT LBL 9. FABRICATED DOUBLER FROM 7075 T6 .071 INCH 10.50 INCHES, 1.0625 
- [SDR AADA5323597](https://openairdocs.org/sdr/AADA5323597), Sep 4, 1997: SUPPORT. CORRODED. DURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY FLOOR SUPPORT BEAM BS 986.5 - BS 1016 LBL 20 DIAGONALLY TO LBL 4 CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT F
- [SDR 98ZZZX108](https://openairdocs.org/sdr/98ZZZX108), Sep 4, 1997: SKIN. CORRODED. DURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOV
- [SDR ZZDA5317997](https://openairdocs.org/sdr/ZZDA5317997), Sep 2, 1997: SKIN. CORRODED. DURING C-CHECK, LT FS 967 FOUND CORROSION UNDER FASTENER HEAD AT STR 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. FABRICATED FILLER FROM 2024 T3 .071 INCH 1.1250 IN
- [SDR 97ZZZM1052](https://openairdocs.org/sdr/97ZZZM1052), Sep 2, 1997: SKIN. CORRODED. DURING C-CHECK, LEFT FUSELAGE STATION 967 CORROSION UNDER FASTENER HEAD AT STRINGER 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. (M)
- [SDR ZZDA5322997](https://openairdocs.org/sdr/ZZDA5322997), Aug 30, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR SUPPORT AT LBL 12 IAW B 737 
- [SDR ZZDA5322897](https://openairdocs.org/sdr/ZZDA5322897), Aug 30, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM BS 328 HAS CORROSION ON UPPER CHORD FROM RBL 48 TO LBL 12, FOUND TO BE BEYOND LIMITS. REMOVED CORR
- [SDR ZZDA5322797](https://openairdocs.org/sdr/ZZDA5322797), Aug 30, 1997: FLOOR BEAM. CORRODED. PASSENGER CABIN FLOOR BEAM BS 294 HAS CORROSION ON UPPER CHORD FROM RBL 12 TO RBL 50. REMOVED CORROSION FROM THE UPPER CHORD FLOOR BEAM IAW B737 SRM 51-10-1. MA
- [SDR ZZDA5321797](https://openairdocs.org/sdr/ZZDA5321797), Aug 30, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR BEAM AT LBL 12 IAW B 737 SRM

All 88: https://openairdocs.org/deregistered/N460AT-2000-07-06/reports.md

## Other aircraft with N460AT

- [Cancelled 2018-04-24](https://openairdocs.org/deregistered/N460AT-2018-04-24): Turner Allan C PERCEPTER ULTRA PUP, S/N AT001-00. Registration expired, pending cancellation. Owner: [Turner Allan C](https://openairdocs.org/faa-owner/TURNER%20ALLAN%20C), [Montello, WI](https://openairdocs.org/faa-place/WI/Montello)

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