# N214AU: Boeing 737-201, registration cancelled 2000-07-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 20, 2000
- Exported to: Chile
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 20214
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 14, 1997
- Last registry action: May 16, 2000
- Mode S code: A1C871
- Owner when cancelled: [First Security Bank Na Owner Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20OWNER%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/N214AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=214AU
- Page: https://openairdocs.org/deregistered/N214AU-2000-07-20

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 737-201: https://openairdocs.org/model/boeing-737-201.md

## Service difficulty reports (57, newest 50)

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

- [SDR F3LA99129](https://openairdocs.org/sdr/F3LA99129), Oct 13, 1999: HEAT DUCT. CRACKED. MLI - DURING CLIMB-OUT FROM MDW, FLIGHT CREW REPORTED THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT WAS DIVERTED TO MOLINE, IL AND LANDED WITHOUT INCIDEN
- [SDR F3LA99113](https://openairdocs.org/sdr/F3LA99113), Aug 12, 1999: WIRE. BROKEN. DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN GROUND WIRE AFT OF BATTERY P
- [SDR F3LA99112](https://openairdocs.org/sdr/F3LA99112), Aug 11, 1999: WIRE. BROKEN. DEN - FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE AT D9022P AND CHECKED OKAY. TC: 90,745. (X
- [SDR F3LA99111](https://openairdocs.org/sdr/F3LA99111), Aug 10, 1999: BATTERY PACK. DISCHARGED. DEN - FLT 317 - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS FLICKERED IN-FLIGHT. MAINTENANCE RECHARGED BATTERY PACKS AND OPERATIONAL CHECKED OKAY. PART TC:
- [SDR F3LA99110](https://openairdocs.org/sdr/F3LA99110), Aug 9, 1999: BATTERY CHARGER. FAILED. DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING DID NOT EXTINGUISH WHEN TESTED. MAINTENANCE REPLACED AFT SEAT BATTERY CHARGING
- [SDR F3LA99080](https://openairdocs.org/sdr/F3LA99080), Jun 16, 1999: BEARING. OUT OF LIMITS. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN RIGHT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .057. MAINTENANCE REPLACED RIGHT MLG FOR
- [SDR F3LA99078](https://openairdocs.org/sdr/F3LA99078), Jun 16, 1999: BEARING. OUT OF LIMITS. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN LEFT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .052. MAINTENANCE REPLACED LEFT MLG FORWA
- [SDR F3LA99028](https://openairdocs.org/sdr/F3LA99028), Apr 4, 1999: BATTERY PACK. DISCHARGED. DEN - UPON WALK AROUND MAINTENANRE REPORTED EMERGENCY LIGHT ACTIVATION CABLE LOOSE AT SLIDE COVER ON L1 DOOR, EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED 
- [SDR F3LA99020](https://openairdocs.org/sdr/F3LA99020), Feb 22, 1999: WIRE. BROKEN. PHX - DURING C-CHECK INSPECTION, REPORTED CABIN EMERGENCY LIGHTING AND FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT OVERWING BATTERY PCK
- [SDR F3LA99019](https://openairdocs.org/sdr/F3LA99019), Feb 22, 1999: WIRE. BROKEN. PHX - DURING C-CHECK INSPECTION, REPORTED BROKEN WIRE IN L1 DOOR EXIT LIGHT. MAINTENANCE REPAIRED BROKEN WIRE PER SPWM 20-30-12. (M)
- [SDR F3LA99016](https://openairdocs.org/sdr/F3LA99016), Feb 22, 1999: BRACKET. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED FASTENER MISSING AND CRACKED MOUNT FLANGE ON 8TH STAGE BLEED DUCT. MAINTENANCE INSTALLED FASTENER AND REPAIRED BRACKET
- [SDR F3LA99010](https://openairdocs.org/sdr/F3LA99010), Feb 22, 1999: FRAME. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED A 4 INCH CRACK IN FRAME AT BS 380, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLA
- [SDR F3LA99009](https://openairdocs.org/sdr/F3LA99009), Feb 22, 1999: SKIN. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED DENT AND CRACK ON RIGHT WING OUTBOARD SIDE OF PYLON, FLAP SIDE LOAD ROLLER AND CORROSION UNDER FLAP ROLLER WEAR STRIP.
- [SDR F3LA99007](https://openairdocs.org/sdr/F3LA99007), Feb 22, 1999: BULKHEAD FRAME. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED FORWARD CARGO RIGHT FORWARD BULKHEAD FRAME CRACKED. MAINTENANCE REMOVED DAMAGED SECTION , FABRICATED REPLACEMENT PARTS
- [SDR F3LA99022](https://openairdocs.org/sdr/F3LA99022), Feb 21, 1999: FITTING. BROKEN. PHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED ATTACH ANGLE AND R
- [SDR F3LA99018](https://openairdocs.org/sdr/F3LA99018), Feb 21, 1999: STIFFENERS. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED WEB STIFFENERS ON FORWARD EDGE OF NR 2 ENGINE THRUST REVERSER COWL CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICAT
- [SDR F3LA99017](https://openairdocs.org/sdr/F3LA99017), Feb 21, 1999: HOUSING. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED 9 INCH CRACK ON NR 6 TURBINE BEARING EXHAUST CASE HOUSING BETWEEN 9-12 O'CLOCK POSITION ON NR 1 ENIGNE. MAINTENANCE RE
- [SDR F3LA99015](https://openairdocs.org/sdr/F3LA99015), Feb 21, 1999: SKIN. CRACKED. PHX - DURING C-CHECK INSPECTION REPORTED A 1.25 INCH CRACK ON LEFT WING TRAILING EDGE INBOARD MIDFLAP INBOARD EDGE FLAP REAR SPAR T-CHORD. MAINTENANCE REMOVED D
- [SDR F3LA99014](https://openairdocs.org/sdr/F3LA99014), Feb 21, 1999: DOOR. BENT. PHX - DURING C-CHECK INSPECTION, REPORTED LEFT MAIN GEAR AFT OUTER CORNER OF INBOARD DOOR BENT AND BULGING. MAINTENANCE REMOVED FASTENERS, CLEANED AREA, RESEALE
- [SDR F3LA99013](https://openairdocs.org/sdr/F3LA99013), Feb 21, 1999: RIB. CRACKED. PHX - DURING C-CHECK INSPECTION, RERPORTED CRACK ON FORWARD SIDE OF RIB AT BS 505. MAINTENANCE REPLACED RIB PER SRM 51-10-1, PAGE 5, AND 51-30-2. (M)
- [SDR F3LA99012](https://openairdocs.org/sdr/F3LA99012), Feb 21, 1999: SKIN. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED A .125 INCH CRACK ON RIGHT WING UPPER WING SKIN AT NR 5 SPOILER CENTER HINGE. MAINTENANCE REPAIRED PER SRM 57-30-1, FI
- [SDR F3LA99011](https://openairdocs.org/sdr/F3LA99011), Feb 21, 1999: WEDGE. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED 1 INCH BY 1.5 INCH CRACK IN LEFT WING TRAILING EDGE FLAP WEDGE. MAINTENANCE REPAIRED PER SRM 57-50-1, FIG 16, DETAIL 1
- [SDR F3LA99006](https://openairdocs.org/sdr/F3LA99006), Feb 21, 1999: FRAME. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED A 4.5 INCH CRACK IN FRAME AT BS 360, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REP
- [SDR F3LA99008](https://openairdocs.org/sdr/F3LA99008), Feb 20, 1999: SKIN. CRACKED. PHX - DURING C-CHECK INSPECTION, REPORTED A .5 INCH CRACK IN LEFT WING UPPER SKIN AT WBL 157. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER/TRIPLER AND REP
- [SDR F3LA99021](https://openairdocs.org/sdr/F3LA99021), Feb 9, 1999: BATTERY PACK. DISCHARGED. PHX - DURING C-CHECK INSPECTION, REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RECHARGED BATTERY PACK PER MM 33-51-11. (M)
- [SDR F3LA98144](https://openairdocs.org/sdr/F3LA98144), Jul 28, 1998: BATTERY PACK. DISCHARGED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK AND SYSTEM CHECKED OKA
- [SDR F3LA98037](https://openairdocs.org/sdr/F3LA98037), Apr 30, 1998: WIRE. FAILED. ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT WAS 1 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA97170](https://openairdocs.org/sdr/F3LA97170), Dec 25, 1997: CONNECTOR. FAILED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED CANNON PLUG WIRE CONNECTING PIN AND CHECKE
- [SDR F3LA97167](https://openairdocs.org/sdr/F3LA97167), Dec 2, 1997: SKIN. CRACKED. PAE - CRACK IN UPPER AFT CORNER OF L-3 WINDOW CUTOUT. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-30-3. (M)
- [SDR F3LA97166](https://openairdocs.org/sdr/F3LA97166), Dec 2, 1997: BULKHEAD. CRACKED. PAE - RIGHT BS 727 BULKHEAD LOWER CHORD DISCOVERED CRACKED DURING ACCOMPLISHMENT OF FRONTIER ENGINEERING ORDER NR 53-10-737-004. REMOVED AND REPLACED LOWER SECT
- [SDR F3LA97165](https://openairdocs.org/sdr/F3LA97165), Dec 2, 1997: SKIN. CORRODED. PAE - CORROSION ON INNER DOUBLER ON BACK SIDE OF FORWARD LAV SERVICING PAN AT STATION 270. CORROSION OUT OF LIMITS IAW SRM 51-10-6, 53-10-1. REMOVED AND REPLACE
- [SDR F3LA97164](https://openairdocs.org/sdr/F3LA97164), Dec 2, 1997: SKIN. CORRODED. PILLOWING SKIN BETWEEN RIVETS AT BS 416, STRINGER 221. REMOVED FASTENERS AND DISCOVERED CORROSION BETWEEN SKIN AND STRINGER, CORROSION ON SKIN OUT OF LIMITS IAW
- [SDR F3LA96051](https://openairdocs.org/sdr/F3LA96051), Oct 21, 1996: STRINGER. CORRODED. PAE - FOUND CORROSION AROUND FASTENERS IN STRINGER 27R, BS 947-967 WL 173. REMOVED DAMAGED SECTION OF STRINGER 27R, FABRICATED REPAIR PARTS AND INSTALLED IAW SR
- [SDR F3LA96050](https://openairdocs.org/sdr/F3LA96050), Oct 18, 1996: BULKHEAD WEB. CRACKED. PAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS REPLACED IAW BOEING SRM AND BOEING DRAWING 
- [SDR F3LA96049](https://openairdocs.org/sdr/F3LA96049), Oct 18, 1996: BULKHEAD WEB. CRACKED. PAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES
- [SDR F3LA96048](https://openairdocs.org/sdr/F3LA96048), Oct 17, 1996: CHORD. CRACKED. PAE - FOUND CRACK INDICATIONS IN LT BS 727, STRINGER 18A OUTBOARD CHORD FORWARD AND AFT OF BOTH FASTENER HOLES. ACCESSED REPAIR AREA. FOUND CRACKS CONTAINED IN 
- [SDR F3LA96046](https://openairdocs.org/sdr/F3LA96046), Oct 17, 1996: FLOORBEAM. CRACKED. PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS BS 520 WL 207.75, RBL 25 AND RBL 46. REPAIRED FLOORBEAM CRACK AT BS 520, WL 207.75, RBL 25 AND RBL 46 IAW EWO 396-
- [SDR F3LA96045](https://openairdocs.org/sdr/F3LA96045), Oct 17, 1996: FLOORBEAM. CRACKED. PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS AT BS 520, WL 207.75, LBL 25 - LBL 47. REPAIRED CRACKS IN FLOORBEAM AT BS 520, WL 207.75, LBL 25, LBL 45 AND LBL 4
- [SDR F3LA96044](https://openairdocs.org/sdr/F3LA96044), Oct 16, 1996: CHORD. CRACKED. PAE - HFEC INSPECTION OF THE BS 178 LT SIDE CHORD AT WL 194-196 SHOWS A CRACK INDICATION. CUT OUT DAMAGED AREA OF CHORD. FABRICATED REPAIR PARTS AND INSTALLED R
- [SDR F3LA96040](https://openairdocs.org/sdr/F3LA96040), Oct 16, 1996: KEELBEAM. CRACKED. PAE - FOUND CRACK IN THE AFT END OF RT KEELBEAM BS 814-818, STRINGER 27 RT. REPAIRED CRACK IAW TRAMCO EWO 96-0613. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 255. (
- [SDR F3LA96047](https://openairdocs.org/sdr/F3LA96047), Oct 15, 1996: STIFFENER. CRACKED. PAE - FOUND CRACK EMANATING FROM FASTENER HOLE AT BS 540, WL 203.5, LBL 26 ON VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER AND INSTAL
- [SDR F3LA96042](https://openairdocs.org/sdr/F3LA96042), Oct 15, 1996: CHORD. CRACKED. HFEC INSPECTION EXHIBITS CRACK APPROX 1.5 INCH LONG IN RADIUS OF BS 540 CHORD BETWEEN STRINGER 21R AND STRINGER 22R, CRACK IS ON SPLICE PLATE. ACCESSED AREA, RE
- [SDR F3LA96041](https://openairdocs.org/sdr/F3LA96041), Oct 15, 1996: DOOR FRAME. CRACKED. PAE - HFEC INSPECTION OF THE FORWARD CARGO DOOR FRAME, REVEALED A CRACK INDICATION AT STRINGER 23R ON THE FORWARD SIDE OF THE FRAME AT THE LOWEST OUTBOARD CORNE
- [SDR F3LA96038](https://openairdocs.org/sdr/F3LA96038), Oct 15, 1996: FRAME. CORRODED. PAE - FOUND CORROSION (C53-208-01) ON AFT SIDE OF FRAME BS 520 RBL 7, WL 150. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FRAME PER SRM 51-40-3. (M)
- [SDR F3LA96039](https://openairdocs.org/sdr/F3LA96039), Oct 14, 1996: FRAME. CRACKED. PAE - FOUND CRACK IN FRAME WEB AT UPPER CORNER OF STRINGER CUTOUT BS 294.5, STRINGER 18R. FOUND CRACK CONTAINED IN FASTENER HOLE. REPAIRED PER SRM 51-40-02 AND 
- [SDR F3LA96037](https://openairdocs.org/sdr/F3LA96037), Oct 14, 1996: SHEAR TIE. CORRODED. PAE - FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-10-4
- [SDR F3LA96036](https://openairdocs.org/sdr/F3LA96036), Oct 12, 1996: FLOORBEAM. CORRODED. PAE - FOUND CORROSION ON UNDERSIDE OF CARGO FLOORBEAM BS 500, RBL 18, WL 156. REMOVED CORROSION ON UNDERSIDE OF FLOORBEAM AND REPAIRED IAW SRM 53-10-1, 51-40-3 
- [SDR F3LA96035](https://openairdocs.org/sdr/F3LA96035), Oct 12, 1996: STRINGER. CRACKED. PAE - FOUND CRACK IN STRINGER 10 LEFT, BS 296, WL 256. REMOVED DAMAGED SECTION OF STRINGER 10L BS 296, WL 256. REPAIRED STRINGER IAW SRM 53-10-3 FIGURE 3 RED WO
- [SDR F3LA96034](https://openairdocs.org/sdr/F3LA96034), Oct 12, 1996: INTERCOSTAL. CRACKED. PAE - FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS ARE CRACKED ON THE AFT OTBOARD FLANGE. REMOVED AND REPLACED FORWARD CARGO DOOR FORW
- [SDR F3LA96033](https://openairdocs.org/sdr/F3LA96033), Oct 12, 1996: STRINGER. CRACKED. FOUND CRACK IN STRINGER 14R AT BS 277. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC INTERIOR 178. (M)

All 57: https://openairdocs.org/deregistered/N214AU-2000-07-20/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990418019709I](https://openairdocs.org/incident/19990418019709I), Apr 18, 1999: Boeing 737201 (N214AU), Omaha, NE. Engine failure after takeoff. Crew followed all check lists, including attempted re-start, returned to departure airport and landed without further incident.
- [Incident 19950720025029I](https://openairdocs.org/incident/19950720025029I), Jul 20, 1995: Boeing 737201 (N214AU), Lincoln, NE. Climbing, right engine oil temp high. Shut down. Returned to omaha. Replaced oil temp bulb.

## Other aircraft with N214AU

- [Registered now](https://openairdocs.org/aircraft/N214AU): Bell 214ST, S/N 28129, built 1984

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