# N212US: Boeing 737-201, registration cancelled 2000-06-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 2, 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: 20212
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 14, 1997
- Last registry action: May 16, 2000
- Mode S code: A1C2C3
- 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/N212US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=212US
- Page: https://openairdocs.org/deregistered/N212US-2000-06-02

From the FAA registry file of October 28, 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 (29)

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

- [SDR F3LA99108](https://openairdocs.org/sdr/F3LA99108), Aug 10, 1999: MASKS. DID NOT DEPLOY. DEN - DURING DEMO FLIGHT, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DROP IN MANUAL MODE. MAINTENANCE RESET T-HANDLE IN COCKPIT AND PERFORMED AN ANNUAL DROP TEST
- [SDR F3LA99084](https://openairdocs.org/sdr/F3LA99084), Jun 25, 1999: LINE. FAILED. PHX - UPON ARRIVAL, FLIGHT CREW REPORTED 'A' SYSTEM HYDRAULIC LIGHT FLICKERED, THEN LOST AL SYSTEM 'A' HYDRAULICS AT ALTITUDE. 'B' SYSTEM AND STANDBY SYSTEM REM
- [SDR F3LA99036](https://openairdocs.org/sdr/F3LA99036), Apr 14, 1999: WEB. CRACKED. DEN - FLT DURING C-CHECK, INSPECTION REPORTED RIGHT A/C BAY VERTICAL WEB CRACKED AT FORWARD END OF RAM AIR DUCT, BBL 41 KEEL BEAM. MAINTENANCE REPAIRED PER EA 7
- [SDR F3LA99034](https://openairdocs.org/sdr/F3LA99034), Apr 14, 1999: FRAME. CRACKED. DEN - DURING C-CHECK, INSPECTION REPORTED TWO CRACKS ON FRAME AT BS 380 BETWEEN STR 20R AND STR 21R IN THE FORWARD CARGO COMPARTMENT. MAINTENANCE FABRICATED AND
- [SDR F3LA98162](https://openairdocs.org/sdr/F3LA98162), Aug 30, 1998: CONTROL CABLE. FAILED. DEN - DURING DESCENT, FLIGHT CREW REPORTED TRAILING EDGE FLAPS STUCK. LEFT FLAP UP, RIGHT FLAP AT 1 DEGREE. LEADING EDGE DEVICES FULL EXTEND. AN EMERGENCY WAS D
- [SDR F3LA98161](https://openairdocs.org/sdr/F3LA98161), Aug 9, 1998: PRESSURE BLKHD. CRACKED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 7 INCH/8 INCH CRACK IN NOSE WHEEL WELL PRESSURE WEB. OUTBOARD RT SIDE AFT OF DOWNLOCK VIEWER. MAINTENANCE REM
- [SDR F3LA97175](https://openairdocs.org/sdr/F3LA97175), Jan 17, 1998: RIB. CRACKED. PAE - FIXED L/E NR 3 SLAT TRACK INBOARD MAIN TRACK, INBOARD ROLLER SUPPORT RIB HAS CRACK, FSS 271, SS 31.42. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-30-02. 
- [SDR F3LA97174](https://openairdocs.org/sdr/F3LA97174), Jan 17, 1998: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHTS FAIL BATTERY CAPACITY TEST. BOTH OVERWING EXIT DOORS, CENTER AISLE, AFT ENTRY AND SERVICE DOOR SIDE LIGHTS AND BOTH AFT SLIDE LIGHTS FAIL 
- [SDR F3LA97173](https://openairdocs.org/sdr/F3LA97173), Jan 17, 1998: WEB. CRACKED. PAE - HORIZ WEB AT BS 661, LBL 67, LL 208 IS CRACKED. FABRICATED WEB USING 7075-T6 .040 AND INSTALLED PER SRM 51-10-2. (M)
- [SDR F3LA97172](https://openairdocs.org/sdr/F3LA97172), Jan 17, 1998: SKIN. WORN. PAE - TWO HOLES BURNED (ERRODED) THROUGH UPPER FWD INBOARD SKIN ABOVE AIR CLEANER IN RT AC BAY. REPAIRED IAW SRM 53-30-3, PAGE 9 AND PAGE 10. DAMAGE OCCURRED DU
- [SDR F3LA97161](https://openairdocs.org/sdr/F3LA97161), Nov 28, 1997: SKIN. CRACKED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 6 INCH CRACK IN THE NOSE WHEEL WELL OVERHEAD SKIN AT STATION 276.5, LBL 6 TO LBL 12. MAINTENANCE REPAIRED CRA
- [SDR F3LA97160](https://openairdocs.org/sdr/F3LA97160), Nov 28, 1997: LIGHT. INOPERATIVE. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY LIGHT AT L1 DOOR AFT FUSELAGE DIM. MAINTENANCE REPLACED LAMP HOUSING AND CHECKED OK. (M)
- [SDR F3LA97153](https://openairdocs.org/sdr/F3LA97153), Oct 1, 1997: BATTERY PACK. DISCHARGED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS BETWEEN ROWS 7 AND 13 INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OKAY. (X)
- [SDR F3LA97134](https://openairdocs.org/sdr/F3LA97134), Jun 1, 1997: BULB. FAILED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROWS 14 A, B, C, 16 A, B, C, 17 A, B, C, AND 18 A, B, C, INOPERATIVE. MAINTENANCE R
- [SDR F3LA96063](https://openairdocs.org/sdr/F3LA96063), Nov 27, 1996: FRAME. CORRODED. PAE - FOUND CORROSION ON FORWARD SIDE OF FUSELAGE FRAME VERTICAL FLANGE, STATION 227.8 RBL 19, WL 168. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM. FLAP P
- [SDR F3LA96061](https://openairdocs.org/sdr/F3LA96061), Nov 26, 1996: SKIN. DENTED. FOUND DENT ON AFT AIRSTAIR DOOR APPROXIMATELY 16 INCHES FROM TOP OF DOOR. REMOVED DAMAGE ON AFT ENTRY DOOR OUTER SKIN 1.75 INCH BY 1.75 INCH APPROX 16 INCHES FR
- [SDR F3LA96060](https://openairdocs.org/sdr/F3LA96060), Nov 21, 1996: SKIN. CRACKED. PAE - FOUND CRACK IN SKIN AT THE TOP EDGE OF LOWER DOOR CUTOUT AT BS 977 WL 208. CRACK IS APPROXIMATE 1.5 INCH LONG, TRAVELING FROM EDGE INTO HOLE AND BEYOND. C
- [SDR F3LA96059](https://openairdocs.org/sdr/F3LA96059), Nov 20, 1996: FLOORBEAM. CORRODED. PAE - FOUND CORROSION ON FLOORBEAM AROUND NUTCLIP HOLE AT BS 947, RBL 50, WL 208. BLENDED DAMAGED AREA PER SRM 51-10-02, DAMAGED AREA WAS FOUND TO BE OUT OF LIM
- [SDR F3LA96058](https://openairdocs.org/sdr/F3LA96058), Nov 19, 1996: CHORD. CRACKED. PAE - CRACK INDICATIONS NOTED (3), RIGHT CHORD BS 178, BETWEEN WL 195 AND WL 204. REMOVED 178 RT WEB FOR ACCESS. REMOVED CRACKED CHORD, FABRICATED NEW CHORD AND
- [SDR F3LA96057](https://openairdocs.org/sdr/F3LA96057), Nov 18, 1996: CHORD. PUNCTURED. PAE - FOUND PUNCTURE IN FAIL/SAFE CHORD BS 440 BETWEEN STRINGER 27 AND 28 RT. PUNCTURE IS BELIEVED TO HAVE BEEN CAUSED BY CORROSION. REMOVED AND REPLACED ENTIRE
- [SDR F3LA96056](https://openairdocs.org/sdr/F3LA96056), Nov 18, 1996: CHORD. CRACKED. PAE - FOUND CRACK INDICATION NOTED AT BS 727 OUTBOARD CHORD AT LEFT STRINGER 18A UPPER AFT FASTENER HOLE. ACCESSED AREA, INSTALLED TEMPORARY REPAIR PER SB 73753
- [SDR F3LA96055](https://openairdocs.org/sdr/F3LA96055), Nov 18, 1996: CHORD. CRACKED. PAE - FOUND CRACK INDICATIONS NOTED IN BS 727 OUTBOARD CHORD AT RT STRINGER 18A BETWEEN FORWARD AD AFT FASTENERS, UPPER AND LOWER. ACCESSED AREA. INSTALLED TEMP
- [SDR F3LA96052](https://openairdocs.org/sdr/F3LA96052), Nov 15, 1996: STRINGER. CORRODED. PAE - FOUND CORROSION ON FORWARD END OF STRINGER BS 260-266 STRINGER 22L. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER AND REPAIRED PER SR
- [SDR F3LA96053](https://openairdocs.org/sdr/F3LA96053), Nov 14, 1996: FLOORBEAM. CORRODED. PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM AT NUTCLIP HOLE BS 986.5 RBL 18 UNDER SIDE OF UPPER CHORD. REPAIRED FLOOR BEAM AT BS 986.5, RLB 18, WL 208 IAW E
- [SDR F3LA96054](https://openairdocs.org/sdr/F3LA96054), Nov 13, 1996: FRAME. CORRODED. PAE - WHILE WORKING FLOOR WEB AT BS 987, FOUND CORROSION AND MECHANICAL DAMAGE ON FRAME AT BS 993, RBL 49, WL 210-206. BLENDED OUT CORROSION ON FRAME. FOUND OUT
- [SDR F3LA96017](https://openairdocs.org/sdr/F3LA96017), Jun 21, 1996: POWER SUPPLY. INOPERATIVE. DEN - DURING AN A-6 CHECK, MX REPORTED THE RIGHT EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED THE RIGHT BATTERY POWER SUPPLY AND CHECKED
- [SDR F3LA96016](https://openairdocs.org/sdr/F3LA96016), Jun 21, 1996: BATTERY PACK. DISCHARGED. DEN - DURING AN A-6 CHECK, MAINTENANCE REPORTED THE RIGHT WING EMERGENCY EXIT LIGHT ABOVE INBOARD FLAPS INOPERATIVE. REPLACED THE RIGHT BATTERY PACK AND CHECKED
- [SDR 96ZZZX570](https://openairdocs.org/sdr/96ZZZX570), Jan 29, 1996: CONTROL MODULE. FAILED. MSP - FLT 417 - UPON ARRIVAL, FLIGHT CREW REPORTED AN ACRID ODOR AND SMOKE IN THE CABIN. ODOR AND SMOKE CLEARED WHEN LEFT PACK WAS TURNED OFF. MAINTENANCE REPLA
- [SDR 96ZZZX569](https://openairdocs.org/sdr/96ZZZX569), Jan 28, 1996: VALVE. MALFUNCTIONED. DEN - FLT 233 - UPON ARRIVAL, FLIGHT CREW REPORTED THE LEFT PACK TEMPERATURE CONTROL WENT TO FULL HOT IN AUTOMATIC MODE CAUSING SMOKE IN THE CABIN. SMOKE DISSIP

## Other aircraft with N212US

- [Registered now](https://openairdocs.org/aircraft/N212US): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 029/US, built 2021

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