# N217US: Boeing 737-201, registration cancelled 2000-07-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 20, 2000
- Exported to: Peru
- 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: 20215
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 14, 1997
- Last registry action: May 16, 2000
- Mode S code: A1D556
- 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/N217US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=217US
- Page: https://openairdocs.org/deregistered/N217US-2000-07-20

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 (50)

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

- [SDR F3LA99109](https://openairdocs.org/sdr/F3LA99109), Aug 10, 1999: MASK. DID NOT DEPLOY. DEN - DURING DEMONSTRATION, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM MANUAL A
- [SDR F3LA99045](https://openairdocs.org/sdr/F3LA99045), Jun 4, 1999: VALVE. FAILED. DEN - FLT 546 - FLIGHT CREW REPORTED CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CLOSED OUTFLOW VALVE USING MANUAL DC AT 32,500 FEET. CABIN CONTINUED TO CLIMB A
- [SDR F3LA99033](https://openairdocs.org/sdr/F3LA99033), Apr 23, 1999: BOLT. CRACKED. DEN - FLT 857 - DURING SERVICE CHECK, EO 71-20-737-002 WAS ACCOMPLISHED WHICH FOUND THE NR 2 ENGINE OUTBOARD LUG BEARING LOOSE AND DISPLACED. AN ULTRA SOUND INS
- [SDR F3LA99002](https://openairdocs.org/sdr/F3LA99002), Jan 13, 1999: WEB. CRACKED. PHX - DURING SERVICE CEHCK, MAINTENANCE REPORTED .5 INCH CRACK ON WEB OF LEFT NLG WHEEL WELL STATION 285. ONE RIVET BORKEN AND EVIDENCE OF INTERGRANULAR CORROSI
- [SDR 99ZZZM189](https://openairdocs.org/sdr/99ZZZM189), Jan 11, 1999: WEB. CRACKED. LEFT NLG W/W STATIN 285, .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANE
- [SDR 99ZZZM187](https://openairdocs.org/sdr/99ZZZM187), Jan 11, 1999: WEB. CRACKED. LEFT NLG W/W STATION 285 HAS .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS 
- [SDR F3LA98197](https://openairdocs.org/sdr/F3LA98197), Dec 9, 1998: BATTERY. DISCHARGED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M186, REF WDM 33.51.01) FAILED TO ILLUMINATE BRI
- [SDR F3LA98196](https://openairdocs.org/sdr/F3LA98196), Dec 9, 1998: BATTERY. DISCHARGED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED CONTROL CABIN ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M185, REF WDM 33.51.01) FAILED TO ILLUMINA
- [SDR F3LA98194](https://openairdocs.org/sdr/F3LA98194), Nov 19, 1998: LINE. LEAKING. DEN - UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 ENGINE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE HYDRAULIC PUMP AND DECLARED AN E
- [SDR F3LA98193](https://openairdocs.org/sdr/F3LA98193), Nov 13, 1998: FAN. MALFUNCTIONED. SAN - UPON DESCENT INTO SAN, FLIGHT CREW REPORTED SULFUR/ELECTRICAL ODOR FROM AIR VENTS AT ROW 5 AND 6 ON LEFT SIDE OF AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDEN
- [SDR F3LA98171](https://openairdocs.org/sdr/F3LA98171), Oct 13, 1998: SOLENOID. FAILED. FLT 658 - DEN - AIR TURN BACK, UPON CLIMB-OUT FROM DEN, FLIGHT CREW REPORTED NR 1 ENGINE START VALVE 'OPEN' LIGHT ILLUMINATED. NR 1 ENGINE WAS SHUT DOWN AND AIR
- [SDR F3LA98075](https://openairdocs.org/sdr/F3LA98075), May 27, 1998: SKIN. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SKIN AND DOUBLER AT BS 980-1012, STRINGER 27R. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PART
- [SDR F3LA98074](https://openairdocs.org/sdr/F3LA98074), May 27, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BAY STRINGER 27R, RBL 5, BS 912-947. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PART
- [SDR F3LA98073](https://openairdocs.org/sdr/F3LA98073), May 27, 1998: FRAME. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN FORWARD GALLEY DOOR AFT FRAME, 4 INCHES DOWN FROM TOP CORNER OUTBOARD RADIUS. MAINTENANCE REMOVED
- [SDR F3LA98072](https://openairdocs.org/sdr/F3LA98072), May 27, 1998: SKIN. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACKS ON UPPER SKIN SURFACE AT RIGHT WING, BL 103.5, TWO INCHES FORWARD OF AFT SPAR. MAINTENANCE FABRICATED REPLACEME
- [SDR F3LA98071](https://openairdocs.org/sdr/F3LA98071), May 27, 1998: DOUBLER. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED LEFT WING FIXED LEADING EDGE SKIN DOUBLER CRACKED AT NR 3 SLAT OUTBOARD AUXILLIARY TRACK CUTOUT. MAINTENANCE REMOVED D
- [SDR F3LA98069](https://openairdocs.org/sdr/F3LA98069), May 27, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 907 PLUS 15, RBL 13, WL 169. MAINTENANCE REMOVED DAMAGED AREA (1.5 INCH BY 1 INCH). FABR
- [SDR F3LA98068](https://openairdocs.org/sdr/F3LA98068), May 27, 1998: BULKHEAD. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, LBL 4.7, WL 192.5 TO 193.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACMENT PARTS AN
- [SDR F3LA98067](https://openairdocs.org/sdr/F3LA98067), May 27, 1998: BULKHEAD. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL RIGHT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA 12 INCHES. FABRICATED REPLA
- [SDR F3LA98066](https://openairdocs.org/sdr/F3LA98066), May 27, 1998: BULKHEAD. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL LEFT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA, 12 INCHES. FABRICATED REPLA
- [SDR F3LA98065](https://openairdocs.org/sdr/F3LA98065), May 27, 1998: SHEAR TIE. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 1006, LBL 4 THROUGH RBL 4, WL 178. MAINTENANCE REMOVED CORRODED AREA, 1.5 INCH BY 2.5 INC
- [SDR F3LA98064](https://openairdocs.org/sdr/F3LA98064), May 27, 1998: INTERCOSTAL. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, LBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AN
- [SDR F3LA98063](https://openairdocs.org/sdr/F3LA98063), May 27, 1998: INTERCOSTAL. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, RBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0476 AN
- [SDR F3LA98061](https://openairdocs.org/sdr/F3LA98061), May 27, 1998: BULKHEAD. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, RBL 4.7, WL 212-213. MAINTENANCE REMOVED CRACKED AREA (2 INCH BY 3.5 INCH), FABRICATED REPLA
- [SDR F3LA98060](https://openairdocs.org/sdr/F3LA98060), May 27, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26L, BS 888-892, LBL 13, WL 163. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 5
- [SDR F3LA98059](https://openairdocs.org/sdr/F3LA98059), May 27, 1998: STRINGER. CORRODED. PAE - DURNIG C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON STRINGER 26R, BS 1006-1014. MAINTENANCE FABRICATED REPLACEMENT STRINGER AND REPAIR PARTS AND RE
- [SDR F3LA98057](https://openairdocs.org/sdr/F3LA98057), May 17, 1998: BULKHEAD WEB. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, LBL 6.7, WL 212-213. MAINTENANCE STOP DRILLED CRACK, FABRICATED REPLACEMENT PARTS AND
- [SDR F3LA98056](https://openairdocs.org/sdr/F3LA98056), May 17, 1998: BULKHEAD WEB. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, RBL 4.7, WL 190-191.5. MAINTENANCE REMOVED DAMAGED AREA (1 INCH BY 1 INCH). FABRICATE
- [SDR F3LA98055](https://openairdocs.org/sdr/F3LA98055), May 17, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AT BS 440, BL0, WL 148. MAINTENANCE REMOVED DAMAGED AREA (4.6 INCH BY 1.1 INCH). FABRICATED REP
- [SDR F3LA98054](https://openairdocs.org/sdr/F3LA98054), May 17, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON SHEAR TIE AT BS 727A, WL 149, RBL 13. MAINTENANCE FABRICATED REPLACEMENT SHEARTIE AND REPAIRED 
- [SDR F3LA98014](https://openairdocs.org/sdr/F3LA98014), Apr 9, 1998: SKIN. CORRODED. DEN - FLT 43 - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD92-25-09), INSPECTION REPORTED BULGING OF SKIN (CORROSION) AT STATION 901, S23R AND
- [SDR F3LA98013](https://openairdocs.org/sdr/F3LA98013), Apr 9, 1998: SKIN. CRACKED. DEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED .625 INCH CRACK SIX INCHES FORWARD OF L-1 DOOR IN FUSELAGE SK
- [SDR F3LA97143](https://openairdocs.org/sdr/F3LA97143), Sep 1, 1997: GEARBOX. FAILED. DEN - FLT 780 - FLIGHT CREW REPORTED NR 1 ENGINE WAS SHUT DOWN DUE TO LOW OIL QTY AND AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED O-RING ON FUEL CARBON SEAL
- [SDR F3LA97095](https://openairdocs.org/sdr/F3LA97095), Feb 18, 1997: RIB. CRACKED. CLT - ONE INCH CRACK IN RIB AROUND RIVET HOLES BS 800, S19R TO S27R. INSTALLED NEW FRAME AND WEBS PER BOEING DRAWINGS 65-C35243 AND 69-42945, AND EA 59494. (M)
- [SDR F3LA97094](https://openairdocs.org/sdr/F3LA97094), Feb 3, 1997: SKIN. CRACKED. CLT - FOUND CRACK IN THE NR 2 ENGINE PYLON SCREW HOLE. INSTALLED NEW ANGLE, DOUBLERS AND FILLERS PER EA 57446, EA 57462, SRM 51-40-01 AND SRM 54-10-3. (M)
- [SDR F3LA97045](https://openairdocs.org/sdr/F3LA97045), Jan 27, 1997: SEAT TRACK. CORRODED. CLT - FOUND SURFACE CORROSION AT SEAT TRACK MOUNT AT STATION 294, RBL 45.5. REMOVED SURFACE CORROSION ALODINED AND PRIMED. (M)
- [SDR F3LA97044](https://openairdocs.org/sdr/F3LA97044), Jan 23, 1997: FLOOR BEAM. CORRODED. CLT - FOUND CORROSION AROUND SCREW HOLE BS 947, RBL 40. REMOVED SURFACE CORROSION ON FLOOR BEAM PER SRM 51-10-06. (M)
- [SDR F3LA97043](https://openairdocs.org/sdr/F3LA97043), Jan 23, 1997: FLOOR BEAM. CORRODED. CLT - FOUND CORROSION AROUND SCREW HOLES AND ADJACENT AREAS, BS 947, RBL 3 THROUGH RBL 22 ON FLOOR BEAM. REMOVED SURFACE CORROSION BY BURNISHING THE TOP SURFACE
- [SDR F3LA97042](https://openairdocs.org/sdr/F3LA97042), Jan 23, 1997: FLOOR BEAM. CORRODED. CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 987, LBL 5. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-0. (M)
- [SDR F3LA97041](https://openairdocs.org/sdr/F3LA97041), Jan 23, 1997: FLOOR BEAM. CORRODED. CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 967, RBL 42. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-6. (M)
- [SDR F3LA97040](https://openairdocs.org/sdr/F3LA97040), Jan 23, 1997: SEAT TRACK. CORRODED. CLT - FOUND CORROSION (C53-107-02) ON AFT GALLEY SEAT TRACK AT STATION 986-1016, RBL 20. REMOVED CORROSION PER SRM 51-10-6 AND ALODINED AND PRIMED THE AREA. (M)
- [SDR F3LA97039](https://openairdocs.org/sdr/F3LA97039), Jan 23, 1997: SUPPORT. CORRODED. CLT - FOUND CORROSION (C53-107-02) ON AFT LAV FLOOR SUPPORT, STATION 1006-966, LBL 10-10. REMOVED NUT PLATES ON THE FLOOR BEAM SUPPORT, REMOVED LIGHT CORROSION 
- [SDR F3LA97038](https://openairdocs.org/sdr/F3LA97038), Jan 23, 1997: FLOOR BEAM. CORRODED. CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 986, RBL 50 THROUGH LBL 21. REMOVED SURFACE CORROSION PER SRM 51-10-6. ALODINED AND PRIMED THE AREA.
- [SDR 97ZZZX313](https://openairdocs.org/sdr/97ZZZX313), Jan 3, 1997: WIRE. FAILED. ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY AISLE PATH LIGHTING AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OKAY.
- [SDR F3LA96008](https://openairdocs.org/sdr/F3LA96008), Feb 14, 1996: WARNING HORN. SOUNDED. FLT NR 546 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE LANDING GEAR WARNING HORN SOUNDED WITH THROTTLES RETARDED TO IDLE AND FLAPS UP. WARNING HORN DID NOT S
- [SDR F3LA95019](https://openairdocs.org/sdr/F3LA95019), Dec 14, 1995: PCU. MALFUNCTIONED. FLT NR 465 - DEN -UPON ARRIVAL, FLIGHT CREW REPORTED RUDDER TRIM REQUIRED ONE FULL UNIT OF RIGHT RUDDER ADJUSTMENT TO ESTABLISH ZERO DEGREE DRIFT. MAINTENANCE R
- [SDR F3LA95015](https://openairdocs.org/sdr/F3LA95015), Jul 31, 1995: ANTI-SKID CONTL. FAILED. BZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHE
- [SDR F3LA95003](https://openairdocs.org/sdr/F3LA95003), Jan 30, 1995: EEL CONNECTOR. BROKEN. FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. PLACARDED PER MEL 33-14. UPON ARRIVAL IN DEN, MAINTENA
- [SDR F3LA95002](https://openairdocs.org/sdr/F3LA95002), Jan 25, 1995: EEL BATTERY PACK. INOPERATIVE. OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTE
- [SDR 95ZZZX785](https://openairdocs.org/sdr/95ZZZX785), Jan 25, 1995: EEL BATT CHARGER. INOPERATIVE. OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTE

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW97LA177](https://openairdocs.org/ntsb/FTW97LA177), May 4, 1997: Boeing 737-201 (N217US), Denver, CO, no damage. Probable cause: The flight attendant's failure to assure that the jetway was placed in the proper position prior to opening the forward cabin entry door.
- [NTSB ATL89IA099](https://openairdocs.org/ntsb/ATL89IA099), Mar 9, 1989: Boeing 737-201 (N217US), Dayton, OH, incident, no damage. Probable cause: AN EXCESSIVELY WORN OUTFLOW VALVE IN THE CABIN EVIRONMENTAL/PRESSURIZATION SYSTEM THAT RESULTED IN A RAPID CABIN DEPRESSURIZATION.

## FAA accident and incident reports (3)

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 19980925038689I](https://openairdocs.org/incident/19980925038689I), Sep 25, 1998: Boeing 737201 (N217US), El Paso, TX. (-5) 2 - 1/2 Inch hydraulic chaffed thru causing loss of -a- system hydraulic fluid. Location was right hand aft wing spar inboard of #2 engine pylon. Crew…
- [Accident 19970504008399A](https://openairdocs.org/incident/19970504008399A), May 4, 1997: Boeing 737201 (N217US), Denver, CO. Aircraft parked on ramp, flight attendant fell from forward entrance door onto ramp. (.4)the parked airplane was ready for pushback when the 'b' flight…
- [Incident 19890309003999I](https://openairdocs.org/incident/19890309003999I), Mar 9, 1989: Boeing 737201 (N217US), Dayton, OH. Lost control of pressurization system. Emergency descent. Found a faulty outflow valve.

## Other aircraft with N217US

- [Registered now](https://openairdocs.org/aircraft/N217US): Raytheon B300, S/N FL-519, built 2007

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