# N207AU: Boeing 737-201, registration cancelled 2000-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2000
- Exported to: Philippines
- Status when cancelled: Valid registration
- 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: 19423
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 14, 1997
- Last registry action: May 20, 1997
- Mode S code: A1AC17
- 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/N207AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=207AU
- Page: https://openairdocs.org/deregistered/N207AU-2000-02-03

From the FAA registry file of October 31, 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 (79, newest 50)

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

- [SDR F3LA99102](https://openairdocs.org/sdr/F3LA99102), Jul 10, 1999: FAIRING. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER
- [SDR F3LA99101](https://openairdocs.org/sdr/F3LA99101), Jul 10, 1999: FAIRING. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RI
- [SDR F3LA99100](https://openairdocs.org/sdr/F3LA99100), Jul 8, 1999: WIRE HARNESS. DAMAGED. DURNG C-CHECK INSPECTION, REPORTED DAMAGED WIRING IN THE VERTICAL STABILIZER. CAUSE OF DAMAGE APPEARS TO BE SKYDROL HYDRAULIC FLUID. THE DAMAGE BEGAN APPROX 8 I
- [SDR F3LA99099](https://openairdocs.org/sdr/F3LA99099), Jun 30, 1999: RIB. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER AFT END. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 
- [SDR F3LA99098](https://openairdocs.org/sdr/F3LA99098), Jun 30, 1999: RIB. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER LOWER SIDE. MAINTENANCE FABRICATED AND REPLACED RIB PER S
- [SDR F3LA99097](https://openairdocs.org/sdr/F3LA99097), Jun 30, 1999: CHORD. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED THREE CRACKS FOUND IN PRESSURE DECK COMPRESSION CHORD AT STATION 663.75, RBL 25 AND LBL 25. MAINTENANCE FABRICATED AND
- [SDR F3LA99096](https://openairdocs.org/sdr/F3LA99096), Jun 30, 1999: IGV. CRACKED. DEN - DURING C-CHECK INSPECTION REPORTED, NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE, 10 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/
- [SDR F3LA99095](https://openairdocs.org/sdr/F3LA99095), Jun 30, 1999: IGV. CRACKED. DEN - DURING C-CHECK, INSPECTION REPORTED NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE AT 2 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P
- [SDR F3LA99090](https://openairdocs.org/sdr/F3LA99090), Jun 29, 1999: SHEAR TIE. CRACKED. DEN - DURING C-CHECK INSPECTION REPORTED, CRACK IN SHEAR TIE, LAST RIVET TO EDGE OF TIE, AT BS 294.5 ABOVE STRINGER 13L. MAINTENANCE REPAIRED CRACKED AT SHEAR T
- [SDR F3LA99088](https://openairdocs.org/sdr/F3LA99088), Jun 29, 1999: ANGLE. CRACKED. DEN - DURING C-CHECK, INSPECTION REPORTED CRACK AT NR 2 ENGINE NOSE COWL FAIRING (SUGAR SCOOP) SEAL RETAINER INNER ANGLE. MAINTENANCE FABRICATED AND INSTALLED R
- [SDR F3LA99087](https://openairdocs.org/sdr/F3LA99087), Jun 28, 1999: SKIN. CRACKED. DEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3
- [SDR F3LA99094](https://openairdocs.org/sdr/F3LA99094), Jun 25, 1999: EXHAUST CASE. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED NR 2 ENGIEN EXHAUST CASE CRACKED AT 3 O'CLOCK STRUT, TOP SIDE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72
- [SDR F3LA99086](https://openairdocs.org/sdr/F3LA99086), Jun 25, 1999: STRINGER. CRACKED. DEN - DURING C-CHECK, INSPECTION REPORTED STRINGER 7R CRACKED ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 360. MAINTENANCE REMOVED DAMAGED AREA, AND FA
- [SDR F3LA99093](https://openairdocs.org/sdr/F3LA99093), Jun 23, 1999: EXHAUST CASE. CRACKED. DEN - DURNG C-CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE STRUT CRACKED AT 9 O'CLOCK POSITION AT ROOT. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W
- [SDR F3LA99092](https://openairdocs.org/sdr/F3LA99092), Jun 23, 1999: EXHAUST CASE. CRACKED. DEN - DURING C-CHECK INSPECTION, REPORTED A 3 INCH CRACK IN THE NR 2 ENGINE EXHAUST CASE UNDER 3 O'CLOCK POSITION STRUT, EXTENDING TOWARD CENTER OF CASE. MAINTE
- [SDR F3LA99091](https://openairdocs.org/sdr/F3LA99091), Jun 22, 1999: IGV. CRACKED. DEN - DURING C-CHECK INSPECTION REPORTED NR 2 ENGINE INLET GUIDE VANE CRACKED AND STOP DRILLED AT 2 O'CLOCK POSITION, AFT WELD. MAINTENANCE WELDED CRACK IAW P/W
- [SDR F3LA99085](https://openairdocs.org/sdr/F3LA99085), Jun 18, 1999: FITTING. CRACKED. DEN - DURING C-4 CHECK INSPECTION, REPORTED LEFT UPPER FORWARD STOP FITTING ON AFT AIRSTAIR DOOR CRACKED. MAINTENANCE INSTALLED REPLACEMENT FITTING PER SRM 51-3
- [SDR F3LA98172](https://openairdocs.org/sdr/F3LA98172), Oct 14, 1998: WIRE. LOOSE. PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA98167](https://openairdocs.org/sdr/F3LA98167), Oct 11, 1998: ACTUATOR. FAILED. DEN - UPON ARRIVAL, FLT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE DURING LANDING. MAINTENANCE REPLACED NR 5 GROUND SPOILER OUTBOARD ACTUATOR, SERVICED
- [SDR F3LA98165](https://openairdocs.org/sdr/F3LA98165), Sep 16, 1998: GASPER FAN. MALFUNCTIONED. PIH - EN ROUTE TO SEA, FLT CREW REPORTED A STRONG ELECTRICAL ODOR IN AFT PASSENGER CABIN. AIRCRAFT WAS DIVERTED TO POCATELLO AND LANDED WITHOUT INCIDENT. MAINTE
- [SDR F3LA98032](https://openairdocs.org/sdr/F3LA98032), Apr 18, 1998: SKIN. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED BULGING SKIN AT AFT CORNER OF CUTOUT AT BS 294.5 WL 148, RBL 24. MAINTENANCE REMOVED CORRODED AREAS. FABRICATED REPLAC
- [SDR F3LA98030](https://openairdocs.org/sdr/F3LA98030), Apr 17, 1998: SKIN. CRACKED. PAE - DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LOWER CORNER OF AFT CARGO DOOR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1, 
- [SDR F3LA98029](https://openairdocs.org/sdr/F3LA98029), Apr 17, 1998: SKIN. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED SKIN PILLOWING AT BS 415-430, STRINGER 18R TO 19R. MAINTENANCE REMOVED A 13 INCH BY 20 INCH CORRODED AREA, FABRICATED 
- [SDR F3LA98031](https://openairdocs.org/sdr/F3LA98031), Apr 16, 1998: LIGHTS. INOPERATIVE. DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA98028](https://openairdocs.org/sdr/F3LA98028), Apr 15, 1998: SKIN. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED BULGE IN SKIN AT BS 1018 BETWEEN STRINGER 27-R AND 28-R. MAINTENANCE REMOVED DAMAGED AREA (7.1 INCH BY 2 INCH). FABRIC
- [SDR F3LA98027](https://openairdocs.org/sdr/F3LA98027), Apr 14, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-R, BS 360-540. MAINTENANCE REMOVED CORRODED AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED 
- [SDR F3LA98026](https://openairdocs.org/sdr/F3LA98026), Apr 10, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 14-R, BS 440-500, AND CRACK IN STRINGER 14-R, BS 440-448. MAINTENANCE REPAIRED CORRODED AREAS, P
- [SDR F3LA98025](https://openairdocs.org/sdr/F3LA98025), Apr 9, 1998: STRINGER. CRACKED. PAE - DURING C-CHECK, INSPECTION REPORTED STRINGER 16-R CRACKED AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE REMOVED A 1 INCH BY 1.
- [SDR F3LA98024](https://openairdocs.org/sdr/F3LA98024), Apr 9, 1998: STRINGER. CRACKED. PAE - DURING C-CHECK INSPECTION, FOUND STRINGER 16L CRACKED AT BS 500B PLUS 19 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS 
- [SDR F3LA98022](https://openairdocs.org/sdr/F3LA98022), Apr 9, 1998: FRAME. CRACKED. PAE - DURING C-CHECK INSPECTION REPORTED, FRAME CRACKED AT BS 360 BETWEEN STRINGER 20R AND 21R. MAINTENANCE REMOVED A 1. INCH BY 3.5 INCH AREA, FABRICATED REPLA
- [SDR F3LA98021](https://openairdocs.org/sdr/F3LA98021), Apr 9, 1998: SKIN. CRACKED. PAE - DURING C-CHECK INSPECTION REPORTED, CRACK AT BS 950 BELOW STRINGER 14R AT EDGE OF SKIN LAP. MAINTENANCE REMOVED A 1 INCH BY 3 INCH AREA, FABRICATED REPLAC
- [SDR F3LA98019](https://openairdocs.org/sdr/F3LA98019), Apr 9, 1998: STRINGER. CRACKED. PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN STRINGER 16R AT BS 500B PLUS 16 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PAR
- [SDR F3LA98018](https://openairdocs.org/sdr/F3LA98018), Apr 9, 1998: STRINGER. CRACKED. PAE - DURING C-CHECK INSPECTION REPORTED, CRACK IN STRINGER 16L AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT
- [SDR F3LA98015](https://openairdocs.org/sdr/F3LA98015), Apr 7, 1998: SKIN. DELAMINATED. PAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FR
- [SDR F3LA98010](https://openairdocs.org/sdr/F3LA98010), Apr 7, 1998: FRAME. CRACKED. DURING C-CHECK, MAINTENANCE REPORTED FRAME CRACKED AT STA 7472, STR 9L. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3. (X)
- [SDR F3LA98023](https://openairdocs.org/sdr/F3LA98023), Apr 6, 1998: STRINGER. CORRODED. PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-L, BS 450-459. MAINTENANCE REMOVED A 3 INCH BY 2.5 INCH AREA, FABRICATED REPLACEMENT PARTS AN
- [SDR F3LA98020](https://openairdocs.org/sdr/F3LA98020), Apr 6, 1998: SKIN. CORRODED. PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON STRINGER 4L SKIN LAP AT BS 500A PLUS 10 INCHES. MAINTENANCE REMOVED A 1.2 INCH BY 2 INCH CORRODED AREA, F
- [SDR F3LA98011](https://openairdocs.org/sdr/F3LA98011), Apr 3, 1998: FLOORBEAM. CORRODED. DURING C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD BS 328 FLOORBEAM, LBL 30-4, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF BS 328 BEAM UPPER CHORD
- [SDR 97ZZZX3892](https://openairdocs.org/sdr/97ZZZX3892), Aug 24, 1997: BATTERY PACK. FAILED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY.
- [SDR F3LA97141](https://openairdocs.org/sdr/F3LA97141), Jul 30, 1997: PRESSURE WEB. CRACKED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EIGHT .5 INCH CRACKS IN LEFT PRESSURE WEB AT STATION 259 AND TWO .5 INCH CRACKS IN RIGHT PRESSURE WEB AT STATIO
- [SDR F3LA97136](https://openairdocs.org/sdr/F3LA97136), Jul 12, 1997: BATTERY PACK. DISCHARGED. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 11 INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHECKED OKAY. (X)
- [SDR F3LA97128](https://openairdocs.org/sdr/F3LA97128), Jun 2, 1997: LIGHT. MALFUNCTIONED. UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD GALLEY DOOR EMERGENCY LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)
- [SDR F3LA97027](https://openairdocs.org/sdr/F3LA97027), Jan 29, 1997: SLIDE. LOW PRESSURE. DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSRUE LOW. REPLACED ESCAPE SLIDE. (M)
- [SDR F3LA97019](https://openairdocs.org/sdr/F3LA97019), Jan 22, 1997: DOUBLER. CORRODED. UPON REMOVAL OF NR 2 DME ANTENNA FOR BS 520 FRAME REMOVAL FOUND CORROSION ON NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0 WL 148.5. REMOVED CORROSION FROM A
- [SDR 97ZZZM203](https://openairdocs.org/sdr/97ZZZM203), Jan 22, 1997: DOUBLER. CORRODED. PAE - UPON REMOVAL OF NR 1 ADF ANTENNA FOR BS 520 FRAME REMOVAL, FOUND CORROSION ON NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. REMOVED CORROSIO
- [SDR F3LA97017](https://openairdocs.org/sdr/F3LA97017), Jan 21, 1997: NOSE CHORD. CORRODED. FOUND CORROSION ON RIGHT LOWER NOSE CHORD HORIZONTAL FLANGE BS 237 TO 250 RBL 18, WL 164. REMOVED RT LOWER NOSE CHORD DUE TO CORROSION WAS BEYOND LIMITS IN A ON
- [SDR F3LA97015](https://openairdocs.org/sdr/F3LA97015), Jan 15, 1997: DELTA BEAM. CRACKED. PAE - FOUND CRACK ON PREVIOUS REPAIR BEHIND RAM AIR DUCT RIGHT SIDE AT BS 574-579, RBL 40, WL 152 ON DELTA BEAM. REMOVED 2 INCH CRACK BY REMOVING DAMAGE AREA, R
- [SDR F3LA97014](https://openairdocs.org/sdr/F3LA97014), Jan 15, 1997: SKIN. GOUGED. PAE - WHILE WORKING ENGINE NR 195 FOUND RT LOWER RAM AIR INTAKE SKIN GOUGED AT BS 500B PLUS 7 STRINGER 24 RT. REMOVED DAMAGED WEB AT BS 500B PLUS7, STRINGER 24 
- [SDR F3LA97013](https://openairdocs.org/sdr/F3LA97013), Jan 15, 1997: FRAME. DAMAGED. FOUND CORROSION ON THE FORWARD SIDE OF THE 520 FRAME IN THE FORWARD CARGO BAY BS 520 LBL 18 TO RBL 14, WL 149. REMOVED DAMAGED FRAME, STRINGER CLIPS, STRINGER 2
- [SDR F3LA97012](https://openairdocs.org/sdr/F3LA97012), Jan 11, 1997: WEB. CORRODED. PAE - FOUND CORROSION IN NOSE WHEEL WELL UPPER HORIZONTAL WEB AROUND RT ACCESS PANEL CUTOUT BS 236 TO 252, LBL 2 TO 16, WL 190. FOUND CORROSION ON NOSE WHEEL WE

All 79: https://openairdocs.org/deregistered/N207AU-2000-02-03/reports.md

## NTSB investigations (1)

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 FTW96LA271](https://openairdocs.org/ntsb/FTW96LA271), Jun 22, 1996: Boeing 737-201 (N207AU), Granite, CO, no damage. Probable cause: An encounter with clear air turbulence.

## FAA accident and incident reports (1)

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.

- [Accident 19960622046049A](https://openairdocs.org/incident/19960622046049A), Jun 22, 1996: Boeing 737201 (N207AU), Granite, CO. (.4)The crew had been forewarned to expect severe turbulence on descent into the denver area. The 'fasten seat belts' sign was turned on, and flight attendants…

## Other aircraft with N207AU

- [Registered now](https://openairdocs.org/aircraft/N207AU): Liberty Aerospace LIBERTY XL-2, S/N 0105, built 2008

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