# N93738: Boeing 727-224, registration cancelled 2000-04-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 12, 2000
- Exported to: Swaziland
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-224](https://openairdocs.org/model/boeing-727-224) (registry code 1384076)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 20666
- Type of aircraft: Fixed wing multi engine
- Certificate issued: October 25, 1988
- Last registry action: November 16, 1999
- Mode S code: AD028C
- 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/N93738
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=93738
- Page: https://openairdocs.org/deregistered/N93738-2000-04-12

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 727-224: https://openairdocs.org/model/boeing-727-224.md

## Service difficulty reports (101, newest 50)

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

- [SDR CALA9802082](https://openairdocs.org/sdr/CALA9802082), Nov 17, 1998: BEARING. WORN. THE NOSE GEAR DOORS OPEN LIGHT ON BOTH THE FORWARD AND SECOND OFFICER'S PANELS WERE ILLUMINATED AFTER GEAR RETRACTION DEPARTING BWI. THE WARNING LIGHTS WERE ACC
- [SDR CALA9801933](https://openairdocs.org/sdr/CALA9801933), Oct 9, 1998: FLOORBEAM. CORRODED. FLOORBEAM TOP HAS SURFACE CORROSION FS 1130 RBL 12-12. REMOVED FASTENERS. CUT OUT ANGLE DAMAGE. FABRICATED NEW ANGLE, SPLICES. FABRICATED NEW FLOORBEAM TREATED 
- [SDR CALA9801932](https://openairdocs.org/sdr/CALA9801932), Oct 9, 1998: SKIN. WORN. RT WING NR 8 SPOILER CENTER CHAFE PAD WORN AND TE WORN/MISSING. DENTS OUT OF LIMITS PER SRM 57-50-1 FIG 5. REMOVED SPOILER PANEL AND SENT OUT FOR REPAIR PER MM 
- [SDR CALA9801931](https://openairdocs.org/sdr/CALA9801931), Oct 9, 1998: FITTING. CORRODED. RIGHT WING TO FUSELAGE AT BS 870 FACE AND BORE HAVE CORROSION. ACCOMPLISHED REPAIR BY OVERSIZE HOLE TO REMOVE CORROSION PER ECRA 5310-63775.
- [SDR CALA9801929](https://openairdocs.org/sdr/CALA9801929), Oct 9, 1998: FITTING. CORRODED. INSPECTION FOUND THE NR 2 AND NR 3 FLAP TRACK FORWARD MOUNT FITTINGS CORRODED. THE FLAP TRACK FITTINGS WERE REPAIRED IAW ECRA 5740-01277.
- [SDR CALA9801928](https://openairdocs.org/sdr/CALA9801928), Oct 9, 1998: FITTING. CORRODED. INSPECTION FOUND RT WING NR 6 AND NR 8 FLAP TRACK ATTACH FITTINGS CORRODED. THE CORROSION WAS REMOVED AND THE FITTINGS WERE REPAIRED IAW ECRA 5740-01277.
- [SDR CALA9801912](https://openairdocs.org/sdr/CALA9801912), Oct 5, 1998: BOTTLE PIN. CORRODED. INSPECTION FOUND RT WING TO FUSELAGE BOTTLE PIN, BUSHING, AND RETAINING BOLT CORRODED AT BS 870. THE BOTTLE PIN, BUSHING, AND RETAINING BOLT WERE REMOVED AND RE
- [SDR CALA9801911](https://openairdocs.org/sdr/CALA9801911), Oct 5, 1998: AILERON TAB. DENTED. INSPECTION FOUND LT INBOARD AILERON TAB DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-31.
- [SDR CALA9801809](https://openairdocs.org/sdr/CALA9801809), Sep 18, 1998: SKIN. DELAMINATED. INSPECTION FOUND RT INBOARD FOREFLAP SKIN DELAMINATED AT LOWER SURFACE INBOARD MOST END. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9801795](https://openairdocs.org/sdr/CALA9801795), Sep 16, 1998: SKIN. CORRODED. INSPECTION FOUND CORROSION IN LT ELEVATOR UPPER TRAILING EDGE SKIN BETWEEN STATIC WICKS. THE CORROSION WAS REMOVED, DOUBLERS WERE INSTALLED IAW SRM 55-20-03.
- [SDR CALA9801794](https://openairdocs.org/sdr/CALA9801794), Sep 16, 1998: PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-
- [SDR CALA9801793](https://openairdocs.org/sdr/CALA9801793), Sep 16, 1998: FITTING. CORRODED. INSPECTION FOUND FITTING CORRODED WHERE RT WING NR 5 FLAP TRACK MOUNTS. THE FITTING AND BUSHING WERE REMOVED AND REPLACED IAW MM 32-11-51, PAGE 401 TO 403 AND M
- [SDR CALA9801792](https://openairdocs.org/sdr/CALA9801792), Sep 16, 1998: CHANNEL. CORRODED. INSPECTION FOUND RT AFT LAV FLOOR WAS HAT CHANNEL CORRODED AT FS 1140, RBL 24 TO 60. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2
- [SDR CALA9801780](https://openairdocs.org/sdr/CALA9801780), Sep 16, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 348, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5 AND 51-10-2.
- [SDR CALA9801779](https://openairdocs.org/sdr/CALA9801779), Sep 16, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND MOUNT HOLES AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS INSTALLED IAW SRM 51-10-2
- [SDR CALA9801769](https://openairdocs.org/sdr/CALA9801769), Sep 15, 1998: ANGLE. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.
- [SDR CALA9801768](https://openairdocs.org/sdr/CALA9801768), Sep 14, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT TOP FLANGE OF INTERCOSTAL THREE INCHES AFT OF FLOOR FRAME FS 970, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INS
- [SDR CALA9801767](https://openairdocs.org/sdr/CALA9801767), Sep 14, 1998: SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL AT FS 1120, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10
- [SDR CALA9801766](https://openairdocs.org/sdr/CALA9801766), Sep 14, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 683 TO 688. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE CORRODED AREA WAS CUT OUT 
- [SDR CALA9801765](https://openairdocs.org/sdr/CALA9801765), Sep 14, 1998: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1034, RBL 12-24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-00 AND 51-10-2.
- [SDR CALA9801745](https://openairdocs.org/sdr/CALA9801745), Sep 14, 1998: PANEL. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 12 SPOILER INBOARD HINGE AREA. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE
- [SDR CALA9801744](https://openairdocs.org/sdr/CALA9801744), Sep 14, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT RT INBOARD MIDFLAP JUST OUTBOARD OF NR 5 FLAP CARRIAGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9801743](https://openairdocs.org/sdr/CALA9801743), Sep 14, 1998: PAD. CORRODED. INSPECTION FOUND CORROSION AT RT WING AFT FALSE SPAR PAD WHERE NR 5 AND NR 6 FLAP TRACKS MOUNT. THE FLAP TRACK MOUNT PADS WERE REMOVED IAW SRM 51-30-2. NEW MOUN
- [SDR CALA9801742](https://openairdocs.org/sdr/CALA9801742), Sep 14, 1998: SKIN. CORRODED. INSPECTION FOUND LT ELEVATOR SKIN UPPER SURFACE CORRODED AROUND STATIC WICK BASE. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-20-03.
- [SDR CALA9801741](https://openairdocs.org/sdr/CALA9801741), Sep 14, 1998: SKIN. CRACKED. INSPECTION FOUND A .75 INCH AND .1093 INCH CRACK IN RT WING LOWER TRAILING EDGE OF INBOARD MIDFLAP, 34 INCHES FROM INBOARD END. THE CRACKS WERE STOP DRILLED IAW
- [SDR CALA9801740](https://openairdocs.org/sdr/CALA9801740), Sep 14, 1998: SKIN. CRACKED. INSPECTION FOUND A .3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHES FROM INBOARD END. A DOUBLER WAS INSTAL
- [SDR CALA9801739](https://openairdocs.org/sdr/CALA9801739), Sep 14, 1998: CHANNEL. CORRODED. INSPECTION FOUND AFT LAV FLOOR HAT CHANNEL CORRODED AT FS 1140-1170, RBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2, PAGE 2
- [SDR CALA9801738](https://openairdocs.org/sdr/CALA9801738), Sep 14, 1998: ANGLE. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN NR 2 SLAT PANEL ATTACH ANGLE BY ANTI-ICE DUCT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IA
- [SDR CALA9801737](https://openairdocs.org/sdr/CALA9801737), Sep 14, 1998: ANGLE. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED 
- [SDR CALA9801736](https://openairdocs.org/sdr/CALA9801736), Sep 14, 1998: TRACK. CORRODED. INSPECTION FOUND NR 4 FLAP TRACK FORWARD CLEVIS CORRODED ON BOTH SIDES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801705](https://openairdocs.org/sdr/CALA9801705), Sep 10, 1998: ANGLE. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STO
- [SDR CALA9801704](https://openairdocs.org/sdr/CALA9801704), Sep 10, 1998: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SR
- [SDR CALA9801703](https://openairdocs.org/sdr/CALA9801703), Sep 10, 1998: DOUBLER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN DOUBLER INSIDE LT INBOARD FLAP AT AFT END OF INBOARD FLAP TRACK CARRIAGE SPINDLE CUTOUT. THE DOUBLER WAS REMOVED AND A NEW D
- [SDR CALA9801702](https://openairdocs.org/sdr/CALA9801702), Sep 10, 1998: RIB. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT O/B MIDFLAP O/B END RIB FORWARD OF MID SPAR. THE CRACK WAS STOP DRILLED. A DOUBLER ANGLE WAS INSTALLED IAW SRM 51-30-2, 
- [SDR CALA9801701](https://openairdocs.org/sdr/CALA9801701), Sep 10, 1998: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN AND RIB DENTED JUST AFT OF NLG AFT DOOR. THE RIB AND SKIN WERE REMOVED AND REPLACED IAW SRM 51-10-1.
- [SDR CALA9801700](https://openairdocs.org/sdr/CALA9801700), Sep 10, 1998: PAD. CORRODED. INSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PA
- [SDR CALA9801699](https://openairdocs.org/sdr/CALA9801699), Sep 10, 1998: TRACK. CORRODED. INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801695](https://openairdocs.org/sdr/CALA9801695), Sep 10, 1998: TRACK. CORRODED. INSPECTION FOUND RT WING NR 8 FLAP TRACK FORWARD ATTACH LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.
- [SDR CALA9801694](https://openairdocs.org/sdr/CALA9801694), Sep 10, 1998: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD BRACKET WHERE RT WING NR 5 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALL
- [SDR CALA9801693](https://openairdocs.org/sdr/CALA9801693), Sep 10, 1998: HAT CHANNEL. CORRODED. INSPECTION FOUND HAT CHANNEL CORRODED AT FS 1150, LBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.
- [SDR CALA9801692](https://openairdocs.org/sdr/CALA9801692), Sep 10, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801691](https://openairdocs.org/sdr/CALA9801691), Sep 10, 1998: SKIN. CORRODED. INSPECTION FOUND RT ELEVATOR SKIN LOWER SURFACE CORRODED. THE CORRODED AREA WAS CUT OUT AND A NEW FITTING AND DOUBLER WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, 
- [SDR CALA9801690](https://openairdocs.org/sdr/CALA9801690), Sep 10, 1998: CARRIAGE. CORRODED. INSPECTION FOUND NR 7 FLAP OUTBOARD FLAP INBOARD CARRIAGE CORRODED. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 57-53-2.
- [SDR CALA9801679](https://openairdocs.org/sdr/CALA9801679), Sep 9, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 22.5 TO 24.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-8 
- [SDR CALA9801678](https://openairdocs.org/sdr/CALA9801678), Sep 9, 1998: ANGLE. CRACKED. INSPECTION FOUND A .375 CRACK IN ANGLE AT INTERCOSTAL AT BS 950A-950B, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.
- [SDR CALA9801677](https://openairdocs.org/sdr/CALA9801677), Sep 9, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1067, RBL 12-24 AND RBL 45-65. THE FLOOR SUPPORTS WERE REMOVED AND A NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1A
- [SDR CALA9801676](https://openairdocs.org/sdr/CALA9801676), Sep 9, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 24-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30
- [SDR CALA9801675](https://openairdocs.org/sdr/CALA9801675), Sep 9, 1998: WEB. CORRODED. INSPECTION FOUND RT WEB CORRODED AT FS 1122, RBL 65. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-2, 51-10-1, PAGE 4, AND 51-30-2.
- [SDR CALA9801674](https://openairdocs.org/sdr/CALA9801674), Sep 9, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT TOP FLANGE SCREW HOLE FS 1050, RBL 35. THE CORRODED AREA WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM
- [SDR CALA9801673](https://openairdocs.org/sdr/CALA9801673), Sep 9, 1998: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-1, AND 51-30-2.

All 101: https://openairdocs.org/deregistered/N93738-2000-04-12/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 FTW76IF096](https://openairdocs.org/ntsb/FTW76IF096), May 25, 1976: Boeing 727 (N93738), San Antonio, TX, incident, minor damage

## FAA accident and incident reports (7)

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 19930720041459I](https://openairdocs.org/incident/19930720041459I), Jul 20, 1993: Boeing 727224 (N93738), Cleveland, OH. Lost a system hydraulic quantity. Landed safely. Replaced a defective hydraulic flex hose on NR2 engine.
- [Incident 19930622023369I](https://openairdocs.org/incident/19930622023369I), Jun 22, 1993: Boeing 727224 (N93738), Houston, TX. Smoke in cockpit and cabin on climb. Returned. Landed overweight safely. Appears compressor seal had failed.
- [Incident 19920106001169I](https://openairdocs.org/incident/19920106001169I), Jan 6, 1992: Boeing 727224 (N93738), Omaha, NE, Minor damage. NR2 engine compressor stall on rotation. Returned. NR2 engine nose dome had separated from N-1TACH drive cover.
- [Incident 19840907053259I](https://openairdocs.org/incident/19840907053259I), Sep 7, 1984: Boeing 727224 (N93738), Chicago. Aircraft diverted and made unscheduled landing because number 1 engine start valve light illuminated.
- [Incident 19800503043689I](https://openairdocs.org/incident/19800503043689I), May 3, 1980: Boeing 727224 (N93738), San Antonio, TX. Windshield cracked in flight. No further incident.
- [Incident 19800319032159I](https://openairdocs.org/incident/19800319032159I), Mar 19, 1980: Boeing 727224 (N93738), Houston, TX. Main hydraulic pressure gauge flickered and dropped to zero. Flap control valve leaking.
- [Incident 19780321010059I](https://openairdocs.org/incident/19780321010059I), Mar 21, 1978: Boeing 727200 (N93738), Tulsa, OK, Substantial damage, 5 fatal. Pilot cut sort during turn onto taxiway. Main gear sank deeply into the mud. Then main collapsed.

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