# N14564: Mcdonnell Douglas DC-9-31, registration cancelled 1999-12-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 8, 1999 - Exported to: Venezuela - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-31](https://openairdocs.org/model/mcdonnell-douglas-dc-9-31) (registry code 302206A) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47490 - Type of aircraft: Fixed wing multi engine - Certificate issued: December 8, 1992 - Last registry action: August 31, 1998 - Mode S code: A0B88A - 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: 40.7608° N, 111.8910° W: Placed by OpenAirDocs: center of Salt Lake City, UT, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14564 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14564 - Page: https://openairdocs.org/deregistered/N14564-1999-12-08 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 Mcdonnell Douglas DC-9-31: https://openairdocs.org/model/mcdonnell-douglas-dc-9-31.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901094](https://openairdocs.org/sdr/CALA9901094), Aug 26, 1999: CONTROL CABLE. BROKEN. A LOUD BANG WAS HEARD UPON GEAR RETRACTION AND THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED W - [SDR CALA9801571](https://openairdocs.org/sdr/CALA9801571), Aug 27, 1998: LIGHT. INOPERATIVE. THE R-1 DOOR EMERGENCY EVACUATION SLIDE FAILED SLIDE LIGHT TEST. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED. - [SDR CALA9801568](https://openairdocs.org/sdr/CALA9801568), Aug 27, 1998: CLIPS. OUT OF ADJUST. THE FORCE REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS WAS LOW AT 15 POUNDS. THE CLIPS WERE REPLACED AND ADJUSTED IAW MM 53-50-3. - [SDR CALA9801524](https://openairdocs.org/sdr/CALA9801524), Aug 24, 1998: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT AFT BAGGAGE BIN STA 775, LONGERON 30 TO 29R. A DOUBLER WAS INSTALLED IAW ECRA 5331-01028. - [SDR CALA9801499](https://openairdocs.org/sdr/CALA9801499), Aug 21, 1998: SPAR CAP. CORRODED. INSPECTION FOUND RT WING AFT LOWER SPAR CAP CORRODED AT WS XRS 364.5. THE AFT LOWER SPAR CAP WAS REPAIRED IAW SRM 57-09, FIGURE 11. - [SDR CALA9801477](https://openairdocs.org/sdr/CALA9801477), Aug 18, 1998: LONGERON. CRACKED. INSPECTION FOUND A CRACK IN LONGERON 16R AT RT LAV WALL, STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18, PAGE 48. - [SDR CALA9801476](https://openairdocs.org/sdr/CALA9801476), Aug 18, 1998: BELTFRAME. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN BELTFRAME AT STA 408, LONGERON 5L. THE BELTFRAME WAS REPAIRED IAW SRM 53-03, FIGURE 4. - [SDR CALA9801472](https://openairdocs.org/sdr/CALA9801472), Aug 17, 1998: LONGERON. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT LT LAV WALL STA 965. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 18. - [SDR CALA9801470](https://openairdocs.org/sdr/CALA9801470), Aug 16, 1998: MEMBRANE. CORRODED. INSPECTION FOUND CUSP MEMBRANE CORRODED AT STA 996, LONGERON 18L. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 25. - [SDR CALA9801469](https://openairdocs.org/sdr/CALA9801469), Aug 16, 1998: LONGERON. CRACKED. INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN LONGERON 17R AT LAV WALL STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGUR - [SDR CALA9801471](https://openairdocs.org/sdr/CALA9801471), Aug 15, 1998: BULKHEAD DOUBLER. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN AFT PRESSURE BULKHEAD DOUBLER ON LT SIDE BELOW DOOR OPENING. REPAIRED IAW SRM 53-05, FIGURE 39. - [SDR CALA9700671](https://openairdocs.org/sdr/CALA9700671), May 8, 1997: SKIN. CRACKED. INSPECTION FOUND A 2 AND 1.2 CRACK IN FUSELAGE SKIN AT STA 1143, LONGERON 14 AND 16R. THE CRACKS WERE STOP DRILLED AND REPAIR DOUBLER WAS INSTALLED IAW SRM 53-0 - [SDR CALA9601545](https://openairdocs.org/sdr/CALA9601545), Nov 2, 1996: RESTRICTOR. CLOGGED. THE SLATS DID NOT EXTEND SYMMETRICALLY ON APPROACH. A SIGNIFICANT ROLL TO THE RIGHT OCCURRED AT SLATS EXTENDED/FLAPS 5 DEGREES, WHICH TOOK 10 DEGREES LEFT TURN - [SDR CALA9601262](https://openairdocs.org/sdr/CALA9601262), Sep 2, 1996: POSN SWITCH. OUT OF ADJUST. THE GEAR DOOR OPEN LIGHT REMAINED ON WITH GEAR RETRACTED AFTER TAKEOFF. CYCLING THE GEAR WAS NO HELP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO IAH THE LIGHT EXT - [SDR CALA9601273](https://openairdocs.org/sdr/CALA9601273), Aug 22, 1996: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK ON REPAIR ANGLE FOR FORMER IN LEFT KEEL BEAM AREA, STA 637.5. A NEW ANGLE WAS INSTALLED IAW SRM 53-03. - [SDR CALA9601274](https://openairdocs.org/sdr/CALA9601274), Aug 21, 1996: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FITTING IN LEFT KEEL BEAM AREA, STA 622. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-03. - [SDR CALA9601272](https://openairdocs.org/sdr/CALA9601272), Aug 21, 1996: BULKHEAD FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN AFT PIT FORWARD BULKHEAD FRAME AT STA 756, LONGERON 26R. A DOUBLER WAS INSTALLED IAW SRM 53-01. - [SDR CALA9601271](https://openairdocs.org/sdr/CALA9601271), Aug 21, 1996: DOUBLER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN DOUBLER JUST AFT OF STA 408, LONGERON 30. A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9601270](https://openairdocs.org/sdr/CALA9601270), Aug 20, 1996: BEAM. CRACKED. INSPECTION FOUND ONE CRACK IN EACH OF MAIN CABIN DOOR BEAMS NR 1, 5 AND 7. THE CRACKS WERE .25 TO 1 INCH IN LENGTH. THE CRACKS WERE REPAIRED IAW SRM 52-05, FIGU - [SDR CALA9601266](https://openairdocs.org/sdr/CALA9601266), Aug 20, 1996: SKIN. CRACKED. INSPECTION FOUND TWO 2 INCH CRACKS IN RUDDER SKIN, LOCATED AT TOP LEFT AND RIGHT SIDE OF RUDDER. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SR - [SDR CALA9601267](https://openairdocs.org/sdr/CALA9601267), Aug 19, 1996: LATCHES. BINDING. THE TAILCONE FAILED DROP CHECK AT 50+ POUNDS WHEN USING THE EXTERIOR RELEASE HANDLE. THE TAILCONE LATCHES WERE LUBRICATED AND OPERATION CHECKED GOOD. - [SDR CALA9601151](https://openairdocs.org/sdr/CALA9601151), Aug 11, 1996: UP/DNLK SWITCH. INOPERATIVE. WHEN GEAR WAS EXTENDED ON APPROACH TO BHM NEITHER THE RED TRANSIT OR GREEN DOWN INDICATION LIGHTS FOR THE NOSE GEAR ILLUMINATED. THE GEAR WAS CYCLED WITH NO CHA - [SDR CAL960201](https://openairdocs.org/sdr/CAL960201), Feb 26, 1996: DNLOCK SWITCH. INOPERATIVE. FLT NR 1819 - IAH - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG GREEN LIGHT NOT ILLUMINATING WHEN GEAR WAS EXTENDED FOR LANDING. CYCLING THE GEAR CAUSED THE LIG - [SDR CAL950932](https://openairdocs.org/sdr/CAL950932), Oct 7, 1995: ANGLE. CORRODED. STA 31J - INSPECTION FOUND CORROSION ON L-ANGLE ATTACHED TO FLOOR BEAM AT FS 926, LBL 25. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW - [SDR CAL950732](https://openairdocs.org/sdr/CAL950732), Aug 18, 1995: RECEPTACLE. BURNED. FLT NR 1579 - FLL - THE CREW REPORTED AN ODOR IN MID CABIN PRIOR TO LANDING AT FLL. MAINTENANCE FOUND PSU RECEPTACLE BETWEEN ROW 12-14 RT BURNED. THE RECEPTACLE - [SDR CAL950475](https://openairdocs.org/sdr/CAL950475), Jun 11, 1995: TRANSFORMER RECT. INOPERATIVE. FLT NR 1279 - IAH - THE NR 2 TRANSFORMER RECTIFIER FAILED ON ROTATION LEAVING IAH (NR 1 RIGHT TRANSFORMER RECTIFIER WAS ON PLACARD). THE DC BUS OFF LIGHT ILLUMI ## Other aircraft with N14564 - [Registered now](https://openairdocs.org/aircraft/N14564): Airbus S A S A321-271NX, S/N 12977, built 2026 - [Cancelled 1971-06-14](https://openairdocs.org/deregistered/N14564-1971-06-14): Aeronca C-3, S/N A-515. Owner: [Sandiego Aero-Space Museum Inc](https://openairdocs.org/faa-owner/SANDIEGO%20AERO-SPACE%20MUSEUM%20INC), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.