# N17535: Mcdonnell Douglas DC-9-32, registration cancelled 2001-08-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 29, 2001 - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47111 - Type of aircraft: Fixed wing multi engine - Certificate issued: February 26, 1998 - Last registry action: May 3, 2001 - Mode S code: A12E9F - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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/N17535 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17535 - Page: https://openairdocs.org/deregistered/N17535-2001-08-29 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 Mcdonnell Douglas DC-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 20000426SH015](https://openairdocs.org/sdr/20000426SH015), Mar 31, 2000: JACKSCREW. MAKING METAL. DURING INSPECTION OF THE HORIZONTAL STABILIZER JACKSCREW ASSY, METAL SHAVINGS WERE FOUND WITHIN THE GREASE ON AND AROUND THE JACKSCREW. FURTHER, THE ACME SCREW - [SDR GTIA9901084](https://openairdocs.org/sdr/GTIA9901084), Aug 18, 1999: WIRE. FAILED. MYR - BOTH EMERGENCY NACELLE LIGHTS INOPERATIVE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 333. REPAIRED WIRING AT AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS - [SDR GTIA9900989](https://openairdocs.org/sdr/GTIA9900989), Jun 22, 1999: WIRE. LOOSE. FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRES OUT ON FLOOR ROW EIGHT RESECURED AS NECESSARY. OPERATION CHECK GOOD IAW DC-9 MM - [SDR GTIA9900942](https://openairdocs.org/sdr/GTIA9900942), Jun 22, 1999: WIRE. LOOSE. FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRE OUT OF FLOOR ROW EIGHT. RESECURED AS NECESSARY. OPERATION CHECKS GOOD IAW DC-9 M - [SDR GTIA9800075](https://openairdocs.org/sdr/GTIA9800075), Jun 26, 1998: LIGHT. INOPERATIVE. OKC - FLT 902 - EMERGENCY FLOOR TRACK BROKE BETWEEN ROWS 11-15. REPAIRED FLOOR TRACK AND LIGHTING IAW DC-9 MM 33-51. OPERATIONAL CHECKS GOOD. (X) - [SDR GTIA9800020](https://openairdocs.org/sdr/GTIA9800020), Feb 4, 1998: SLIDE. FELL OFF. MAIN CABIN DOOR SLIDE PACK FELL OFF. REINSTALLED MAIN CABIN DOOR SLIDE IAW DC-9 MM 25-62-0, INSTALLATION CHECKS GOOD. RII ACCOMPLISHED. (M) - [SDR GTIA9700414](https://openairdocs.org/sdr/GTIA9700414), Dec 19, 1997: BATTERY PACK. DISCHARGED. DTW - FLT 610 - ON DAILY INSPECTION, LEFT AND RIGHT EMERGENCY NACELLE LIGHTS WOULD NOT ILLUMINATE. REPLACED LEFT AND RIGHT EMERGENCY NACELLE LIGHTS BATTERY PACK - [SDR GTIA9700413](https://openairdocs.org/sdr/GTIA9700413), Dec 15, 1997: SLIDE. FELL OFF. DTW - FLT 841 - DURING DAILY INSPECTION, FOUND GALLEY DOOR EMERGENCY SLIDE HAD FALLEN OFF. INSTALLED GALLEY DOOR EMERGENCY SLIDE IAW DC9 MM 25-62-0. RII INSPECT - [SDR GTIA9700405](https://openairdocs.org/sdr/GTIA9700405), Nov 25, 1997: FIRE LOOP. MALFUNCTIONED. CLIMBING THROUGH 8,000 FEET THE 'A' LOOP LIGHT CAME ON AS WELL AS THE LIGHT FOR NR 1 ENGINE, WENT TO 'B', TEST OK. GROUND OPS CHECKED NR 1 ENGINE FIRE LOOP SYST - [SDR CALA9701119](https://openairdocs.org/sdr/CALA9701119), Jul 19, 1997: CONNECTOR. DIRTY. THE LT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE EMERGENCY GEAR EXTENSION LEVER WAS - [SDR CALA9601424](https://openairdocs.org/sdr/CALA9601424), Oct 8, 1996: ACTUATOR. INOPERATIVE. WHEN GEAR WAS RETRACTED ON TAKEOFF, THE GEAR DOOR OPEN AND RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. APPROXIMATELY 15 SECONDS LATER THE SPEED BRAKE SP - [SDR CAL951067](https://openairdocs.org/sdr/CAL951067), Nov 26, 1995: LATCH SPRING. LACK OF LUBE. FLT NR 1090 - ATL - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. THE RE - [SDR CAL951020](https://openairdocs.org/sdr/CAL951020), Oct 24, 1995: SKIN. CORRODED. HOU - INSPECTION FOUND CORROSION ON SKIN AT STA 250 BELT FRAME, LONGERON 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (X) - [SDR CAL950991](https://openairdocs.org/sdr/CAL950991), Oct 24, 1995: FITTING. CORRODED. HOU - INSPECTION FOUND INTERGRANULAR CORROSION AT BELTFRAME STATION 832, FITTING TO RIGHT CUSP. THE FITTING WAS REPLACED IAW SRM 51-30-0. (M) - [SDR CAL951055](https://openairdocs.org/sdr/CAL951055), Oct 21, 1995: BULKHEAD. CORRODED. HOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALL - [SDR CAL951023](https://openairdocs.org/sdr/CAL951023), Oct 19, 1995: DOUBLER. CORRODED. HOU - INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 218, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) - [SDR CAL951022](https://openairdocs.org/sdr/CAL951022), Oct 19, 1995: BRACKET. CORRODED. HOU - INSPECTION FOUND CABIN FLOOR SUPPORT BRACKET AT STA 160, AND 8 INCHES - 10 INCHES, LEFT OF CENTERLINE CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW S - [SDR CAL951021](https://openairdocs.org/sdr/CAL951021), Oct 19, 1995: BELT FRAME. CRACKED. HOU - INSPECTION FOUND A .25 INCH CRACK COMING FROM HI-LOCK HOLE ON BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED SECTION OF BELT FRAME WAS CUT OUT AND A NEW - [SDR CAL950993](https://openairdocs.org/sdr/CAL950993), Oct 19, 1995: FRAME. CRACKED. HOU - INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM FASTENER HOLE ABOVE FLOOR ON FRAME AT STATION 813. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-03. (M) - [SDR CAL950992](https://openairdocs.org/sdr/CAL950992), Oct 19, 1995: FLOOR SUPPORTS. CORRODED. HOU - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STATION 200. THE CORROSION EXTENDED THE FULL LENGTH FROM LEFT TO RIGHT SIDE OF FUSELAGE. FOUR FLOOR - [SDR CAL950988](https://openairdocs.org/sdr/CAL950988), Oct 19, 1995: FRAME. CRACKED. HOU - INSPECTION FOUND A 3 INCH CRACK EXTENDING FROM FASTENER IN FRAME AT STATION 794, STRINGER 18L. THE FRAME WAS REPAIRED IAW SRM 53-11-3, FIGURE 1. (M) - [SDR CAL951057](https://openairdocs.org/sdr/CAL951057), Oct 18, 1995: SKIN. CRACKED. HOU - INSPECTION FOUND TWO .75 INCH CRACKS AT RIVETS IN SKIN LAP AT STA 1038 ABOVE RIGHT PYLON. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE - [SDR CAL951056](https://openairdocs.org/sdr/CAL951056), Oct 18, 1995: SKIN. CRACKED. HOOU - INSPECTION FOUND A .75 INCH CRACK IN SKIN LAP AT STATION 1038 ABOVE LEFT PYLON. THE SKIN CRACK WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW - [SDR CAL951024](https://openairdocs.org/sdr/CAL951024), Oct 18, 1995: LONGERON. CORRODED. HOU - INSPECTION FOUND LONGERON 30 AT STA 218 CORRODED IN TWO. A LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02. (X) - [SDR CAL950995](https://openairdocs.org/sdr/CAL950995), Oct 18, 1995: LONGERON. CRACKED. HOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 8L AT STATION 446. THE LONGERON WAS REPAIRED IAW SRM 53-02. (M) - [SDR CAL951053](https://openairdocs.org/sdr/CAL951053), Oct 17, 1995: SPLICE. CRACKED. HOU - INSPECTION FOUND A 4 INCH CRACK IN LEADING EDGE SPLICE BETWEEN NR 6 AND NR 7 SLAT TRACK. THE LEADING EDGE SPLICE WAS REPAIRED IAW ECRA 5710-01701. (M) - [SDR CAL950990](https://openairdocs.org/sdr/CAL950990), Oct 17, 1995: LE SPLICE. CRACKED. HOU - INSPECTION FOUND A 1 INCH CRACK IN LEADING EDGE SPLICE BETWEEN THE NR 3 AND NR 4 SLAT TRACK. A DOUBLER WAS INSTALLED IAW ECRA 5710-01697. (M) - [SDR CAL950989](https://openairdocs.org/sdr/CAL950989), Oct 17, 1995: SPAR CAP. CORRODED. HOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M) - [SDR CAL951054](https://openairdocs.org/sdr/CAL951054), Oct 15, 1995: DOOR JAMB. CRACKED. HOU - INSPECTION FOUND A 2 INCH CRACK AT LEFT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03176 AND EA 653A006. (M - [SDR CAL950717](https://openairdocs.org/sdr/CAL950717), Aug 13, 1995: BEAM. CORRODED. IAH - DURING INSPECTION, FOUND CORROSION ON LONGITUDINAL BEAM AT FORWARD AIRSTAIR CUTOUT BETWEEN STATION 160 AND 200. THE LONGITUDINAL BEAM WAS REMOVED AND REPL - [SDR CAL950716](https://openairdocs.org/sdr/CAL950716), Aug 13, 1995: SKIN. CRACKED. IAH - DURING INSPECTION, FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD AIRSTAIR DOOR CUTOUT. A REPAIR WAS FABRICATED AND INSTALLED IAW - [SDR CAL950306](https://openairdocs.org/sdr/CAL950306), Apr 20, 1995: SKIN. CRACKED. IAH - A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 965R, THREE INCHES ABOVE L15. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B. (W) ## FAA accident and incident reports (2) 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 19981230044169I](https://openairdocs.org/incident/19981230044169I), Dec 30, 1998: Doug DC932 (N17535), Minneapolis, MN. (-5) Flt. 900 reported a gear problem to msp ATCT while inbound to msp. Emergency was standing by and aircraft landed without incident. Aircraft log write-up… - [Incident 19931220049649I](https://openairdocs.org/incident/19931220049649I), Dec 20, 1993: Doug DC932 (N17535), Baltimore, MD. Left outboard tire failed on rollout. Changed both left tires. Suspect transient in anti-skid system. ## Other aircraft with N17535 - [Cancelled 2026-02-04](https://openairdocs.org/deregistered/N17535-2026-02-04): Schweizer 269C-1, S/N 0225, built 2005. Exported to South Africa. Owner: [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper) --- 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.