# N43537: 1967 Mcdonnell Douglas DC-9-32, registration cancelled 2002-07-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 30, 2002 - 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) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47112 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 1, 1981 - Certificate issued: March 6, 1998 - Last registry action: May 24, 2001 - Mode S code: A53892 - 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/N43537 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=43537 - Page: https://openairdocs.org/deregistered/N43537-2002-07-30 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901100](https://openairdocs.org/sdr/CALA9901100), Aug 29, 1999: WIRE. BROKEN. INSPECTION FOUND FORWARD SECTION OF EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE FOUND A BROKEN LIGHT SOCKET WIRE. A NEW SOCKET ASSEMBLY WAS SPLICED IN AND - [SDR CALA9900708](https://openairdocs.org/sdr/CALA9900708), Jun 18, 1999: BATTERIES. DISCHARGED. INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERIES IN BATTERY PACK WERE REPLACED AND EMERGENCY LIGHT OPERATION CHECKED GOOD. - [SDR CALA9900194](https://openairdocs.org/sdr/CALA9900194), Feb 25, 1999: WIRE. BROKEN. THE EMERGENCY AISLE PATH LIGHTS DID NOT ILLUMINATE WHEN ON POSITION WAS SELECTED DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A BROKEN WIRE ON SWITCH IN COCKPIT. - [SDR CALA9900162](https://openairdocs.org/sdr/CALA9900162), Feb 17, 1999: VANE. CORRODED. INSPECTION FOUND LT WING FLAP O/B FIXED VANE I/B END LOWER SURFACE CORRODED WITH RIVETS PULLING THROUGH. THE LT O/B FLAP VANE WAS REMOVED AND REPLACED IAW MM 27 - [SDR CALA9900156](https://openairdocs.org/sdr/CALA9900156), Feb 15, 1999: BLKHD BRACKET. CRACKED. INSPECTION FOUND TWO AFT CARGO FORWARD BULKHEAD SPLICE BRACKETS WITH .5 INCH CRACKS. NEW FITTINGS WERE INSTALLED IAW SRM 51-10-1 AND 51-00-00. - [SDR CALA9900155](https://openairdocs.org/sdr/CALA9900155), Feb 15, 1999: SUPPORT. CORRODED. INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT TEE CHANNEL CORRODED AT STA 160, LBL 8. THE FLOOR SUPPORT T CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALL - [SDR CALA9900154](https://openairdocs.org/sdr/CALA9900154), Feb 15, 1999: WIRE. BROKEN. EMERGENCY LIGHT BATTERY PACKS FAILED TEST AT LT LAV AND FORWARD ENTRY. REPAIRED BROKEN WIRES, SECURED LOOSE GROUND, AND TIGHTENED BATTERY CONTACTS. OPERATION CH - [SDR CALA9900151](https://openairdocs.org/sdr/CALA9900151), Feb 13, 1999: FLOORBEAM. CHAFED. INSPECTION FOUND A HOLE CHAFED IN LOWER CHORD OF FORWARD CARGO COMPARTMENT FLOORBEAM AT FS 389, RBL 2. A REPAIR WAS INSTALLED IAW SRM 53-05-00, FIGURE 20A, PAGE - [SDR CALA9900150](https://openairdocs.org/sdr/CALA9900150), Feb 13, 1999: SKIN. DEBONDED. INSPECTION FOUND LT WING LOWER SKIN PANEL DEBONDED AROUND SCREW HOLE FORWARD OF OUTER WHEEL WELL AREA. THE SKIN PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW - [SDR CALA9900149](https://openairdocs.org/sdr/CALA9900149), Feb 13, 1999: PANEL. DEBONDED. INSPECTION FOUND THE LT WING UPPER T/E FIXED PANEL DEBONDED WITH SURFACE CORROSION ON BOTTOM, JUST I/B OF AILERON. THE PANEL WAS REMOVED, REPAIRED, AND REINSTAL - [SDR CALA9900148](https://openairdocs.org/sdr/CALA9900148), Feb 13, 1999: VANE. DENTED. INSPECTION FOUND LT WING FLAP AFT MOVEABLE VANE DENTED AND ONE SPOT WORN THROUGH AT LOWER SURFACE NEAR I/B END. THE FLAP VANE WAS REMOVED AND REPLACED IAW MM 27 - [SDR CALA9900141](https://openairdocs.org/sdr/CALA9900141), Feb 12, 1999: RIB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT APU DOOR INNER RIB. THE RIB WAS REPAIRED IAW SRM 52-01-00, FIGURE 2 AND 51-10-3. - [SDR CALA9900140](https://openairdocs.org/sdr/CALA9900140), Feb 12, 1999: TAB. DELAMINATED. INSPECTION FOUND LT ELEVATOR CONTROL TAB DELAMINATED ON UPPER SURFACE. THE LT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-00 AND 27-30-3. - [SDR CALA9900139](https://openairdocs.org/sdr/CALA9900139), Feb 12, 1999: FITTING. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FITTING OF FORWARD ENTRY DOOR AT UPPER AFT STOP PAD AREA. THE FASTENERS AND FITTING WERE REMOVED AND THE CRACK WAS STOP DRI - [SDR CALA9900138](https://openairdocs.org/sdr/CALA9900138), Feb 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT T CHANNEL CORRODED BETWEEN STA 160 AND 229, BL 0. THE CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW - [SDR CALA9900121](https://openairdocs.org/sdr/CALA9900121), Feb 8, 1999: DOOR. OUT OF ADJUST. THE LT AFT OVERWING EMERGENCY EXIT DOOR FAILED UNLOCK FORCE TEST. THE LATCH BAR SCREWS WERE ADJUSTED TO OBTAIN THE REQUIRED FORCE TO UNLOCK THE EXIT DOOR IAW MM - [SDR CALA9801934](https://openairdocs.org/sdr/CALA9801934), Oct 9, 1998: LIGHT. CRACKED. FWD AISLE PATH LIGHTING COVER IN FIRST CLASS NEEDS TO BE RE-SECURED. REPLACED FWD SECTION OF BASE AND END CAP ASSY. - [SDR CALA9601530](https://openairdocs.org/sdr/CALA9601530), Oct 25, 1996: SKIN. PUNCTURED. A MAINTENANCE LIFT TRUCK STRUCK THE FUSELAGE CREATING A HOLE THROUGH SKIN AT STA 140.038, 3 INCHES BELOW LONGERON 20R. THE HOLE WAS APPROXIMATELY .875 L BY .5 W - [SDR CALA9601298](https://openairdocs.org/sdr/CALA9601298), Sep 10, 1996: RELAY. CRACKED. THE AIRCRAFT HAD A HISTORY OF THE GPWS GIVING A TOO LOW GEAR WARNING AT LOW ALTITUDES DURING LANDING, WHICH RESULTED IN TWO INSTANCES OF A GO-AROUND. THE WARNIN - [SDR CAL960610](https://openairdocs.org/sdr/CAL960610), May 14, 1996: BATTERIES. DISCHARGED. CLE - FLT 1144 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY BATTERIES WERE FOUND AT FAULT. THE NICAD BATTERIES IN POWER SUPPLY WERE R - [SDR CAL951034](https://openairdocs.org/sdr/CAL951034), Nov 5, 1995: SKIN. CRACKED. IAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, - [SDR 97ZZZX4197](https://openairdocs.org/sdr/97ZZZX4197), Oct 19, 1995: STEERING PISTON. PIN SHEARED. ONE EACH OF TWO STEERING PISTON PINS THAT GO THROUGH COLLAR, PN 5920605-503, WAS SHEARED INSIDE THE COLLAR. THE BREAK WAS IN THE BOTTOM THIRD OF THE SHANK. THER - [SDR CAL950939](https://openairdocs.org/sdr/CAL950939), Oct 18, 1995: ACTUATOR PIN. SHEARED. DHN - INSPECTION FOUND THE NLG RIGHT NOSE STEERING ACTUATOR PIN SHEARED. THE STEERING CONTROL LEVER ASSEMBLY AND RIGHT NOSE STEERING CYLINDER ASSEMBLY WERE REMO ## Other aircraft with N43537 - [Registered now](https://openairdocs.org/aircraft/N43537): Hale Gerald E RANS-S12XL, S/N 04040986, built 2006 - [Cancelled 1984-05-15](https://openairdocs.org/deregistered/N43537-1984-05-15): Piper PA-32R-301T, S/N 32R-8429011, built 1984. Exported to Switzerland. Owner: [Globe Aero Limited Inc](https://openairdocs.org/faa-owner/GLOBE%20AERO%20LIMITED%20INC), [Lakeland, FL](https://openairdocs.org/faa-place/FL/Lakeland) --- 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.