# N15525: Mcdonnell Douglas DC-9-32, registration cancelled 2000-10-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 18, 2000 - Exported to: Democratic Republic of the Congo - 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: 47531 - Type of aircraft: Fixed wing multi engine - Certificate issued: May 7, 1993 - Last registry action: May 18, 1999 - Mode S code: A0DF7E - Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7533° N, 95.4129° W: Placed by OpenAirDocs at the center of ZIP code 77019, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N15525 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15525 - Page: https://openairdocs.org/deregistered/N15525-2000-10-18 From the FAA registry file of November 4, 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900091](https://openairdocs.org/sdr/CALA9900091), Jan 28, 1999: POWER SUPPLY. INOP. THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE B5-25 POWER SUPPLY AT STA 635 WAS REMOVED AND REPLACED. - [SDR CALA9801390](https://openairdocs.org/sdr/CALA9801390), Aug 5, 1998: SKIN. CRACKED. INSPECTION FOUND AFT CARGO BARRIER DOOR SKIN CRACKED AND DELAMINATED ON INBOARD SIDE WITH A PUNCTURE ON OUTBOARD SIDE. THE DOOR WAS DISASSEMBLED. THE OUTER SKIN - [SDR CALA9801388](https://openairdocs.org/sdr/CALA9801388), Aug 5, 1998: SKIN. CRACKED. INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED - [SDR CALA9801389](https://openairdocs.org/sdr/CALA9801389), Aug 4, 1998: SKIN. CORRODED. INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-0, 51- - [SDR CALA9801382](https://openairdocs.org/sdr/CALA9801382), Jul 31, 1998: STRAP. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-0. - [SDR CALA9801381](https://openairdocs.org/sdr/CALA9801381), Jul 31, 1998: BRACKET. GOUGED. INSPECTION FOUND NR 1 THRUST REVERSER PANEL BRACKET GOUGED. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2A, AND 5 - [SDR CALA9801380](https://openairdocs.org/sdr/CALA9801380), Jul 31, 1998: ANGLE. CRACKED. INSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, A - [SDR CALA9801370](https://openairdocs.org/sdr/CALA9801370), Jul 30, 1998: PANEL. CORRODED. INSPECTION FOUND CORROSION ON TOP SIDE LEFT WING PANEL NR 1122A. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, PAGE 8, 57-31-1, 51-10-3, AND 51-3 - [SDR CALA9801365](https://openairdocs.org/sdr/CALA9801365), Jul 29, 1998: SPLICE. CORRODED. INSPECTION FOUND FLOOR PANEL SPLICE PLATE IN AFT CARGO PIT AT STA 935 CORRODED. A NEW FLOOR PANEL SPLICE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND - [SDR CALA9801364](https://openairdocs.org/sdr/CALA9801364), Jul 29, 1998: PANEL. GOUGED. INSPECTION FOUND RT WING LEADING EDGE PANEL NR 1248 GOUGED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2. - [SDR CALA9801363](https://openairdocs.org/sdr/CALA9801363), Jul 29, 1998: ANGLE. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE - [SDR CALA9801362](https://openairdocs.org/sdr/CALA9801362), Jul 29, 1998: FLOOR. CRACKED. INSPECTION FOUND AFT CARGO FLOOR PANEL AT STA 756-935 CRACKED AND WORN IN SEVERAL PLACES. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0. - [SDR CALA9701227](https://openairdocs.org/sdr/CALA9701227), Aug 14, 1997: LONGERON. CRACKED. INSPECTION FOUND A 1 CRACK IN LONGERON 17R AT STA 965. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18. - [SDR CAL960042](https://openairdocs.org/sdr/CAL960042), Jan 14, 1996: DRIVE MECHANISM. BROKEN. FLT NR 1787 - IAH - LEFT LEADING EDGE SLAT WOULD NOT RETRACT AFTER LANDING AT IAH. NO IN FLIGHT ABNORMALITIES WERE OBSERVED. MAINTENANCE FOUND THE LEFT OUTBOARD - [SDR CAL950844](https://openairdocs.org/sdr/CAL950844), Sep 20, 1995: JAMB DOOR. DENTED. HOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M) - [SDR CAL950842](https://openairdocs.org/sdr/CAL950842), Sep 17, 1995: SKIN. CRACKED. HOU - INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038 BETWEEN LONGERON 10R AND 11R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE - [SDR CAL950845](https://openairdocs.org/sdr/CAL950845), Sep 16, 1995: LONGERON. CORRODED. HOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS S - [SDR CAL950852](https://openairdocs.org/sdr/CAL950852), Sep 15, 1995: BLKHD WEB. CRACKED. HOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M - [SDR CAL950833](https://openairdocs.org/sdr/CAL950833), Sep 8, 1995: ANGLE. CRACKED. HOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT WHEEL WELL ATTACH ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30. (M) - [SDR CAL950843](https://openairdocs.org/sdr/CAL950843), Sep 7, 1995: BRACKET. CRACKED. HOU - INSPECTION FOUND A .75 INCH CRACK IN NR 4 LEFT FLAP HINGE OUTBOARD BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M) - [SDR CAL950839](https://openairdocs.org/sdr/CAL950839), Sep 7, 1995: CUSP. CORRODED. HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 165 JUST FORWARD OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FI - [SDR CAL950838](https://openairdocs.org/sdr/CAL950838), Sep 7, 1995: CUSP. CORRODED. HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 200 JUST AFT OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE - [SDR CAL950834](https://openairdocs.org/sdr/CAL950834), Sep 7, 1995: BRACKET. CRACKED. HOU - INSPECTION FOUND A .5 INCH CRACK IN THE RIGHT FLAP NR 4 FLAP HINGE INBOARD AND OUTBOARD BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CAL950832](https://openairdocs.org/sdr/CAL950832), Sep 6, 1995: JAMB. CORRODED. HOU - INSPECTION FOUND CORROSION ON FORWARD BAGGAGE BIN DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44, PAGE 105. (M) ## Other aircraft with N15525 - [Cancelled 1970-12-30](https://openairdocs.org/deregistered/N15525-1970-12-30): Miller P D Y-1S, S/N 310. Owner: [Saloky William D](https://openairdocs.org/faa-owner/SALOKY%20WILLIAM%20D), [Phillipsburg, NJ](https://openairdocs.org/faa-place/NJ/Phillipsburg) --- 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.