# N16815: 1982 Douglas DC-9, registration cancelled 2002-09-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 17, 2002 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Douglas DC-9](https://openairdocs.org/model/douglas-dc-9) (registry code 3022002) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Serial number: 49113 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: June 7, 1982 - Certificate issued: June 20, 1990 - Last registry action: June 10, 2002 - Mode S code: A111FF - Owner when cancelled: [Eal Delaware Xi Corp](https://openairdocs.org/faa-owner/EAL%20DELAWARE%20XI%20CORP) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16815 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16815 - Page: https://openairdocs.org/deregistered/N16815-2002-09-17 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 Douglas DC-9: https://openairdocs.org/model/douglas-dc-9.md ## Service difficulty reports (86, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0200001](https://openairdocs.org/sdr/CALA0200001), Jan 2, 2002: FUSE. BLOWN. INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROW 5-12 INOPERATIVE. MAINTENANCE FOUND FUSE BLOWN IN BATTERY CHARGER AND WIRING AT ROW 5 SHORTED TO THE SEAT - [SDR CALA0100764](https://openairdocs.org/sdr/CALA0100764), Aug 19, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND MAIN CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1117-1174. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100761](https://openairdocs.org/sdr/CALA0100761), Aug 15, 2001: FLOOR PANEL. PUNCTURED. INSPECTION FOUND CABIN FLOOR PANEL PUNCTURED AT FS 256-313. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1 AND ECRA 5320-01265. - [SDR CALA0100746](https://openairdocs.org/sdr/CALA0100746), Aug 8, 2001: INTERCOSTAL. CRACKED. INSPECTION FOUND A 7" CRACK IN R-1 DOOR INNER INTERCOSTA UNDER HINGE ATTACH POINT. THE R-1 DOOR WAS REMOVED IAW MM 52-41-00. THE CRACK WAS STOP DRILLED AND A RE - [SDR CALA0100745](https://openairdocs.org/sdr/CALA0100745), Aug 7, 2001: PAN. GOUGED. INSPECTION FOUND R-1 DOOR LOWER PAN GOUGED AT RIVNUTS. THE PAN SUPPORT WAS REMOVED FOR ACCESS IAW SRM 51-30-02. A REPAIR ANGLE AND DOUBLER WAS INSTALLED IAW ECR - [SDR CALA0100744](https://openairdocs.org/sdr/CALA0100744), Aug 7, 2001: SKIN. DENTED. INSPECTION FOUND RT WING O/B FLAP O/B TRAILING EDGE SKIN LOWER SURFACE DENTED. THE SKIN WAS REMOVED IAW SRM 51-30-2 AND THE SUPPORT RIBS WERE FOUND DAMAGED. NEW - [SDR CALA0100742](https://openairdocs.org/sdr/CALA0100742), Aug 5, 2001: MOUNT. CORRODED. INSPECTION FOUND R/H WING I/B FLAP HINGE #2 CORRODED IN BOTTOM MOUNT HOLE. THE HOLE WAS REAMED AND TWO BUSHINGS WERE INSTALLED IAW EA 9-2750-2-A0914 AND ECRA 27 - [SDR CALA0100741](https://openairdocs.org/sdr/CALA0100741), Aug 4, 2001: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT FS 1271 FROM LONGERON 27L TO 27R. THE CORRODED AREA OF FRAME WAS CUT OUT IAW SRM 53-03, FIGURE 2A. A REPAIR WAS INSTALLED IAW - [SDR CALA0100739](https://openairdocs.org/sdr/CALA0100739), Aug 3, 2001: SKIN. GOUGED. INSPECTION FOUND R/H ELEVATOR LOWER SKIN SURFACE O/B OF TRIM TAB PUSH ROD FAIRING GOUGED. THE SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70- - [SDR CALA0100738](https://openairdocs.org/sdr/CALA0100738), Aug 3, 2001: BRACKET. CRACKED. INSPECTION FOUND A 1" CRACK IN T-BRACKET OF FORWARD CARGO DOOR UPPER INTERNAL PAN FORWARD OF AFT HINGES. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED - [SDR CALA0100737](https://openairdocs.org/sdr/CALA0100737), Aug 3, 2001: WEB. CORRODED. INSPECTION FOUND FORWARD CARGO TORQUE BOX WEB CORRODED AROUND FASTENER HOLES AT STA 370. THE TORQUE BOX WEB AND SUPPORT ANGLE WERE REMOVED IAW SRM 51-10-4 AND 5 - [SDR CALA0100736](https://openairdocs.org/sdr/CALA0100736), Aug 3, 2001: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR TORQUE BOX WEB TANG. THE CRACKED AREA OF WEB TANG WAS TRIMMED OUT AND A DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5 - [SDR CALA0100734](https://openairdocs.org/sdr/CALA0100734), Aug 3, 2001: ANGLE. CRACKED. INSPECTION FOUND A 1" CRACK IN T-ANGLE AT FORWARD CARGO DOOR UPPER INTERNAL PAN AFT OF FORWARD HINGE. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS INSTALLED IA - [SDR CALA0100733](https://openairdocs.org/sdr/CALA0100733), Aug 3, 2001: CHANNEL. CRACKED. INSPECTION FOUND A 1" CRACK IN L/H MLG DOOR CHANNEL AT FORWARD END OF DOOR JUST ABOVE DOOR SEAL. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5281-2-A0904 AND ECRA 5 - [SDR CALA0100731](https://openairdocs.org/sdr/CALA0100731), Jul 31, 2001: SPLICE. CORRODED. INSPECTION FOUND LONGERON 29L SPLICE CORRODED IN FORWARD CARGO AREA AT FS 225. THE LONGERON SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 53-01, FIG - [SDR CALA0100730](https://openairdocs.org/sdr/CALA0100730), Jul 31, 2001: FRAME. CORRODED. INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 522 BETWEEN LONGERONS 28L AND 28R. THE CORRODED AREA OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53- - [SDR CALA0100728](https://openairdocs.org/sdr/CALA0100728), Jul 31, 2001: SKIN. GOUGED. INSPECTION FOUND R/H ELEVATOR SKIN LOWER SURFACE JUST OUTBOARD OF #2 HINGE MOUNTING PAD GOUGED. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS INSTALLED IA - [SDR CALA0100725](https://openairdocs.org/sdr/CALA0100725), Jul 30, 2001: SKIN. DENTED. INSPECTION FOUND RUDDER CONTROL TAB SKIN DENTED IN THE LOWER LEFT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE TAB WAS REPAIRED, WEIGHED, AND BALANCED - [SDR CALA0100718](https://openairdocs.org/sdr/CALA0100718), Jul 30, 2001: SKIN. DENTED. INSPECTION FOUND L/H "0" SLAT EXTERNAL SKIN DENTED. THE SKIN AND ATTACHING PARTS WERE REMOVED IAW SRM 51-30-6 AND 51-30-1. A DOUBLER WAS INSTALLED IAW SRM 57-09 - [SDR CALA0100717](https://openairdocs.org/sdr/CALA0100717), Jul 30, 2001: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT FS 160 - 200, RBL 35 TO RBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 53-10-1. - [SDR CALA0100716](https://openairdocs.org/sdr/CALA0100716), Jul 29, 2001: SPACER. CORRODED. INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM SPACER CORRODED AROUND RIVNUTS. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-30-4 AND 51-10- - [SDR CALA0100715](https://openairdocs.org/sdr/CALA0100715), Jul 29, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT FS 845-1032. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED WITH SPLICES IAW SRM 53-05, FIGURE 4F - [SDR CALA0100714](https://openairdocs.org/sdr/CALA0100714), Jul 29, 2001: SKIN. DENTED. INSPECTION FOUND L/H EXTERIOR FUSELAGE SKIN DENTED AT FS 522 ABOVE L25 AND AT FS 494 ABOVE L25. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER W - [SDR CALA0100713](https://openairdocs.org/sdr/CALA0100713), Jul 29, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN L/H CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 5 - [SDR CALA0100711](https://openairdocs.org/sdr/CALA0100711), Jul 29, 2001: FLOOR PANEL. BROKEN. INSPECTION FOUND CABIN L/H O/B FLOOR PANELS BROKEN OFF AT FASTENER HOLES AT FS 1079-1155 AND FS 1155-1250. THE PANELS WERE REPAIRED IAW SRM 51-70-1. - [SDR CALA0100710](https://openairdocs.org/sdr/CALA0100710), Jul 29, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT FS 1174-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-3. - [SDR CALA0100709](https://openairdocs.org/sdr/CALA0100709), Jul 29, 2001: FLOOR PANEL. PUNCTURED. INSPECTION FOUND CABIN R/H I/B FLOOR PANEL PUNCTURED AT FS 389-408. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265 AND SRM 51-30-1. - [SDR CALA0100708](https://openairdocs.org/sdr/CALA0100708), Jul 28, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND COPILOT'S I/B FLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-30-01, 53-21-0, SHEET 23, 51- - [SDR CALA0100705](https://openairdocs.org/sdr/CALA0100705), Jul 27, 2001: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, RBL 44 TO RBL 56. THE CORRODED SECTION OF CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30- - [SDR CALA0100704](https://openairdocs.org/sdr/CALA0100704), Jul 27, 2001: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR CUSP ANGLE CORRODED AT FS 203. THE CORRODED SECTION OF CUSP ANGLE WAS CUT OUT IAW SRM 51-30-1. A CUSP ANGLE AND SPLICE WERE INSTALLED - [SDR CALA0100702](https://openairdocs.org/sdr/CALA0100702), Jul 27, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND L/H SEAT TRACK CORRODED AT STA 1108-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1. - [SDR CALA0100701](https://openairdocs.org/sdr/CALA0100701), Jul 27, 2001: PAN. CRACKED. INSPECTION FOUND DOOR PAN CRACKED AROUND BOTTOM STOP AT AFT CARGO DOOR AFT SIDE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 1 & 4 AND ECRA 5230-0 - [SDR CALA0100700](https://openairdocs.org/sdr/CALA0100700), Jul 27, 2001: WEB. CRACKED. INSPECTION FOUND CUSP WEB CRACKED AFT OF L-2 DOOR AT STA 1174, LBL 60. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1. - [SDR CALA0100699](https://openairdocs.org/sdr/CALA0100699), Jul 26, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 798-1108. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1. - [SDR CALA0100698](https://openairdocs.org/sdr/CALA0100698), Jul 26, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED IA - [SDR CALA0100697](https://openairdocs.org/sdr/CALA0100697), Jul 26, 2001: SKIN. GOUGED. INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AND GOUGED BELOW NR 2 ENGINE APRON AT STA 1309. THE DAMAGED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A REPAI - [SDR CALA0100696](https://openairdocs.org/sdr/CALA0100696), Jul 26, 2001: SKIN. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED BELOW HANDLES. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 52-05. - [SDR CALA0100692](https://openairdocs.org/sdr/CALA0100692), Jul 25, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND R/H CENTER SEAT TRACK CORRODED AT FS 798-874. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30 - [SDR CALA0100690](https://openairdocs.org/sdr/CALA0100690), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FLOOR PANELS M-P DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100689](https://openairdocs.org/sdr/CALA0100689), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN FLOOR PANELS B-K DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100688](https://openairdocs.org/sdr/CALA0100688), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN L/H I/B FLOOR PANEL DELAMINATED AT FS 1079-1155 AND R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 927-1003. NEW FLOOR PANELS WERE INSTALLED I - [SDR CALA0100687](https://openairdocs.org/sdr/CALA0100687), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND MAIN CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1174-1250 AND FS 1309-1361. A R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 1250-1309. A NEW FLOOR - [SDR CALA0100686](https://openairdocs.org/sdr/CALA0100686), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN R/H I/B AND CENTER FLOOR PANELS AT FS 1117-1174 DELAMINATED AND CENTER PANEL AT FS 1079-1117 DELAMINATED. NEW FLOOR PANELS WERE INSTALLED - [SDR CALA0100685](https://openairdocs.org/sdr/CALA0100685), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 826-886 AND AT FS 945-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100684](https://openairdocs.org/sdr/CALA0100684), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND L/H I/B FLOOR PANEL PUNCTURED AT FS 769-826 AND L/H I/B FLOOR PANEL AT FS 864-886 WAS DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320 - [SDR CALA0100683](https://openairdocs.org/sdr/CALA0100683), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND R/H I/B FLOOR PANELS DELAMINATED AT FS 826-927. A CENTER PANEL AT FS 886-946 AND CENTER & RIGHT CENTER PANELS AT FS 807-826 WERE FOUND DELAMINA - [SDR CALA0100682](https://openairdocs.org/sdr/CALA0100682), Jul 25, 2001: FLOOR PANEL. DELAMINATED. INSPECTION FOUND MAIN CABIN R/H CENTER AND L/H CENTER FLOOR PANELS DELAMINATED AT FS 693-769. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265. - [SDR CALA0100677](https://openairdocs.org/sdr/CALA0100677), Jul 24, 2001: SKIN. DENTED. INSPECTION FOUND L/H LOWER EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 29L. THE DENT WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 53-0 - [SDR CALA0100676](https://openairdocs.org/sdr/CALA0100676), Jul 24, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT FS 275, LONGERON 17L. THE DENTED AREA OF SKIN WAS REMOVED IAW SRM 51-30-2. NEW SKIN WAS INSTALLED IAW SRM 51-3 - [SDR CALA0100675](https://openairdocs.org/sdr/CALA0100675), Jul 24, 2001: SKIN. DAMAGED. INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 180, LONGERON 23R. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 12, PAGE 35. A REPAIR DOUBLER AND FINGER DOU All 86: https://openairdocs.org/deregistered/N16815-2002-09-17/reports.md ## FAA accident and incident reports (1) 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 19960202003189I](https://openairdocs.org/incident/19960202003189I), Feb 2, 1996: Doug DC9 (N16815), Las Vegas, NV. Narrative: incident occurred at FL 280 40 minutes from las. Right hydraulic pressure low light came on and right hydraulic quantity decreased to 1.5 qts.… ## Other aircraft with N16815 - [Cancelled 2005-12-12](https://openairdocs.org/deregistered/N16815-2005-12-12): Cessna 172S, S/N 172S9921. Exported to Slovenia. Owner: [Globe Aero Ltd](https://openairdocs.org/faa-owner/GLOBE%20AERO%20LTD), [Lakeland, FL](https://openairdocs.org/faa-place/FL/Lakeland) - [Cancelled 2005-10-21](https://openairdocs.org/deregistered/N16815-2005-10-21): Cessna 172, S/N 172C9921. N-number assigned (import), not yet registered - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N16815-undated): Bell 206B, S/N 2222. N-number assigned, not yet registered --- 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.