# N14814: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2002-10-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 2, 2002 - Exported to: Indonesia - Status when cancelled: Second triennial mailing, no response - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49112 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: May 24, 1982 - Certificate issued: June 19, 1990 - Last registry action: December 29, 1997 - Mode S code: A0C300 - Owner when cancelled: [Eal Delaware Xi Corp](https://openairdocs.org/faa-owner/EAL%20DELAWARE%20XI%20CORP) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0593° N, 73.5444° W: Placed by OpenAirDocs at the center of ZIP code 06902, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14814 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14814 - Page: https://openairdocs.org/deregistered/N14814-2002-10-02 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-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0200032](https://openairdocs.org/sdr/CALA0200032), Jan 23, 2002: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN #1 ENGINE UPPER THRUST REVERSER OUTER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 7830-01000. - [SDR CALA0200031](https://openairdocs.org/sdr/CALA0200031), Jan 23, 2002: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN #2 ENGINE UPPER THRUST REVERSER OUTER SKIN. TWO DOUBLERS WERE INSTALLED IAW ECRA 7830-01000. - [SDR CALA0001780](https://openairdocs.org/sdr/CALA0001780), Nov 16, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND TWO .5 INCH CRACKS IN INTERCOSTAL IN MID CARGO COMPARTMENT AT STA 769 - 788, CENTERLINE. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001745](https://openairdocs.org/sdr/CALA0001745), Nov 13, 2000: FRAME. CORRODED. INSPECTION FOUND AFT SIDE OF BELT FRAME CORRODED IN AFT BAGGAGE BIN AT STA 1302, LONGERON 22L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A NEW SECTION WAS I - [SDR CALA0001744](https://openairdocs.org/sdr/CALA0001744), Nov 13, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT STA 1212 - 1322. A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 51-30. - [SDR CALA0001723](https://openairdocs.org/sdr/CALA0001723), Nov 10, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE UNDER LT AFT LAV AT STA 1338. A REPAIR WAS INSTALLED IAW ECRA 5305-01051. - [SDR CALA0001705](https://openairdocs.org/sdr/CALA0001705), Nov 9, 2000: PAN. GOUGED. INSPECTION FOUND AFT BAGGAGE BIN DOOR STOP PAD FITTING ATTACH POINT SKIN GOUGED AT AFT LOWER LOCATION. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01540. - [SDR CALA0001703](https://openairdocs.org/sdr/CALA0001703), Nov 8, 2000: WEB. CORRODED. INSPECTION FOUND CUSP AT LT SIDE FLOOR LINE CORRODED AT STA 190 - 237. A REPAIR WAS INSTALLED IAW ECRA 5310-04066. - [SDR CALA0001699](https://openairdocs.org/sdr/CALA0001699), Nov 7, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT MID SEAT TRACK CORRODED AT STA 1030 - 1200. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA0001685](https://openairdocs.org/sdr/CALA0001685), Nov 3, 2000: CHANNEL. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD Z-CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 53-05, FIGURE 63, SHEET 1. - [SDR CALA0001684](https://openairdocs.org/sdr/CALA0001684), Nov 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1030 - 1132. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05. - [SDR CALA0001682](https://openairdocs.org/sdr/CALA0001682), Nov 2, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 1.125 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1463. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23. - [SDR CALA9900989](https://openairdocs.org/sdr/CALA9900989), Aug 5, 1999: WIRE. LOOSE. THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF FROM IAH. THE GEAR HANDLE WAS EXTENDED, BUT THE LIGHT REMAINED ON WITH THE - [SDR CALA9900454](https://openairdocs.org/sdr/CALA9900454), Apr 26, 1999: MANIFOLD. CRACKED. NUMBER 2 FUEL FLOW INDICATES HIGHER THAN NUMBER 1 ON TAKEOFF. AT CLIMB POWER NUMBER 2 FUEL FLOW IS 1000 POUNDS HIGHER AND AT CRUISE 500 POUNDS HIGHER. FUEL USED - [SDR CALA9801903](https://openairdocs.org/sdr/CALA9801903), Oct 2, 1998: BELTFRAME. CORRODED. INSPECTION FOUND BELTFRAME CORRODED AT STA 1322 BETWEEN LONGERON 29L AND 29R. THE CORROSION WAS REMOVED, FILLER AND DOUBLERS INSTALLED IAW SRM 53-03, FIGURE 2A. - [SDR CALA9801902](https://openairdocs.org/sdr/CALA9801902), Oct 1, 1998: FITTING. WORN. INSPECTION FOUND RT MLG RETRACT ACTUATOR UPPER ATTACH COKE BOTTLE FITTING WORN. A NEW COKE BOTTLE FITTING AND BUSHINGS WERE INSTALLED IAW MM 57-40-02. - [SDR CALA9801901](https://openairdocs.org/sdr/CALA9801901), Oct 1, 1998: BELTFRAME. CORRODED. INSPECTION FOUND BELTFRAME WEB CORRODED AT STA 1338 BETWEEN LONGERONS 25 AND 26. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, - [SDR CALA9801895](https://openairdocs.org/sdr/CALA9801895), Oct 1, 1998: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. THE DOOR BEAM WAS REPLACED IAW WORK CARD 99-5240-1-0002. - [SDR CALA9801894](https://openairdocs.org/sdr/CALA9801894), Sep 30, 1998: SKIN. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 1418, LONGERON 2R. REPAIRED IAW SRM 53-04, FIGURE 40. - [SDR CALA9801416](https://openairdocs.org/sdr/CALA9801416), Aug 7, 1998: B NUT. LEAKING. THE RT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO 1.5 QUARTS ON CLIMB-OUT OF DCA EN ROUTE TO EWR. THE RIGHT PUMP AND AUX PUMP WERE TURNED OFF. THE GEAR WAS MANU - [SDR CALA9800100](https://openairdocs.org/sdr/CALA9800100), Jan 24, 1998: WIRE. BROKEN. THE NLG INDICATED RED UNSAFE WHEN GEAR WAS EXTENDED, BUT THE COCKPIT INDICATOR PIN SHOWED DOWN AND LOCKED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND THE - [SDR CALA9601910](https://openairdocs.org/sdr/CALA9601910), Dec 29, 1996: FUEL CONTL UNIT. MALFUNCTIONED. THE APU AUTO SHUT DOWN INFLIGHT AND THE HIGH OIL TEMP LIGHT ILLUMINATED. ALSO, THE NR 2 FIRE BOTTLE LOW AGENT LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT EWR WITH - [SDR CALA9601574](https://openairdocs.org/sdr/CALA9601574), Oct 17, 1996: THRESHOLD. CORRODED. INSPECTION FOUND LT AFT SERVICE DOOR THRESHOLD WEB AT AFT LOWER CORNER CORRODED. THE CORRODED WEB SECTION WAS REMOVED. A NEW WEB REPAIR SECTION WAS FABRICATED A - [SDR CALA9601573](https://openairdocs.org/sdr/CALA9601573), Oct 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 218 TO 238, LBL 14. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-1 - [SDR CALA9601572](https://openairdocs.org/sdr/CALA9601572), Oct 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150 TO 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9601571](https://openairdocs.org/sdr/CALA9601571), Oct 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150-200, LBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 51- - [SDR CALA9601570](https://openairdocs.org/sdr/CALA9601570), Oct 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 160 TO 200, LBL 44. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9601566](https://openairdocs.org/sdr/CALA9601566), Oct 8, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200-204, LBL 56. THE FLOORBOARD SUPPORT WAS REMOVED AND A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW - [SDR CALA9601577](https://openairdocs.org/sdr/CALA9601577), Oct 7, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT F.S. 1155, LBL 18 - 40. THE FLOOR SUPPORT WAS REMOVED AND A SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30- - [SDR CALA9601576](https://openairdocs.org/sdr/CALA9601576), Oct 7, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT FORWARD BULKHEAD OF MID CARGO COMPARTMENT, STA 541, STRINGER 29L TO 28L. THE FLOOR SUPPORT WAS REMOVED IAW SRM 5 - [SDR CALA9601575](https://openairdocs.org/sdr/CALA9601575), Oct 7, 1996: BRACE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT MLG DOOR CENTER BRACE. THE CENTER BRACE WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED AND THE BRACE WAS REINSTALLE - [SDR CALA9601569](https://openairdocs.org/sdr/CALA9601569), Oct 7, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 168 FROM RBL 10 TO RBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW - [SDR CALA9601568](https://openairdocs.org/sdr/CALA9601568), Oct 7, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, RBL 10 TO RBL 44. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51- - [SDR CALA9601567](https://openairdocs.org/sdr/CALA9601567), Oct 7, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, LBL 7 TO RBL 5. THE CORRODED SECTION WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53 - [SDR CALA9601578](https://openairdocs.org/sdr/CALA9601578), Oct 6, 1996: SUPPORT. CORRODED. INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 221, LBL 3. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A REPLACEMENT PART WAS FABRICATED AND INSTALLED I - [SDR CALA9601565](https://openairdocs.org/sdr/CALA9601565), Oct 5, 1996: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AND DENT IN FUSELAGE SKIN AT STA 258 JUST BELOW STRINGER 21R. THE DENT WAS REWORKED AND THE CRACKED AREA WAS CUT OUT. A FILLER - [SDR CALA9601140](https://openairdocs.org/sdr/CALA9601140), Aug 8, 1996: HYD LINE. LEAKING. THE RT HYDRAULIC SYSTEM QUANTITY BEGAN TO DECREASE DURING CLIMB. THE R/H HYDRAULIC QUANTITY CONTINUED TO DROP SLOWLY WHILE AT CRUISE. THE TRANSFER PUMP, RT HYDR - [SDR CAL960059](https://openairdocs.org/sdr/CAL960059), Jan 20, 1996: FIRE DET MODULE. INOPERATIVE. FLT NR 421 - IAH - THE NR 1 ENGINE LOOP 'B' FIRE DETECTOR LIGHT AND MASTER CAUTION LIGHT ILLUMINATED DURING CLIMB-OUT AT 18,000 FEET. THE NR 1 ENGINE LOOP SWITC - [SDR CAL950649](https://openairdocs.org/sdr/CAL950649), Aug 8, 1995: FUEL PUMP. LEAKING. DFW - FLT 0140 - THE NR 1 FUEL QUANTITY DECREASED FROM 6500 TO 1350 WITHIN 15 MINUTES WHILE ENROUTE FROM LAS TO IAH. THE CROSSFEED PROCEDURE WAS USED AND THE NR ## 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 19950808031859I](https://openairdocs.org/incident/19950808031859I), Aug 8, 1995: Doug DC982 (N14814), Dallas-Ft Worth, TX. Severe fuel loss. Diverted dfw. Fuel leak left engine. Fuel pressure warning to fuel pump separated leaked fuel. ## Other aircraft with N14814 - [Registered now](https://openairdocs.org/aircraft/N14814): Cessna 172S, S/N 172S10451, built 2007 --- 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.