# N16808: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2002-11-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 13, 2002 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49262 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 25, 1984 - Certificate issued: February 8, 2001 - Last registry action: February 8, 2001 - Mode S code: A111DF - Owner when cancelled: [East Trust-Sub 12](https://openairdocs.org/faa-owner/EAST%20TRUST-SUB%2012) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16808 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16808 - Page: https://openairdocs.org/deregistered/N16808-2002-11-13 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100837](https://openairdocs.org/sdr/CALA0100837), Sep 7, 2001: BATTERY. DISCHARGED. INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR INOPERATIVE. THE BATTERIES FOR THE PORTABLE EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED IAW - [SDR CALA0001957](https://openairdocs.org/sdr/CALA0001957), Dec 19, 2000: SKIN. DENTED. INSPECTION FOUND LT AFT FUSELAGE SKIN DENTED JUST AFT OF LOUVER. THE DENT WAS COLD WORKED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEETS 11 - [SDR CALA0000113](https://openairdocs.org/sdr/CALA0000113), Feb 1, 2000: SKIN. DENTED. INSPECTION FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE DENTED AT XFS 71 TO XFS 77.50. A DOUBLER WAS INSTALLED IAW EA9-5513-2-AD577 AND ECRA 5510 - [SDR CALA0000112](https://openairdocs.org/sdr/CALA0000112), Feb 1, 2000: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN VERTICAL SUPPORT FITTING AT FS 200, LBL 50. THE VERTICAL SUPPORT FITTING WAS REPLACED IAW SRM 51-30-05. - [SDR CALA0000111](https://openairdocs.org/sdr/CALA0000111), Feb 1, 2000: SKIN. DENTED. INSPECTION FOUND RT HORIZONTAL STABILIZER DENTED EIGHT FEET AND NINE FEET FROM STABILIZER ROOT AT LEADING EDGE. THE AREA WAS REPAIRED IAW SRM 55-03, PAGE 6 AND - [SDR CALA0000110](https://openairdocs.org/sdr/CALA0000110), Feb 1, 2000: SUPPORT. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WHEEL WELL FORWARD JAMB SUPPORT. AN ANGLE AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-11, 51-10-03, AND 53-10-01, FIGURE - [SDR CALA0000109](https://openairdocs.org/sdr/CALA0000109), Feb 1, 2000: PAN. GOUGED. INSPECTION FOUND R-1 DOORJAMB LOWER PAN AT SILL PLATE GOUGED. THE R-1 DOOR JAMB LOWER PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 55. - [SDR CALA0000080](https://openairdocs.org/sdr/CALA0000080), Jan 25, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED BETWEEN STA 1040 AND 1338. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5. - [SDR CALA0000055](https://openairdocs.org/sdr/CALA0000055), Jan 21, 2000: WEB. CRACKED. INSPECTION FOUND CUSP WEB CRACKED AT FS 1174, LBL 43. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW SECTION AND DOUBLER WERE INSTALLED IAW SRM 51-30-5. - [SDR CALA0000054](https://openairdocs.org/sdr/CALA0000054), Jan 21, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT AT FS 200, BL 0 TO RBL 44 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9901547](https://openairdocs.org/sdr/CALA9901547), Dec 2, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE FIRST CLASS OVERHEAD EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE OVERHEAD LI - [SDR CALA9800689](https://openairdocs.org/sdr/CALA9800689), Apr 23, 1998: STRUT. REQUIRED SERVICE. THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF FROM ORD. THE CHECKLIST WAS PERFORMED AND WHEN THE GEAR WAS PUT DOWN IT EXTENDED WITH A BANG. THE AIRCRAFT WAS RETUR - [SDR CALA9701765](https://openairdocs.org/sdr/CALA9701765), Dec 14, 1997: CABLES. OUT OF ADJUST. THE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND THE AFT PASSENGER ENTRANCE DOOR HANDLE WAS EXCESSIVE. MAINTENANCE RIGGED THE TAILCONE - [SDR CALA9701759](https://openairdocs.org/sdr/CALA9701759), Dec 11, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 CRACK IN MAIN CABIN DOOR INTERCOSTAL. THE CRACK WAS IN RADIUS AND LOCATED AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REMOVED AND REPLA - [SDR CALA9701758](https://openairdocs.org/sdr/CALA9701758), Dec 11, 1997: JAMB. CORRODED. INSPECTION FOUND DOOR JAMB BEAM OF MAIN BAGGAGE BIN CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63 AND ECRA 5310-03642. - [SDR CALA9701757](https://openairdocs.org/sdr/CALA9701757), Dec 10, 1997: BEAM. CRACKED. INSPECTION FOUND A .75 CRACK IN FORWARD LOWER CORNER OF FORWARD SERVICE DOOR LOWER BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-02, 51-30-04, AND 51-30-05. - [SDR CALA9700964](https://openairdocs.org/sdr/CALA9700964), Jun 21, 1997: RADIO PANEL. CHAFED WIRE. THE OBSERVER'S RADIO PANEL STARTED TO SMOKE WHILE EN ROUTE. THE PANEL WAS REMOVED, THE CONNECTOR PLUGS WERE DISCONNECTED, AND THE SMOKE CEASED. THE FLIGHT CONTI - [SDR CALA9600966](https://openairdocs.org/sdr/CALA9600966), Jul 5, 1996: GROUND SHIFT ROD. BROKEN. THE AIR/GROUND SHIFT MECHANISM WOULD NOT COME OUT OF GROUND MODE AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND GROUND SHIFT ROD ON - [SDR CAL960098](https://openairdocs.org/sdr/CAL960098), Jan 21, 1996: SKIN. DELAMINATED. MIA - INSPECTION FOUND RIGHT WING CENTER SPAR TRAILING EDGE LOWER PANEL BELOW INBOARD AND OUTBOARD ANTI-SKID VALVES DELAMINATED. THE DELAMINATED AREA WAS CUT OU - [SDR CAL960094](https://openairdocs.org/sdr/CAL960094), Jan 19, 1996: SUPPORT. CORRODED. MIA - INSPECTION FOUND CORROSION ON FLOOR SUPPORT TRACK IN CENTER CARGO COMPARTMENT BETWEEN BS 570-695, LBL 20. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS - [SDR CAL960160](https://openairdocs.org/sdr/CAL960160), Jan 17, 1996: BULKHEAD. CRACKED. MIA - INSPECTION FOUND A .5 INCH CRACK IN CANTED BULKHEAD WEB JUST FORWARD OF RUDDER TRIM ACTUATOR DRUM AT FS 1490, RIGHT SIDE. THE CRACKED WEB WAS REMOVED AND - [SDR CAL960162](https://openairdocs.org/sdr/CAL960162), Jan 15, 1996: ANGLE. CRACKED. MIA - INSPECTION FOUND A .5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE - [SDR CAL960159](https://openairdocs.org/sdr/CAL960159), Jan 15, 1996: FLOOR WEB. CRACKED. MIA - INSPECTION FOUND AN 8 INCH CRACK IN SUB FLOOR WEB ON RIGHT SIDE, STATION 1300, STRINGER 18. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGU - [SDR CAL960100](https://openairdocs.org/sdr/CAL960100), Jan 15, 1996: SKIN. DELAMINATED. MIA - INSPECTION FOUND RIGHT WING INBOARD SPOILER UPPER SKIN DELAMINATED AT FORWARD INBOARD AREA. THE DAMAGED CORE WAS CUT OUT AND A HOT BOND REPAIR WAS DONE IA - [SDR CAL960093](https://openairdocs.org/sdr/CAL960093), Jan 15, 1996: SUPPORT. CORRODED. MIA - INSPECTION FOUND FLOOR BOARD SUPPORT HAT CHANNEL CORRODED IN MAIN CABIN AT STATION 1165. A NEW FLOOR BOARD SUPPORT HAT CHANNEL WAS FABRICATED AND INSTALLE - [SDR CAL960095](https://openairdocs.org/sdr/CAL960095), Jan 14, 1996: VANE. GOUGED. MIA - INSPECTION FOUND TOP INBOARD END OF RIGHT WING 5TH FOREFLAP VANE HAD GOUGES. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-1 - [SDR CAL960101](https://openairdocs.org/sdr/CAL960101), Jan 13, 1996: VANE. CHAFED. MIA - INSPECTION FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE SEGMENT CHAFED WITH METAL CURLED AT INBOARD UPPER END. THE CHAFED AREA WAS CUT OUT. FILLER AND DOUB - [SDR CAL960099](https://openairdocs.org/sdr/CAL960099), Jan 13, 1996: SKIN. CHAFED. MIA - INSPECTION FOUND LEFT WING INBOARD FLAP UPPER SURFACE CHAFED INTO TWENTY INCHES FROM OUTBOARD END. THE CHAFED AREA WAS CUT OUT. AN INTERNAL DOUBLER AND FI - [SDR CAL960097](https://openairdocs.org/sdr/CAL960097), Jan 13, 1996: SKIN. DELAMINATED. MIA - INSPECTION FOUND LEFT WING LOWER TRAILING EDGE SKIN PANEL DELAMINATED AROUND MOUNT SCREWS FOR INBOARD AND OUTBOARD ANTI-SKID VALVES. THE PANEL WAS REPAIRE - [SDR CAL960096](https://openairdocs.org/sdr/CAL960096), Jan 13, 1996: VANE. DINGED. MIA - INSPECTION FOUND LOWER SURFACE OF INBOARD LEFT FLAP VANE DINGED AND ERODED DUE TO IMPACT DAMAGE CAUSED BY TIRE DEBRIS. A HOT BOND REPAIR WAS PERFORMED IAW - [SDR CAL960106](https://openairdocs.org/sdr/CAL960106), Jan 11, 1996: BATTERY PACK. DISCHARGED. MIA - INSPECTION FOUND THE FORWARD ENTRY EMERGENCY LIGHT DIM. THE BATTERIES FOR THE EMERGENCY LIGHT WERE REMOVED, RECHARGED, AND REINSTALLED. (M) - [SDR CAL960105](https://openairdocs.org/sdr/CAL960105), Jan 11, 1996: BATTERY PACK. DISCHARGED. MIA - INSPECTION FOUND THE AISLE OVERHEAD EMERGENCY LIGHT AT AFT GALLEY TO LAV INOPERATIVE. THE BATTERIES FOR THE EMERGENCY LIGHT WERE REMOVED, CHARGED, AND REI - [SDR CAL960103](https://openairdocs.org/sdr/CAL960103), Jan 11, 1996: BATTERY. DISCHARGED. MIA - INSPECTION FOUND AFT GALLEY EMEREGNCY LIGHT DIM. THE BATTERIES FOR THE LIGHT WERE REMOVED, CHARGED AND REINSTALLED. (M) - [SDR CAL960102](https://openairdocs.org/sdr/CAL960102), Jan 11, 1996: BATTERY PACK. DISCHARGED. MIA - INSPECTION FOUND FORWARD GALLEY EMERGENCY LIGHT DIM. THE BATTERY PACK WAS REPLACED AND A LAMP WAS INSTALLED PER MM 33-50-0. (M) - [SDR CAL951181](https://openairdocs.org/sdr/CAL951181), Dec 28, 1995: CLAMP. BROKEN. FLT 1263 - CLE - THE NR 2 ENG FIRE WARN LIGHT ILLUMINATED DURING CLIMB-OUT OF CLE. THE FIRE LIGHT WENT OUT FOR ABOUT 1 MIN AFTER LEVELING OFF, AND CAME ON AGAIN - [SDR CAL950596](https://openairdocs.org/sdr/CAL950596), Jul 15, 1995: GEN CONTL PNL. INOPERATIVE. GSO - FLT 0402 - THE RIGHT CSD OIL TEMP WENT OFF SCALE HIGH AFTER TAKEOFF FROM MCO. THE CSD WAS DISCONNECTED AND THE APU WAS STARTED TO POWER THE RIGHT AC BUS. ## Other aircraft with N16808 - [Cancelled 2007-09-14](https://openairdocs.org/deregistered/N16808-2007-09-14): Cessna 172R, S/N 17281427, built 2007. Exported to India. Owner: [Cessna Aircraft Company](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20COMPANY), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) --- 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.