# N16807: Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2012-02-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 7, 2012 - Status when cancelled: Third renewal notice - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49261 - Type of aircraft: Fixed wing multi engine - Certificate issued: June 14, 2004 - Last registry action: June 15, 2010 - Mode S code: A111DE - Owner when cancelled: [Avtec USA Inc](https://openairdocs.org/faa-owner/AVTEC%20USA%20INC) - Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas) - Owner type: Corporation - Owner's area on the map: 36.0845° N, 115.1461° W: Placed by OpenAirDocs at the center of ZIP code 89119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16807 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16807 - Page: https://openairdocs.org/deregistered/N16807-2012-02-07 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-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100008](https://openairdocs.org/sdr/CALA0100008), Jan 8, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL AND AFT ATTACH ANGLE IN MID PIT CORRODED BETWEEN STA 709 AND 788, L27R TO L28R. THE INTERCOSTAL AND ANGLE WERE REMOVED AND A NEW IN - [SDR CALA0100002](https://openairdocs.org/sdr/CALA0100002), Jan 1, 2001: TAB. LOOSE. INSPECTION FOUND RUDDER TAB T/E METAL TAB LOOSE ON RT SIDE. THE RUDDER TRIM TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-02, PARAGRAPH B & C. - [SDR CALA0002005](https://openairdocs.org/sdr/CALA0002005), Dec 29, 2000: SKIN. DENTED. INSPECTION FOUND RT GROUND SPOILER SKIN DENTED IN TWO PLACES ON UPPER SURFACE. THE DENTED AREAS WERE REMOVED AND DOUBLERS WERE INSTALLED IAW SRM 57-04, FIGURE 5 - [SDR CALA0002004](https://openairdocs.org/sdr/CALA0002004), Dec 29, 2000: DOUBLER. GOUGED. INSPECTION FOUND REPAIR DOUBLERS AT FORWARD AND AFT LOWER CORNER OF AFT CARGO DOOR GOUGED. THE DOUBLERS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-3, AND - [SDR CALA0002003](https://openairdocs.org/sdr/CALA0002003), Dec 29, 2000: PAN. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. THE CRACK WAS STOP DRILLED IAW EA 9-52812-A0807. A DOUBLER WAS INSTALLED IAW SRM 51-10- - [SDR CALA0002002](https://openairdocs.org/sdr/CALA0002002), Dec 29, 2000: DOUBLER. GOUGED. INSPECTION FOUND DOUBLER AT NR 2 ENGINE LOWER T/R O/B CORNER BENT AND GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, - [SDR CALA0002000](https://openairdocs.org/sdr/CALA0002000), Dec 27, 2000: PAN. CRACKED. INSPECTION FOUND A 2" CRACK IN MID CARGO DOOR OUTER PAN AT LOWER EDGE AFT STOP AREA. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01554. - [SDR CALA0001997](https://openairdocs.org/sdr/CALA0001997), Dec 26, 2000: SKIN. BULGED. INSPECTION FOUND AFT CARGO DOOR SKIN BULGED AT RIVET NUTS HOLDING SEAL RETAINER AROUND DOOR. THE RIVET NUTS WERE REMOVED IAW SRM 51-30-7. A DOUBLER WAS INSTALLE - [SDR CALA0001996](https://openairdocs.org/sdr/CALA0001996), Dec 26, 2000: ANGLE. CORRODED. INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN FS 1155-1174, LBL 50 (ATTACHED TO LOWER FACE OF CUSP WEB). THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS IN - [SDR CALA0001995](https://openairdocs.org/sdr/CALA0001995), Dec 26, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL NUTPLATE HOLES CORRODED IN MID CARGO PIT AT FS 769-788, LONGERON 27L-28L. THE INTERCOSTAL AND FITTING WERE REMOVED AND A NEW INTERC - [SDR CALA0001994](https://openairdocs.org/sdr/CALA0001994), Dec 26, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT AFT END UPPER SURFACE OF NR 1 PYLON ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND - [SDR CALA0001992](https://openairdocs.org/sdr/CALA0001992), Dec 26, 2000: DOOR FRAME. GOUGED. INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR JAMB UPPER LATCH CUTOUT GOUGED. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0822 AND ECRA 5330-03018. - [SDR CALA0001983](https://openairdocs.org/sdr/CALA0001983), Dec 21, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT FS 1079-1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5 AND 51-30-1. - [SDR CALA0001982](https://openairdocs.org/sdr/CALA0001982), Dec 21, 2000: ANGLE. CRACKED. INSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 5 - [SDR CALA0001981](https://openairdocs.org/sdr/CALA0001981), Dec 21, 2000: STOP. CORRODED. INSPECTION FOUND AFT CARGO DOOR STOPS NR 8, 12, AND 14 CORRODED AND WORN. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5330-02819. - [SDR CALA0001978](https://openairdocs.org/sdr/CALA0001978), Dec 21, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND CORROSION AT FASTENER HOLES ON UPPER AND LOWER SURFACES OF RT CARGO TRACK IN MID PIT AT STA 541-636. THE TRACK WAS REMOVED AND A NEW TRACK WAS - [SDR CALA0001975](https://openairdocs.org/sdr/CALA0001975), Dec 21, 2000: RIB. CRACKED. INSPECTION FOUND NR 2 AND 5 I/B INTERNAL RIBS OF NR 2 ENGINE UPPER T/R BUCKET CRACKED. THE CRACKS WERE 0.025" LONG. NEW RIBS WER INSTALLED IAW SRM 51-30-1. - [SDR CALA0001974](https://openairdocs.org/sdr/CALA0001974), Dec 20, 2000: FITTING. CRACKED. INSPECTION FOUND MID CARGO DOOR LOWER FORWARD INNER STOP SUPPORT FITTING CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10 - [SDR CALA0001973](https://openairdocs.org/sdr/CALA0001973), Dec 20, 2000: SHEAR TIE. CRACKED. INSPECTION FOUND A 1/2 INCH CRACK IN SHEAR FOOT ON BULKHEAD FRAME AT STA 1309, L14R. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND EA 9-53 - [SDR CALA0001972](https://openairdocs.org/sdr/CALA0001972), Dec 20, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT AFT PIT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES AT FS 1211-1332. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, - [SDR CALA0001971](https://openairdocs.org/sdr/CALA0001971), Dec 20, 2000: SPAR. CORRODED. INSPECTION FOUND RT HORIZONTAL STABILIZER FRONT BARREL NUT HOLE CORRODED AT FORWARD LOWER BOLT HOLE. THE CORROSION WAS REMOVED IAW SRM 51-10-5. THE HOLE WAS REA - [SDR CALA0001970](https://openairdocs.org/sdr/CALA0001970), Dec 20, 2000: WEB. CORRODED. INSPECTION FOUND LT CUSP WEB CORRODED FROM FS 1117-1174 FORWARD OF L-2 DOOR. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, - [SDR CALA0001963](https://openairdocs.org/sdr/CALA0001963), Dec 19, 2000: SUPPORT. BENT. INSPECTION FOUND CENTER SUPPORT IN AFT PIT BENT AT BULKHEAD, STA 1003, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-3, A - [SDR CALA0001962](https://openairdocs.org/sdr/CALA0001962), Dec 19, 2000: ANGLE. CORRODED. INSPECTION FOUND ANGLE CORRODED AT LT CARGO TRACK, FS 522 FALSE BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-1 - [SDR CALA0001961](https://openairdocs.org/sdr/CALA0001961), Dec 19, 2000: ANGLE. CORRODED. INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN STA 1136 AND 1155, LBL 50. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, - [SDR CALA0001959](https://openairdocs.org/sdr/CALA0001959), Dec 19, 2000: SKIN. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND RE - [SDR CALA0001958](https://openairdocs.org/sdr/CALA0001958), Dec 19, 2000: SKIN. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND RE - [SDR CALA0001948](https://openairdocs.org/sdr/CALA0001948), Dec 18, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 352-457. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, 51-10-3, 51-30-1, AND 51-30-5. - [SDR CALA0001947](https://openairdocs.org/sdr/CALA0001947), Dec 18, 2000: ANGLE. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT ANGLE IN AFT PIT AT STA 1003, LBL 12. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 5 - [SDR CALA0001945](https://openairdocs.org/sdr/CALA0001945), Dec 18, 2000: PAN. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER AND SHEAR CLIP WERE INSTALLED IAW EA 9-5281-2-A0807 AND SRM 51-10-3. - [SDR CALA0001944](https://openairdocs.org/sdr/CALA0001944), Dec 18, 2000: BRACKET. CRACKED. INSPECTION FOUND A 0.030 INCH CRACK IN SUPPORT BRACKET IN AFT PIT AT FORWARD BULKHEAD, STA 1003, LBL 10. THE SUPPORT BRACKET WAS REMOVED AND A NEW BRACKET WAS I - [SDR CALA0001943](https://openairdocs.org/sdr/CALA0001943), Dec 18, 2000: SKIN. DENTED. INSPECTION FOUND LT SIDE OF AFT ENTRANCE AIRSTAIR DOOR EXTERIOR SKIN DENTED. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-30-2, 51-3 - [SDR CALA0001942](https://openairdocs.org/sdr/CALA0001942), Dec 18, 2000: CHANNEL. CRACKED. INSPECTION FOUND TWO EACH 0.075 INCH CRACKS IN RT HORIZONTAL STABILIZER AFT SPAR HAT SECTION CHANNEL. THE HAT SECTION CHANNEL WAS REMOVED AND A NEW CHANNEL WAS - [SDR CALA0001932](https://openairdocs.org/sdr/CALA0001932), Dec 16, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 427-925. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIGURE 4B. - [SDR CALA0001931](https://openairdocs.org/sdr/CALA0001931), Dec 16, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 190, L21R. THE SKIN WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, AND 51- - [SDR CALA0001928](https://openairdocs.org/sdr/CALA0001928), Dec 16, 2000: FLOOR PANEL. BENT. INSPECTION FOUND CABIN RT O/B FLOOR PANEL BENT AT FS 465-541 AND AT FS 541-617. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-24-0, 53-01, 51-30-2, - [SDR CALA0001927](https://openairdocs.org/sdr/CALA0001927), Dec 15, 2000: PAN. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK IN LT I/B MLG DOOR AFT LOWER PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 28. A REPAIR DOUBLER WAS INSTALLED IAW SRM - [SDR CALA0001926](https://openairdocs.org/sdr/CALA0001926), Dec 15, 2000: PAN. CRACKED. INSPECTION FOUND TWO 1/2 INCH CRACKS IN RT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5280-01254, 51-10-3, 51-30-2, AND EA 9-5281-2 - [SDR CALA0001923](https://openairdocs.org/sdr/CALA0001923), Dec 15, 2000: SKIN. CORRODED. INSPECTION FOUND FORWARD EDGE OF AFT CARGO DOOR SKIN CORRODED AT CENTER FITTING. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05,51-10-6, AND 51-30-2. - [SDR CALA0001922](https://openairdocs.org/sdr/CALA0001922), Dec 15, 2000: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT FS 1193, LONGERON 30, IN AFT PIT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, 51-30-1, AND 51-3 - [SDR CALA0001921](https://openairdocs.org/sdr/CALA0001921), Dec 15, 2000: EXPANSION JOINT. CRACKED. INSPECTION FOUND EXPANSION JOINTS CRACKED AND BUCKLED AT CABIN FLOOR PANEL CNTER STA 886-939. THE EXPANSION JOINTS WERE REMOVED AND NEW EXPANSION JOINTS WERE IN - [SDR CALA0001918](https://openairdocs.org/sdr/CALA0001918), Dec 14, 2000: FLOORBEAM. GOUGED. INSPECTION FOUND LOWER SIDE OF MAIN DECK FLOORBEAM GOUGED AT STA 1174, RBL 4 AND AT STA 1193, RBL 4. REPAIRS WERE PERFORMED AT EACH LOCATION IAW SRM 53-05, FIGU - [SDR CALA0001917](https://openairdocs.org/sdr/CALA0001917), Dec 14, 2000: WEB. CRACKED. INSPECTION FOUND A 1/4 INCH CRACK IN TANG ON TORQUE BOX WEB AT STA 220 AFT OF L-1 DOOR, LONGERON 15L. A DOUBLER WAS INSTALLED IAW EA 9-5314-2-A0811 AND SRM 51-3 - [SDR CALA0001916](https://openairdocs.org/sdr/CALA0001916), Dec 14, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT SERVICE DOOR ENTRYWAY FLOOR SUPPORT CORRODED AT FS 1155 BETWEEN LT CENTER AND O/B SEAT TRACKS, LBL 44-54. - [SDR CALA0001903](https://openairdocs.org/sdr/CALA0001903), Dec 12, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 5 - [SDR CALA0001902](https://openairdocs.org/sdr/CALA0001902), Dec 12, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND LT CABIN FLOORBEAM CORRODED AROUND NUT CLIP HOLES. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 20A. - [SDR CALA0001898](https://openairdocs.org/sdr/CALA0001898), Dec 12, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 225, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 51-10-4. - [SDR CALA0001897](https://openairdocs.org/sdr/CALA0001897), Dec 11, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10- - [SDR CALA0001896](https://openairdocs.org/sdr/CALA0001896), Dec 11, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 195-200, LBL 55 AND AT STA 200-256, LBL 14. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLE - [SDR CALA0001895](https://openairdocs.org/sdr/CALA0001895), Dec 11, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10 All 85: https://openairdocs.org/deregistered/N16807-2012-02-07/reports.md --- 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.