# N33805: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2004-05-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 18, 2004 - 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: 49249 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 2, 1984 - Certificate issued: February 12, 2004 - Last registry action: February 12, 2004 - Mode S code: A3B5FD - Owner when cancelled: [Olsf LLC](https://openairdocs.org/faa-owner/OLSF%20LLC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N33805 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=33805 - Page: https://openairdocs.org/deregistered/N33805-2004-05-18 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 (49) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA2000279](https://openairdocs.org/sdr/CALA2000279), May 11, 2002: ACTUATOR. CORRODED. AFT VENTRAL STAIRS ACTUATOR LOWER TUBE, RT, IS CORRODED 2 INCHES. REPLACED RT LOWER STRUT ON VENTRAL STAIRS AND PERFORMED ADJUSTMENT AND TEST IAW MM 52-63-00. - [SDR CALA0101000](https://openairdocs.org/sdr/CALA0101000), Nov 12, 2001: BATTERY PACK. DISCHARGED. THE OVERWING EMERGENCY EXIT IDENTIFIERS ABOVE DOORS ON LT AND RT SIDE OF AIRCRAFT WERE FOUND INOPERATIVE. THE BATTERIES IN EMERGENCY BATTERY PACKS IN O/H BIN AT - [SDR CALA0100958](https://openairdocs.org/sdr/CALA0100958), Oct 17, 2001: POWER SUPPLY. DISCHARGED. BOTH LEFT AND RIGHT OVERWING EVACUATION LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM 33-53-00 PAGE 407. - [SDR CALA0100112](https://openairdocs.org/sdr/CALA0100112), Feb 10, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERON 22L AND 23L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04-38 AND - [SDR CALA0100109](https://openairdocs.org/sdr/CALA0100109), Feb 9, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1031 - 1169. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGUR - [SDR CALA0100098](https://openairdocs.org/sdr/CALA0100098), Feb 2, 2001: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 6. - [SDR CALA0100097](https://openairdocs.org/sdr/CALA0100097), Feb 2, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1117 - 1136. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED I - [SDR CALA0100096](https://openairdocs.org/sdr/CALA0100096), Feb 2, 2001: SKIN. GOUGED. INSPECTION FOUND SKIN GOUGED AT AFT CARGO DOOR LOWER EDGE OF PAN. THE RIVETS WERE REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND EA 9-5230-2-A0832. - [SDR CALA0100088](https://openairdocs.org/sdr/CALA0100088), Feb 1, 2001: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LEFT W/W FORWARD I/B (FWD OF MLG ATTACH) ANGLE T-FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51- - [SDR CALA0100083](https://openairdocs.org/sdr/CALA0100083), Jan 31, 2001: SKIN. CORRODED. INSPECTION FOUND INNER SKIN DOUBLER CORRODED AT FS 1286 BETWEEN LONGERONS 21L AND 22L. THE INNER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND - [SDR CALA0100084](https://openairdocs.org/sdr/CALA0100084), Jan 30, 2001: FRAME. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN AFT ACCESSORY COMPARTMENT FRAME UNDER RADIUS BLOCK AT LONGERON ATTACH POINT, FS 1446, LONGERON 5L. THE FRAME WAS REMOVED AND - [SDR CALA0100080](https://openairdocs.org/sdr/CALA0100080), Jan 29, 2001: PAN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE - [SDR CALA0100079](https://openairdocs.org/sdr/CALA0100079), Jan 29, 2001: FLOORBEAM. CORRODED. INSPECTION FOUND AFT LT LAV FLOORBEAM CORRODED AT STA 1322, LBL 41. THE CORROSION WAS TRIMMED OUT AND A DOUBLER, REPAIR STRIP, AND SHIM WERE INSTALLED IAW SRM 5 - [SDR CALA0100076](https://openairdocs.org/sdr/CALA0100076), Jan 27, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERONS 21L AND 22L. THE DENT WAS COLD WORKED IAW SRM 53-04-38. A REPAIR DOUBLER WAS INSTALLE - [SDR CALA0100075](https://openairdocs.org/sdr/CALA0100075), Jan 27, 2001: WEB. CORRODED. INSPECTION FOUND AFT CARGO DOOR WEB CORRODED AROUND ATTACH RIVNUT HOLES. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE CORRODED AREAS WERE REPAIRED IAW SRM 52- - [SDR CALA0100074](https://openairdocs.org/sdr/CALA0100074), Jan 26, 2001: FITTING. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR LOWER FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND - [SDR CALA0100073](https://openairdocs.org/sdr/CALA0100073), Jan 26, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERONS 17L AND 18L. THE SKIN WAS REMOVED AND REPLACED IAW SRM 53-34-0, FIGURE 2, PAGE 7, 51- - [SDR CALA0100072](https://openairdocs.org/sdr/CALA0100072), Jan 26, 2001: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, F - [SDR CALA0100071](https://openairdocs.org/sdr/CALA0100071), Jan 25, 2001: STRUCTURE. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS IN FORWARD LOWER CORNER OF LT MLG I/B DOOR. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3 - [SDR CALA0100068](https://openairdocs.org/sdr/CALA0100068), Jan 24, 2001: ANGLE. CORRODED. INSPECTION FOUND CUSP ANGLE AT L-1 DOOR, FS 200, LBL 54 CORRODED. THE CUSP ANGLE WAS REMOVED AND REPLACED IAW EA 9-5310-2-A0829 AND ECRA 5310-04094. - [SDR CALA0100067](https://openairdocs.org/sdr/CALA0100067), Jan 24, 2001: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR FITTING AND WITH UPPER INTERCOSTAL CLIP CRACKED. THE FITTING AND T-ANGLE WERE REMOVED AND A NEW FITTING AND AN - [SDR CALA0100065](https://openairdocs.org/sdr/CALA0100065), Jan 23, 2001: SKIN. DENTED. INSPECTION FOUND LT FORWARD FUSELAGE SKIN DENTED AT FS 133, L10L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 53-04, FIGURE 3 - [SDR CALA0100064](https://openairdocs.org/sdr/CALA0100064), Jan 23, 2001: SKIN. DENTED. INSPECTION FOUND FUSELAGE EXTERNAL SKIN AT FORWARD LT SIDE OF E AND E DOOR CUTOUT STA 145, L28L DENTED. THE SKIN WAS REPAIRED BY INSTALLING FILLER AND DOUBLERS - [SDR CALA0100054](https://openairdocs.org/sdr/CALA0100054), Jan 22, 2001: FITTING. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR FITTING I/B OF AFT HINGE. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-2 - [SDR CALA0100053](https://openairdocs.org/sdr/CALA0100053), Jan 22, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1032 - 1184. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA0100052](https://openairdocs.org/sdr/CALA0100052), Jan 21, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTA - [SDR CALA0100051](https://openairdocs.org/sdr/CALA0100051), Jan 21, 2001: DOOR FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK (PAST STOP DRILL) IN RT MLG DOOR SUPPORT FRAME AT STA 946, RBL 10. THE EXISTING REPAIR DOUBLERS WERE REMOVED FOR ACCESS IAW SRM - [SDR CALA0100044](https://openairdocs.org/sdr/CALA0100044), Jan 17, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 260 BETWEEN LONGERONS 24R AND 25R AND BETWEEN LONGERONS 27L AND 28L. A DOUBLER WAS INSTALLED AT EACH LOCATI - [SDR CALA0100043](https://openairdocs.org/sdr/CALA0100043), Jan 17, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 375 BETWEEN LONGERON 29L AND 30 AND AT FS 470, BETWEEN LONGERONS 20L AND 21L. A DOUBLER WAS INSTALLED AT EA - [SDR CALA0100038](https://openairdocs.org/sdr/CALA0100038), Jan 16, 2001: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 500 - 520 BETWEEN LONGERONS 20R AND 21R AND AT FS 550 - 560 BETWEEN LONGERONS 21L AND 22L. THE DENTS WERE C - [SDR CALA0100037](https://openairdocs.org/sdr/CALA0100037), Jan 16, 2001: FRAME. CRACKED. INSPECTION FOUND E&E COMPARTMENT FRAME CRACKED PAST STOP DRILL HOLE AT FS 150, L21R. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR W - [SDR CALA9901474](https://openairdocs.org/sdr/CALA9901474), Nov 6, 1999: POWER SUPPLY. INOP. INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT ROWS 23-27. THE BATTERY POWER SUPPLY AT STATION 1150 IN RT OVERHEAD BIN WAS REMOVED AND REPLACED AND O - [SDR CALA9900117](https://openairdocs.org/sdr/CALA9900117), Feb 5, 1999: SKIN. DENTED. INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 218, LONGERON 17L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02766. - [SDR CALA9900116](https://openairdocs.org/sdr/CALA9900116), Feb 5, 1999: BRACE. CRACKED. INSPECTION FOUND A CRACK OF UNSPECIFIED LENGTH IN THE LT GROUND SPOILER ACTUATOR I/B ATTACH BRACKET CROSS BRACE. A NEW CROSS BRACE WAS INSTALLED IAW SRM 51-30-5 - [SDR CALA9900107](https://openairdocs.org/sdr/CALA9900107), Feb 2, 1999: ESCAPE LINE. FRAYED. INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY ESCAPE LINES FRAYED. NEW ESCAPE LINE WAS INSTALLED IAW SRM 51-30-1 AND MM 25-61-00, FIGURE 202. - [SDR CALA9900095](https://openairdocs.org/sdr/CALA9900095), Jan 29, 1999: BEAM. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FORWARD SERVICE DOOR NR 4 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30. - [SDR CALA9900094](https://openairdocs.org/sdr/CALA9900094), Jan 29, 1999: BEAM. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN OUTBOARD RADIUS OF MAIN CABIN DOOR TOP NR 1 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9701503](https://openairdocs.org/sdr/CALA9701503), Oct 24, 1997: FCU. LEAKING. WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU AUTO SHUTDOWN WHEN CLIMBING THROUGH 28,000 FEET. THE APU WAS RESTARTED AT 26,000 - [SDR CALA9700222](https://openairdocs.org/sdr/CALA9700222), Feb 19, 1997: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND TWO EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY AT FAULT. THE POWER SUPPLY WAS REMOVED AND RE - [SDR CALA9700152](https://openairdocs.org/sdr/CALA9700152), Jan 28, 1997: DOOR PAN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN AT LOCK AFT CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A. - [SDR CALA9700147](https://openairdocs.org/sdr/CALA9700147), Jan 27, 1997: DOOR PAN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FORWARD BAGGAGE BIN DOOR PAN AT LOCK CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A. - [SDR CALA9700154](https://openairdocs.org/sdr/CALA9700154), Jan 22, 1997: FITTING. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN UPPER RIGHT FITTING AND A 1.5 INCH CRACK IN UPPER LEFT FITTING AT MAIN BAGGAGE BIN STA 826. THE FITTINGS WERE REPLACED IAW - [SDR CALA9700153](https://openairdocs.org/sdr/CALA9700153), Jan 22, 1997: BELT FRAME. CORRODED. INSPECTION FOUND BELT FRAME LOWER CHANNEL CORRODED AT STA 1307, LONGERON 27R TO 27L. THE CORRODED SECTION OF BELT FRAME WAS CUT OUT, A NEW SEGMENT OF FRAME AND - [SDR CALA9700151](https://openairdocs.org/sdr/CALA9700151), Jan 21, 1997: DOOR PAN. CRACKED. INSPECTION FOUND A 1.25 INCH CRACK AT LOWER HINGE CUTOUT OF MAIN CABIN DOOR PAN. THE PAN WAS REPLACED IAW SRM 52-11-0. - [SDR CALA9700150](https://openairdocs.org/sdr/CALA9700150), Jan 20, 1997: ANGLE. CORRODED. INSPECTION FOUND Z-ANGLE AND FLOOR MOUNTS CORRODED AT AFT SERVICE DOOR THRESHOLD. A NEW Z-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. - [SDR CALA9700149](https://openairdocs.org/sdr/CALA9700149), Jan 20, 1997: RIB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT WING LEADING EDGE RIB JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 270. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5710-01776. - [SDR CALA9700148](https://openairdocs.org/sdr/CALA9700148), Jan 20, 1997: RIB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE RIB, TWO RIBS OUTBOARD OF 8R SLAT TRACK, STA XRS 277. A DOUBLER WAS INSTALLED IAW SRM 57-01. - [SDR CALA9600647](https://openairdocs.org/sdr/CALA9600647), May 25, 1996: ACTUATOR. INOPERATIVE. THE NOSE GEAR WAS SLOW TO RETRACT AFTER TAKEOFF. THE RED LIGHT EXTINGUISHED AND DOORS CLOSED AFTER APPROXIMATELY 20 TO 25 SECONDS. THE FLIGHT WAS CONTINUED AND - [SDR CAL950114](https://openairdocs.org/sdr/CAL950114), Feb 10, 1995: CIRCUIT BREAKER. FAILED. FLT NR 0246 - IAH - SEVERAL LEFT AC BUS CIRCUIT BREAKERS BEGAN POPPING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT ## Other aircraft with N33805 - [Cancelled 2008-04-21](https://openairdocs.org/deregistered/N33805-2008-04-21): Hawker Beechcraft 390, S/N RB-235. Exported to Germany. Owner: [Hawker Beechcraft Corp](https://openairdocs.org/faa-owner/HAWKER%20BEECHCRAFT%20CORP), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - [Cancelled 1948-11-24](https://openairdocs.org/deregistered/N33805-1948-11-24): Aeronca 65-TL, S/N 9491. Owner: [Jack Powley](https://openairdocs.org/faa-owner/JACK%20POWLEY), [Mifflintown, PA](https://openairdocs.org/faa-place/PA/Mifflintown) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N33805-undated): Piper PA-34-200T, S/N 347570164 --- 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.