# N9305N: 1986 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2007-05-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 21, 2007 - Exported to: Cambodia - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - 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: 49395 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 30, 1995 - Certificate issued: May 21, 2007 - Last registry action: May 21, 2007 - Mode S code: ACE8BD - Owner when cancelled: [Compass Capital Corp](https://openairdocs.org/faa-owner/COMPASS%20CAPITAL%20CORP) - 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/N9305N - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9305N - Page: https://openairdocs.org/deregistered/N9305N-2007-05-21 From the FAA registry file of November 5, 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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20040847](https://openairdocs.org/sdr/AALA20040847), Aug 14, 2004: CONNECTOR. SHORTED. INFLIGHT T1261 DFW SAT/14 AT 26,000 FEET LEVEL GOT AN INDICATION OF AFT CARGO FIRE. FOLLOWED QRH AND BOTH BOTTLES FIRED. LANDED WITHOUT INCIDENT. REPLACED NR 1 - [SDR ZW0A0212902](https://openairdocs.org/sdr/ZW0A0212902), Dec 26, 2002: VALVE. DEFECTIVE. NOSE GEAR STRUT FLAT NOT ALLOWING GEAR TO RETRACT. REMOVED AND REPLACED SCHRADER VALVE AND RESERVICED STRUT. - [SDR ZW0A0212801](https://openairdocs.org/sdr/ZW0A0212801), Dec 23, 2002: SEAL. LOOSE. BOTH HEAT EXCHANGERS LEAKING NOT ALLOWING AIRCRAFT TO PRESSURIZE. TIGHTENED SEALS ON BOTH HEAT EXCHANGERS. - [SDR ZW0A0210401](https://openairdocs.org/sdr/ZW0A0210401), Oct 8, 2002: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTING BETWEEN ROWS 15 TO 21 WERE FLASHING ON AND OFF DURING FLIGHT. REPLACED THE POWER SUPPLY. - [SDR ZW0A0206201](https://openairdocs.org/sdr/ZW0A0206201), Jun 11, 2002: FITTING. CRACKED. DURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1361 BETWEEN LONGERON 23L AND 24L. FABRICATED AND INSTALLED NEW FORMER FOOT SECTION PER SPM 6-70-01, PAG - [SDR ZW0A0206003](https://openairdocs.org/sdr/ZW0A0206003), Jun 5, 2002: FLOORBEAM. DAMAGED. DURING CHECK-C MAINT THE FLOOR BEAM CAP WAS GROUND BEYOND LIMITS AT STA 1322, LBL 34. REPAIRED FLOOR BEAM CAP PER SRM 53-05, FIG 20A. - [SDR ZW0A0205902](https://openairdocs.org/sdr/ZW0A0205902), Jun 4, 2002: TIE CLIP. CRACKED. DURING CHECK-C CRACKED TIE CLIP AT STA 1437 VERT BULKHEAD TO LONG 3R. REPLACED TIE CLIP PER SPM 6-70-01. - [SDR ZW0A0205303](https://openairdocs.org/sdr/ZW0A0205303), May 22, 2002: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN LATERAL FLOOR BEAM AT STA 180, FROM RBL 8 TO RBL 43. FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 51-01, PAGE 1 ITEM C - [SDR ZW0A0205302](https://openairdocs.org/sdr/ZW0A0205302), May 17, 2002: STRINGER. CRACKED. DURING CHECK-C MAINT STRINGER 3 LT WAS CRACKED AT STA 160, ABOVE ELECT PANEL. REPAIRED LONGERON 3 PER SRM 53-02, FIG 18. - [SDR ZW0A0205301](https://openairdocs.org/sdr/ZW0A0205301), May 17, 2002: DOOR FRAME. CRACKED. DURING CHECK-C MAINT THE RT FWD GALLEY SERVICE DOOR HAD A CRACKED DOUBLER LOWER HINGE ARM. REPLACED WITH NEW FRAME PART PER SPM 6-70-01. - [SDR ZW0A0205203](https://openairdocs.org/sdr/ZW0A0205203), May 16, 2002: LONGERON. CRACKED. DURING CHECK-C MAINT THE NUMBER 4 LT LONGERON WAS CRACKED AT STA 160. REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-02, FIG 18. - [SDR ZW0A0111203](https://openairdocs.org/sdr/ZW0A0111203), Nov 25, 2001: WIRE. BROKEN. DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RH SIDE. - [SDR ZW0A011123](https://openairdocs.org/sdr/ZW0A011123), Nov 25, 2001: WIRE. BROKEN. DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RT SIDE. - [SDR ZW0A0107502](https://openairdocs.org/sdr/ZW0A0107502), Aug 25, 2001: BATTERY PACK. THE CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATED WHEN POWER WAS REMOVED FROM THE AIRCRAFT. REPLACED THE BATTERY PACK. CHECK-C 5-7-01 STL. --CLOSED-- - [SDR ZW0A0107101](https://openairdocs.org/sdr/ZW0A0107101), Aug 17, 2001: LAMP. DURING LANDING THE RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, DUE TO BURNED OUT BULB. REPLACED LIGHT BULB P/N 387.LAST CHECK C 05/07/01 STL. --- CLOSED - - [SDR ZW0A0106303](https://openairdocs.org/sdr/ZW0A0106303), Aug 4, 2001: BATTERY PACK. DISCHARGED. DURING MAINTENANCE THE AFT FLOOR EGRESS LIGHTS WERE INOP DUE TO WEAR. REPLACED BATTERY PACK P/N5822-2 AND FEEDER JUMPER CABLE PER MM 33-51-01. - [SDR ZW0A0103202](https://openairdocs.org/sdr/ZW0A0103202), Jun 8, 2001: BATTERY PACK. DISCHARGED. IN FLIGHT THE EGRESS LIGHTS AT ROWS 15 TO 22 ILLUMINATED. REPLACED THE BATTER PACK. CHECK-C 5-7-01 STL. - [SDR ZW0A0102705](https://openairdocs.org/sdr/ZW0A0102705), Jun 2, 2001: POWER SUPPLY. DISCHARGED. AN OVERWING EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-7-01 STL. - [SDR ZW0A0102302](https://openairdocs.org/sdr/ZW0A0102302), May 24, 2001: BATTERY. DISCHARGED. THE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 5-7-01 STL. - [SDR TWAA0106301](https://openairdocs.org/sdr/TWAA0106301), Apr 9, 2001: WIRE. BROKEN. THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE. REPAIRED A BROKEN WIRE IN CEILING OF AFT LEFT LAVATORY. CHECK-C 2-5-01 JFK. - [SDR TWAA0010009](https://openairdocs.org/sdr/TWAA0010009), Jun 20, 2000: FRAME. CRACKED. DURING CHECK-C MAINT, THE FAIRING SUPPORT FRAME WAS CRACKED AT STA 946, RBL 7 AND LBL 7. REPAIRED BOTH PER SRM 53-05, FIG 81, PAGE 267. - [SDR TWAA0010008](https://openairdocs.org/sdr/TWAA0010008), Jun 16, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, THE FLOORBEAM WAS CORRODED AT STA 1323, LBL 22. REPAIRED FLOORBEAM PER SRM 53-05 PAGE 31 FIG 20A. - [SDR TWAA0010503](https://openairdocs.org/sdr/TWAA0010503), Jun 13, 2000: SKIN. CORRODED. DURING CHECK-C MAINT, THE SURFACE AT LE AT TELESCOPING ANTI-ICE DUCT, 0.045 IN MATERIAL WAS REMOVED FOR CORROSION REMOVAL. MATERIAL THICKNESS IS 0.250 IN PER SR - [SDR TWAA0009710](https://openairdocs.org/sdr/TWAA0009710), Jun 13, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON FLOORBEAM AT STA 1309, LOCATED 6 INCHES LEFT OF CENTER LINE. REMOVED AND REPLACED FLOOR SUPPORT. USED TWA (P/N 56-2789) - [SDR TWAA0009708](https://openairdocs.org/sdr/TWAA0009708), Jun 12, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, FOUND FORMER RING AT STA 1309 CORRODED BETWEEN LONGERONS 29L AND 29R. REMOVED CORROSION PER SPM 6-80-01. TRIMMED CORRODED AREA OVER LONGER - [SDR TWAA0009611](https://openairdocs.org/sdr/TWAA0009611), Jun 12, 2000: ATTACH ANGLE. CRACKED. DURING CHECK-C MAINT, THE ATTACH ANGLE ON BOTTOM OF DORSAL FIN CRACKED THROUGH THE SCREW HOLE, LT SIDE APROX STA 1420. INSTALLED REPAIR ANGLE PER SRM 53-01 PAGE - [SDR TWAA0009610](https://openairdocs.org/sdr/TWAA0009610), Jun 12, 2000: WEB. CORRODED. DURING CHECK-C MAINT, THE MEMBRANE AT LONGERON 18L BETWEEN STATION 218 TO 237, O/B OF CHAIR TRACK, WAS CORRODED. FABRICATED NEW PART PER DRAWING 5930544 AND 993 - [SDR TWAA0009709](https://openairdocs.org/sdr/TWAA0009709), Jun 11, 2000: STRUCTURE. DAMAGED. DURING CHECK-C MAINT, FOUND CLASS 3 REPAIR AT STA 200 TO 225, LONGERON 4L TO 6L. REPAIRED PER SRM 53-04 FIG 12B, SHEETS 9 AND 10. MESSAGE SENT TO ENGINEERING PE - [SDR TWAA0009707](https://openairdocs.org/sdr/TWAA0009707), Jun 11, 2000: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, FOUND INTERGRANULAR CORROSION ON NUMBER 4 CHAIR TRACK, RBL 22 INCHES, STA 1144. INSTALLED SPLICE REPAIR PER SRM 53-05, FIG 4F. - [SDR TWAA0009612](https://openairdocs.org/sdr/TWAA0009612), Jun 11, 2000: ATTACH ANGLE. CRACKED. DURING CHECK-C MAINT, THE RT DORSAL FIN ATTACH ANGLE ON FUSELAGE STA 1420 WAS CRACKED. INSTALLED NEW ANGLE PER DOUGLAS DRAWING 174968, PER SPM 6-70-01 WITH FAST - [SDR TWAA0009609](https://openairdocs.org/sdr/TWAA0009609), Jun 8, 2000: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, CABIN STA 1155 LRL 47 HAD CORROSION ON TRACK NUMBER 2. REPLACED TRACK SECTION PER SRM 53-05, FIG 4F. - [SDR TWAA0009608](https://openairdocs.org/sdr/TWAA0009608), Jun 8, 2000: FLOORBOARD. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOOR PANEL SUPPORT AT STA 200, BL 0 TO RBL 50. REMOVED CORROSION PER SPM 6-80-1. REPLACED SUPPORT EXTRUSION PER - [SDR TWAA0009607](https://openairdocs.org/sdr/TWAA0009607), Jun 8, 2000: SEAT TRACK. CORRODED. DURING CHECK-C MAINT, NUMBER 3 CHAIR TRACK FROM STA 1031 TO 1309 HAD CORROSION BEYOND LIMITS. REPLACED NUMBER 3 CHAIR TRACK PER IPC 53-40-00 FIG 19B AND SRM 53- - [SDR TWAA0012105](https://openairdocs.org/sdr/TWAA0012105), Jun 7, 2000: SPAR. CORRODED. DURING CHECK-C MAINT ON THE RT WING, CORROSION WAS FOUND ON THE REAR SPAR BETWEEN CENTER AND O/B AILERON HINGE. FABRICATED ACCORDING TO SRM 59-09 FIG 5. FABRICA - [SDR TWAA0009604](https://openairdocs.org/sdr/TWAA0009604), Jun 7, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOORBEAM, LEFT AFT LAV STA 1338, 20 INCH LBL AND 30 IN LBL. CORROSION REMOVED PER SPM 6-80-01 PAGE 31 TO 42, AND - [SDR TWAA0009606](https://openairdocs.org/sdr/TWAA0009606), Jun 6, 2000: SEAT TRACK. WORN. DURING CHECK-C MAINT, THE FIRST OFFICER''S RT FWD CHAIR TRACK WAS WORN ON UPPER AND LOWER SURFACES. REPLACED FLOOR TRACK PER MM 53-40-01 PAGE 203. - [SDR TWAA0009406](https://openairdocs.org/sdr/TWAA0009406), Jun 6, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, THE AFT CARGO BIN HAD CORROSION ON FORMER RING AT STA 1271, LONGERON 30. AT STA 1271 ON FORMER RING AT LONGERON 30 REMOVED CORROSION PER S - [SDR TWAA0009405](https://openairdocs.org/sdr/TWAA0009405), Jun 6, 2000: BRACKET. CRACKED. DURING CHECK-C MAINT, A FUSELAGE ANGLE BRACKET WAS CRACKED AT STA 946, LBL 7 INSIDE KEEL BEAM LOWER FWD CORNER. FABRICATED PART FROM 7075-T6 PER SPM AND PRINT 9 - [SDR TWAA0009605](https://openairdocs.org/sdr/TWAA0009605), Jun 5, 2000: STIFFENER. CRACKED. DURING CHECK-C MAINT AT STA 996 BODY FAIRING STIFFENER BOTTOM CORD HAD A 6.5 INCH CRACK AND THE REPAIR ANGLE HAD 1.5 INCH CRACK. STOP DRILLED CRACKS PER SRM 53- - [SDR TWAA0009304](https://openairdocs.org/sdr/TWAA0009304), Jun 5, 2000: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT AT CABIN STA 1155, LBL 33, FOUND CORROSION ON FLOOR SUPPORT BETWEEN NUMBER 2 AND 3 TRACKS. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53- - [SDR TWAA0009005](https://openairdocs.org/sdr/TWAA0009005), Jun 4, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, FOUND CABIN MEMBRANE CORRODED AT STA 503 TO 522, LONGERON 18L. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01, PAGE 9. - [SDR TWAA0009004](https://openairdocs.org/sdr/TWAA0009004), Jun 1, 2000: STRAP. CORRODED. DURING CHECK-C MAINT, THE RT WING UPPER O/B SPOILER, O/B END, TRAILING EDGE SUPPORT STRAP HAD CORROSION. REMOVED DAMAGED SUPPORT STRAP AND REPLACED WITH NEW PAR - [SDR TWAA9914604](https://openairdocs.org/sdr/TWAA9914604), Oct 28, 1999: BATTERY. DISCHARGED. DURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHTS INOP AT ROWS 28L AND 28R THROUGH ROWS 26L AND R AND 5 EACH INOP IN THE TAIL SECTION. REPLACED BATTERY. AC01 9- - [SDR TWAA9814305](https://openairdocs.org/sdr/TWAA9814305), Sep 6, 1998: COALESCER BAG. DIRTY. STRONG ODOR WITH SMOKY HAZE IN COCKPIT AND CABIN AFTER TAKEOFF. FLT RETURNED TO SFO. CHECKED ALL ACFT COMPARTMENTS, CHECKED APU CHECK VALVE, AND ACM OUTLETS FOR - [SDR TWAA9804603](https://openairdocs.org/sdr/TWAA9804603), Mar 27, 1998: COALESCER. DIRTY. LGA - FLT 293 - AFTER TAKEOFF SMOKE FILLED CABIN AND COCKPIT WITH ODOR AND LIGHT HAZY SMOKE. FLIGHT RETURNED TO LGA. FOUND AIR COND PACK COALESCER BAGS CLOGGED - [SDR TWAA9808816](https://openairdocs.org/sdr/TWAA9808816), Jun 13, 1997: SKIN. GOUGED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND GOUGE IN SKIN PANEL AT LONGERON 22, STATION 1211 TO 1117. REPAIRED SKIN PANEL PER SRM 53-04, FIG 12B. (M) - [SDR TWAA9806003](https://openairdocs.org/sdr/TWAA9806003), Jun 13, 1997: SKIN. GOUGED. MCI - DURING C-CHECK MAINTENANCE FOUND A DEEP GOUGE ON LEFT SIDE OF FUSELAGE, LONGERON 18 TO 26, STATION 1211 TO 1338. REPLACED SKIN PANEL, LONGERON 18 TO 26, S - [SDR TWAA9753002](https://openairdocs.org/sdr/TWAA9753002), Mar 8, 1997: SKIN. DAMAGED. STL - DURING SPECIAL CHECK, FOUND DAMAGE ON LEFT AFT FUSELAGE, AFT OF FLAP. REPAIRED PER ARA 11135A AND SRM 53-04. (M) - [SDR 96ZZZM1068](https://openairdocs.org/sdr/96ZZZM1068), Jun 2, 1996: SCHRADER VLV. FAILED. MSY - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. FOLOWED ORH PROCEDURES. FOUND NOSE LANDING GEAR STRUT DEFLATED AND A DEF - [SDR 96ZZZX3268](https://openairdocs.org/sdr/96ZZZX3268), May 23, 1996: COALESCER BAG. DIRTY. MCI - FLT 667 - DURING CLIMB WHEN ENGINE ANTI-ICE WAS TURNED ON, A BURNING ODOR WAS NOTICED IN THE CABIN. TURNED OFF ENGINE ANTI-ICE. FOUND DIRTY COALESCER, MFG ## 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 19960813027439I](https://openairdocs.org/incident/19960813027439I), Aug 13, 1996: Doug DC983 (N9305N), Wichita, KS. Narrative: aircraft N9305N, an MD-180, en route from st. louis, Missouri to albuquerque, new Mexico, 40 miles south of Wichita at 35K, no. 1 engine started… ## Other aircraft with N9305N - [Registered now](https://openairdocs.org/aircraft/N9305N): Cessna 172S, S/N 172S11132, built 2011 - [Cancelled 1990-09-14](https://openairdocs.org/deregistered/N9305N-1990-09-14): Piper PA-28R-200, S/N 28R35005. Exported to Canada --- 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.