# N9306T: 1987 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2009-10-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 14, 2009 - Exported to: Afghanistan - 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: 49567 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 8, 1996 - Certificate issued: July 23, 2008 - Last registry action: July 23, 2008 - Mode S code: ACE8E5 - Owner when cancelled: [Global Aircraft Solutions Inc](https://openairdocs.org/faa-owner/GLOBAL%20AIRCRAFT%20SOLUTIONS%20INC) - Location: [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson) - Owner type: Corporation - Owner's area on the map: 32.1478° N, 110.9354° W: Placed by OpenAirDocs at the center of ZIP code 85706, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N9306T - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9306T - Page: https://openairdocs.org/deregistered/N9306T-2009-10-14 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 (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20041249](https://openairdocs.org/sdr/AALA20041249), Dec 25, 2004: BATTERY PACK. DISCHARGED. DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11. SYSTEM GROUND CHECKE - [SDR AALA20041068](https://openairdocs.org/sdr/AALA20041068), Oct 22, 2004: COMPRESSOR. STALLED. T512/22 RT ENGINE COMPRESSOR STALL CLIMBING THROUGH 17,000 MEAN SEA LEVEL. AIRSPEED 320 KTS, EGT 700-750 DEGREES C. DID NOT SHUTDOWN TIL TOUCHDOWN. ALL OTHER IN - [SDR TWAA0104601](https://openairdocs.org/sdr/TWAA0104601), Mar 9, 2001: POWER SUPPLY. DISCHARGED. THE EGRESS LIGHTS WERE INOPERATIVE AFT OF THE AFT GALLEY. REPLACED THE POWER PACK. CHECK-C 2-23-01 STL. - [SDR TWAA0018103](https://openairdocs.org/sdr/TWAA0018103), Nov 13, 2000: PLUG. MISSING. THE EMERGENCY EXIT INDICATOR WAS MISSING AT ROW 21, RT SIDE OF CABIN. RE-INSTALLED INDICATOR. CHECK-C 5-10-00 MCI. - [SDR TWAA0007404](https://openairdocs.org/sdr/TWAA0007404), May 7, 2000: HANDLE. CRACKED. FWD CARGO DOOR, DOOR HANDLE CRACKED. NDT CONFIRMED. REMOVED AND REPLACED DOOR HANDLE AND SPRING PER MM 52-31-00. CK-C 05/07/00 MCI. - [SDR TWAA0006912](https://openairdocs.org/sdr/TWAA0006912), Apr 28, 2000: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION AT INTERCOSTAL DOUBLERS, STA 1212 TO 1231 AND STA 1212 AT LONGERON 229R. REMOVED FASTENERS AND DOUBLERS. REMOVED CORROSION - [SDR TWAA0006911](https://openairdocs.org/sdr/TWAA0006911), Apr 28, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, STA 1212 FORMER RING HAD CORROSION FROM LONGERON 28L TO 29R. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED AREA PER SRM 51-10-03. - [SDR TWAA0006910](https://openairdocs.org/sdr/TWAA0006910), Apr 28, 2000: FRAME. CORRODED. DURING CHECK-C MAINT, STA 1231 FORMER RING HAD CORROSION FROM LONGERON 29L TO 29R. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED AREA PER SRM 51-10-03. - [SDR TWAA0006909](https://openairdocs.org/sdr/TWAA0006909), Apr 28, 2000: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON TOP AND BOTTOM OF FLOOR BRACE AT STA 1212, BETWEEN LONGERON 29R AND 28L. REMOVED CORROSION PER SPM 6-80-01. TREATED ARE - [SDR TWAA0006908](https://openairdocs.org/sdr/TWAA0006908), Apr 28, 2000: LONGERON. CORRODED. DURING CHECK-C MAINT, FOUND LONGERON 30 HAD CORROSION AROUND RIVETS FROM STA 1231 TO 1271. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED AREA PER SRM 51 - [SDR TWAA0006803](https://openairdocs.org/sdr/TWAA0006803), Apr 26, 2000: SPLICE. CORRODED. DURING CHECK-C MAINT, LONGERON NUMBER 30 SPLICE WAS CORRODED AT FWD AND AFT ENDS, STA 1243 AND 1196. REPLACED NUMBER 30 LONGERON SPLICE AT STA 1243 AND 1196 PER - [SDR TWAA0006612](https://openairdocs.org/sdr/TWAA0006612), Apr 24, 2000: GALLEY TRACK. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON TRACK NR 5 AT NUMBER 1 GALLEY, STA 200 TO 256. REPLACED SECTION OF NR 5 SEAT TRACT STA 200 TO 256. SPLICED AT STA 256 P - [SDR TWAA0006611](https://openairdocs.org/sdr/TWAA0006611), Apr 24, 2000: STRUCTURE. CRACKED. DURING CHECK-C MAINT AT THE LT MAIN LANDING GEAR, CORNER BRACKET RT FWD BETWEEN MLG DOORS, FWD I/B CORNER OF RT MLG DOOR IS CRACKED AT STA 937. INSTALLED NEW CO - [SDR TWAA0006428](https://openairdocs.org/sdr/TWAA0006428), Apr 24, 2000: SKIN. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON LOWER FUSELAGE SKIN, STA 770, STRINGER 12R. INSTALLED EXTERNAL DOUBLER PER SRM 53-04, FIG 12B. - [SDR TWAA0006427](https://openairdocs.org/sdr/TWAA0006427), Apr 22, 2000: GALLEY TRACK. CORRODED. DURING CHECK-C MAINT, THE GALLEY TRACK NUMBER 6 AT FWD END OF STA 218 HAD CORROSION ON THE TRACK. CUT AND SPLICED TRACK TO REMOVE CORROSION PER SRM 53-05, FIG 4 - [SDR TWAA0006426](https://openairdocs.org/sdr/TWAA0006426), Apr 22, 2000: PLATE. CORRODED. DURING CHECK-C MAINT, THE LT SIDE STABILIZER WRAP AROUND SEAL PLATE HAD SEVERAL SCREW HOLES WITH CORROSION. MADE DOUBLER PER SRM 53-01. REMOVED CORROSION BY SPO - [SDR TWAA0006425](https://openairdocs.org/sdr/TWAA0006425), Apr 21, 2000: SKIN. CORRODED. DURING CHECK-C MAINT, FUSELAGE SKIN AND INTERIOR DOUBLER HAD LIGHT CORROSION BETWEEN THEM AT STA 1307, ABOVE STRINGER 22L. REMOVED LIGHT CORROSION ON SKIN AND I - [SDR TWAA0006424](https://openairdocs.org/sdr/TWAA0006424), Apr 21, 2000: STRUCTURE. CRACKED. DURING CHECK-C MAINT THE FORWARD CARGO DOOR, WHERE FWD AND AFT LATCH CAMS COME THRU THE DOOR, FITTINGS ARE WORN AND LOCK BOLT REQUIRED WORK. REMOVED DAMAGED HUC - [SDR TWAA0006423](https://openairdocs.org/sdr/TWAA0006423), Apr 21, 2000: LATCH. CRACKED. DURING CHECK-C MAINT, THE FWD CARGO DOOR, AFT SIDE OF DOOR, HAD CRACK AT LATCH CAM ON BOTH INSIDE AND OUTSIDE PAN. INSTALLED DOUBLER PER 52-05, FIG 50 ON INSIDE - [SDR TWAA0006429](https://openairdocs.org/sdr/TWAA0006429), Apr 20, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT, AT STA 1322, RBL 17 TO RBL 51, LEVEL 2 CORROSION ON TOP OF FLOOR BEAM. REPAIRED AS INSTRUCTED ON ARA 16962. REMOVED CORROSION PER SPM 6-80 - [SDR TWAA0006907](https://openairdocs.org/sdr/TWAA0006907), Apr 18, 2000: SKIN. DENTED. DURING CHECK-C MAINT, FOUND FUSELAGE SKIN DENT AT STA 446, 0.027 DEEP, .0312 INCH FROM EDGE OF ALTERNATE STATIC PORT LOWER AFT PERIMETER. REPAIRED PER BOEING ME - [SDR TWAA0006422](https://openairdocs.org/sdr/TWAA0006422), Apr 18, 2000: STRUCTURE. CRACKED. DURING CHECK-C MAINT, THE AFT CARGO DOOR HAD CRACKS UNDER DOOR SEAL, TOP AFT SIDE OF DOOR LATCH. REPAIRED CRACKS UNDER DOOR SEAL ON AFT CARGO DOOR PER SRM 52-05 - [SDR TWAA0006421](https://openairdocs.org/sdr/TWAA0006421), Apr 18, 2000: RIB. CRACKED. DURING CHECK-C MAINT, TIE CLIP WAS CRACKED AT LT WING FRONT SPAR TO RIB AT UPPER T/E, 9 INCHES I/B OF NUMBER 7 TRACK, AFT OF NR 2 L/E SLAT. REPLACED CLIP. RIB F - [SDR TWAA0006102](https://openairdocs.org/sdr/TWAA0006102), Apr 16, 2000: FRAME. CORRODED. DURING C CHECK, STA 1308 FORMER RING HAD CORROSION FROM STRINGER 24 LT, TO 24 RT, AFT SIDE. REMOVED CORROSION PER SRM 51-10-3 AND SPM 6-80-1. INSTALLED REPAIR P - [SDR TWAA0006111](https://openairdocs.org/sdr/TWAA0006111), Apr 14, 2000: FLOORBEAM. CRACKED. DURING C CHECK, FOUND CRACK IN MEMBRANE AT STA 1280, AND 1296 TO 1309, LONGER 18 LT. STOP DRILLED CRACKS. INSTALLED REPAIR DOUBLER OVER CRACKED MEMBRANE AND INS - [SDR TWAA0005806](https://openairdocs.org/sdr/TWAA0005806), Apr 6, 2000: ANGLE. CRACKED. DURING C CHECK, MAINT FOUND A CRACK AT DOUBLER ANGLE FWD SIDE OF REAR BULKHEAD, BELOW LONGERON 1. STOP DRILLED TO QUARTER INCH. REPAIRED WITH 2 EA 0.025 THICK D - [SDR TWAA0005805](https://openairdocs.org/sdr/TWAA0005805), Apr 3, 2000: FLOORBEAM. CORRODED. DURING C CHECK, MAINT CABIN FLOOR MEMBRANE LOWER SURFACE, AT STA 200 AFT SIDE OF FLOORBEAM, AT BL 0 WAS CORRODED. REMOVED CORRODED FLOOR MEMBRANE AT STA 200 TO - [SDR TWAA0005804](https://openairdocs.org/sdr/TWAA0005804), Apr 3, 2000: FLOORBEAM. CORRODED. DURING C CHECK, MAINT CABIN FLOOR MEMBRANE LOWER SURFACE AT AFT SIDE OF STA 200 FLOORBEAM, RBL 22, WAS CORRODED. REMOVED CORRODED MEMBRANE AT STA 200 TO 218, LB - [SDR TWAA0005502](https://openairdocs.org/sdr/TWAA0005502), Mar 30, 2000: ANGLE. CORRODED. DURING CHECK-C MAINT AT STA 434 FOUND LEVEL 2 CORROSION ON T ANGLE FWD END OF INTERCOSTAL, LONGERON 29R. INSTALLED NEW T ANGLE (P/N 491258-501). SECURED TO STRU - [SDR TWAA0005501](https://openairdocs.org/sdr/TWAA0005501), Mar 28, 2000: TIE CLIP. CRACKED. DURING CHECK-C MAINT ON THE RT WING, THE TIE CLIP FROM RIB TO FRONT SPAR WAS CRACKED AT UPPER T/E 26 INCHES O/B OF NR 11 L/E TRACK. CONFIRMED BY NDT. REPLACED R - [SDR TWAA0005008](https://openairdocs.org/sdr/TWAA0005008), Mar 24, 2000: CLIP. CORRODED. DURING CHECK-C MAINT, FOUND DELAMINATION CORROSION PART OF CLIP/RETAINERS FOR SEAL BOTTOM OF AIRSTAIR DOOR. INSTALLED 2 NEW PRE-FABRICATED L ANGLES FROM 7075-T6 - [SDR TWAA0002902](https://openairdocs.org/sdr/TWAA0002902), Feb 16, 2000: ENGINE. FAILED. THE RIGHT ENGINE FAILED AT 12,000 FEET IN CLIMB WITH A LOUD BANG. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO STL. FOUND TURBINE HAD FAILED WITH ENGINE CASE PEN - [SDR TWAA9912801](https://openairdocs.org/sdr/TWAA9912801), Sep 13, 1999: LAMP. FAILED. THE AFT STAIR EMERGENCY LIGHT AND THE EGRESS LIGHT AT ROW 33 WERE INOPERATIVE. RELAMPED THE TWO AFT STAIR LIGHTS, AND RECONNECTED THE EGRESS STRIP AT ROW 33. CH - [SDR TWAA9911102](https://openairdocs.org/sdr/TWAA9911102), Aug 7, 1999: TIRE. FAILED. DURING TAKEOFF AT SJC, THE NUMBER 1 TIRE COMPLETELY SEPARATED FROM THE WHEEL, CAUSING FAILURE OF THE RH HYDRAULIC SYSTEM. DURING THE LANDING AT SFO THE NUMBER 2 - [SDR TWAA9814601](https://openairdocs.org/sdr/TWAA9814601), Sep 9, 1998: SAFETY STRAP. OUT OF POSITION. ON CLIMB-OUT, R1 DOOR HAD AN AIR NOISE. SAFETY STRAP CAUGHT IN DOOR. STRAP WAS STOWED. CHECK-C1. - [SDR TWAA9814102](https://openairdocs.org/sdr/TWAA9814102), Sep 1, 1998: FUSE. FAILED. THE RT HYD SYSTEM FAILED DURING GEAR RETRACTION AFTER TAKEOFF. COMPLETE FLUID LOSS FROM RT SIDE. RT HYD PUMP LATER FAILED. FLT RETURNED TO STL. REPLACED NR 3 BR - [SDR TWAA9809407](https://openairdocs.org/sdr/TWAA9809407), Mar 16, 1998: SUPPORT. CRACKED. MCI - DURING CHECK-C, MAINTENANCE FOUND AFT END OF LT MLG DOOR HINGE AND ABOVE DOORWAY FRAME SUPPORT BRACE WITH ID CRACKED. REPLACED SUPPORT BRADE PER SRM 51-01 - [SDR TWAA9803201](https://openairdocs.org/sdr/TWAA9803201), Mar 5, 1998: VANE. DAMAGED. LAX - FLT 467 - AT APPROX 2000 FT LEFT ENGINE FAILED. RETURNED LAX. MADE SMOOTH OVERWEIGHT LANDING. FOUND TURBINE FAILURE INCLUDING LOSS OF TAIL CONE. CHANGED E - [SDR TWAA9711201](https://openairdocs.org/sdr/TWAA9711201), Sep 12, 1997: CLAMP. LOOSE. STL - FLT 118 - DURING CLIMB, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. TIGHTENED CLAMPS ON THE LEFT HAND AUGMENTATION VALVE. OPERATIONAL CHECK N - [SDR TWAA9766002](https://openairdocs.org/sdr/TWAA9766002), Jun 9, 1997: SPRAY DEFLECTOR. LOOSE. STL - FLT 121 - DURING CLIMB, NOSE GEAR UNSAFE LIGHT ILLUMINATED. TIGHTENED AND RESAFTIED AFT BOLTS ON NOSE GEAR SPRAY DEFLECTOR AND CLEANED AND LUBRICATED GEAR - [SDR 96ZZZX3655](https://openairdocs.org/sdr/96ZZZX3655), May 25, 1996: HYD PUMP. FAILED. STL - FLT 134 - DURING CRUISE, LEFT ENGINE HYDRAULIC PUMP FAILED. AIRCRAFT RETURNED TO AIRPORT. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP DUE TO A SHEARED ## Other aircraft with N9306T - [Cancelled 1991-08-09](https://openairdocs.org/deregistered/N9306T-1991-08-09): Piper PA-38-112, S/N 3878A0016. Owner: [Vandenberg Airport Inc](https://openairdocs.org/faa-owner/VANDENBERG%20AIRPORT%20INC), [Tampa, FL](https://openairdocs.org/faa-place/FL/Tampa) --- 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.