# N907TW: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2007-03-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 1, 2007 - Exported to: South Africa - Status when cancelled: Sale reported - 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: 49165 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 31, 1983 - Last registry action: January 10, 2007 - Mode S code: AC8AEB - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N907TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=907TW - Page: https://openairdocs.org/deregistered/N907TW-2007-03-01 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 (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0303209](https://openairdocs.org/sdr/ZW0A0303209), Mar 18, 2003: LIGHT. INOPERATIVE. THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE 20 INCH FLEX ASSEMBLY. CHECK-C 1-30-03 STL. - [SDR ZW0A0302702](https://openairdocs.org/sdr/ZW0A0302702), Feb 22, 2003: A/C PACK. CONTAMINATED. AT GATE VISIBLE SMOKE AND SMOKE SMELL IN AFT OF AC AFTER TURNING ON PACKS DUE TO POSSIBLE DE-ICER FLUID CONTAMINATION. TURNED OFF PACKS AND REPLACED LT AND RT W - [SDR ZW0A0200801](https://openairdocs.org/sdr/ZW0A0200801), Jan 16, 2002: BATTERY PACK. THE AFT CABIN EMERGENCY LIGHTS STAYED ILLUMINATED WITH THE COCKPIT SWITCH SELECTED OFF. REPLACED THE BATTERY PACK. CHECK-C 6-15-01 MCI. --CLOSED-- - [SDR ZW0A0103003](https://openairdocs.org/sdr/ZW0A0103003), Jun 5, 2001: FLOOR PANEL. CORRODED. DURING CHECK-C MAINT FOUND LIGHT CORROSION ON METAL FLOOR PANEL APPROX STA 197 TO 200, RBL 52 TO 57. REMOVED AND FABRICATED NEW PANEL. - [SDR ZW0A0103002](https://openairdocs.org/sdr/ZW0A0103002), Jun 4, 2001: MOUNT. DAMAGED. DURING CHECK-C MAINT FOUND BULGE IN FUSELAGE SKIN AND RIVET HEAD POPPING ABOVE LONGERON 22, BETWEEN OUTFLOW VALVE AND AFT LAV DUMP. INSTALLED NEW OUTFLOW MOUNT - [SDR ZW0A0102513](https://openairdocs.org/sdr/ZW0A0102513), May 30, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 5, STA 200 TO 246, SEVERAL PLACES ON FLOOR SUPPORT. REPLACED CORRODED SECTION OF TRACK FROM STA 200-246 WIT - [SDR ZW0A0102512](https://openairdocs.org/sdr/ZW0A0102512), May 30, 2001: WEB. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN MEMBRANE ON RT SIDE AT STA 217, UNDER NUMBER 5 FLOOR PANEL, AND FOUND CORROSION AT STA 200. INSTALLED 7075-T6 0.025 MEMBRANE - [SDR ZW0A0102511](https://openairdocs.org/sdr/ZW0A0102511), May 30, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, RBL 53. REMOVED AND INSTALLED NEW FLOOR SUPPORT MADE FROM SAMPLE EXTRUDED AND INSTALLED - [SDR ZW0A0102510](https://openairdocs.org/sdr/ZW0A0102510), May 30, 2001: FRAME. CORRODED. DURING CHECK-C MAINT FOUND STA 1309 FORMER RING CORRODED BETWEEN LONGERON 27L AND 27R. REMOVED CORROSION PER SPM 6-80-01 AND SPLICED IN NEW SECTION PER SRM 53-0 - [SDR ZW0A0102509](https://openairdocs.org/sdr/ZW0A0102509), May 29, 2001: LONGERON. CORRODED. DURING CHECK-C MAINT FOUND LONGERON 22L CORRODED AT STA 1297. REMOVED CORRODED AREA AND INSTALLED FILLER AND SPLICES PER SRM 53-02, FIG 18. - [SDR ZW0A0102508](https://openairdocs.org/sdr/ZW0A0102508), May 29, 2001: INTERCOSTAL. CRACKED. DURING CHECK-C MAINT THE FWD LT CORNER OF KEEL BEAM INTERNAL STRUCTURE WAS CRACKED APPROX 3.5 IN AT STA 938 ABOVE AND FWD OF LT GEAR DOOR. REPLACED INTERCOSTAL - [SDR ZW0A0102507](https://openairdocs.org/sdr/ZW0A0102507), May 29, 2001: SUPPORT BRACKET. CRACKED. DURING CHECK-C MAINT THE SUPPORT BRACKET WAS CRACKED IN THREE AREAS AT FWD OTBD CORNER OF KEEL BEAM, INTERNAL STA 938 APPROX 3 INCHES ABOVE SKIN. REPLACED SUPPO - [SDR ZW0A0102506](https://openairdocs.org/sdr/ZW0A0102506), May 29, 2001: SUPPORT. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN LOWER AFT INBD CORNER OF RT WHEEL WELL IN SUPPORT AND REPAIR DOUBLER, APPROX STA 988. REPLACED SUPPORT AND FASTENERS PER SPM - [SDR ZW0A0102406](https://openairdocs.org/sdr/ZW0A0102406), May 25, 2001: SKIN. BULGED. DURING CHECK-C MAINT FOUND BULGE 12 INCHES TO 15 INCHES ABOVE CUSP AT STA 246, LT SIDE SKIN. REMOVED DAMAGED SKIN. REPAIRED PER SRM 53-04-12C. - [SDR ZW0A0102405](https://openairdocs.org/sdr/ZW0A0102405), May 25, 2001: FITTING. CRACKED. DURING CHECK-C MAINT FOUND T-FITTINGS CRACKED AT STA 1309, BETWEEN LONGERON 15 AND 16, AND ANOTHER BELOW LONGERON 14R AND FWD SIDE OF PYLON SUPPORT WALL. INSTAL - [SDR ZW0A0102404](https://openairdocs.org/sdr/ZW0A0102404), May 25, 2001: INTERCOSTAL. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORRODED INTERCOSTAL AT STA 1212 TO 1219, BETWEEN LONGERON 30 AND 29R. REMOVED CORRODED INTERCOSTAL. INSTALLED - [SDR ZW0A0102403](https://openairdocs.org/sdr/ZW0A0102403), May 25, 2001: FITTING. CORRODED. DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION AT FWD AND AFT SIDES OF FORMER FOOT, STA 1212 BETWEEN LONGERON 30 AND 29R. REMOVED FORMER FOOT. REMO - [SDR ZW0A0102326](https://openairdocs.org/sdr/ZW0A0102326), May 24, 2001: BRACKET. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER FWD CORNER OF AFT CARGO DOOR THRESHOLD. INSTALLED NEW BRACKET PER SRM 51-10-5 AND SRM 51-60-0, FIG 4 PAGE - [SDR ZW0A0102307](https://openairdocs.org/sdr/ZW0A0102307), May 24, 2001: FRAME. CRACKED. DURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1437, BETWEEN LONGERON 1 AND 2R. INSTALLED NEW CLIP (FORMER FOOT) PER SRM 51-30-2, SRM 51-30-5 AND SRM 5 - [SDR ZW0A0102325](https://openairdocs.org/sdr/ZW0A0102325), May 23, 2001: BRACKET. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN BRACKET, LOWER AFT CORNER OF THE AFT CARGO DOOR THRESHOLD. REPLACED LOWER AFT THRESHOLD BRACKET. USED SUBSTITUTE HI-LOKS - [SDR ZW0A0102324](https://openairdocs.org/sdr/ZW0A0102324), May 23, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND NUMBER 1 CHAIR TRACK CORRODED FROM STA 1079 TO 1309. REPLACED CORRODED SECTION OF TRACK FROM STA 1079 TO 1136 WITH NEW SECTION. INSTA - [SDR ZW010102323](https://openairdocs.org/sdr/ZW010102323), May 23, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON TOP SIDE OF FLOORBEAM AT STA 1338, BL 47R THRU BL 57R. REMOVED DAMAGED SECTION OF FLOORBEAM CAP. MANUFACTURED NEW SECTIO - [SDR ZW0A0102104](https://openairdocs.org/sdr/ZW0A0102104), May 19, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 3 CABIN CHAIR TRACK, STA 1261 TO 1308, 1155 TO 1193, 1221 TO 1261, AND 1193 TO 1221. INSTALLED SEAT TRACK REPAIR - [SDR ZW0A0102105](https://openairdocs.org/sdr/ZW0A0102105), May 18, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN, CHAIR TRACK NUMBER 3 HAD CORROSION AT STA 1130 TO 1155. CHANGED TRACK. DRILLED TRACK AND INSTALLED 2 SPLICES. INSTALLED S - [SDR ZW0A0102103](https://openairdocs.org/sdr/ZW0A0102103), May 18, 2001: WEB. CORRODED. DURING CHECK-C MAINT FOUND MEMBRANE/FLOOR PAN CORRODED, STA 1136 TO 1174, LBL 50-59. REMOVED AND REPLACED WEB SECTION PER SRM 51-70-4, FIG 2 SHEET 1 PAGE 5. - [SDR ZW0A0102102](https://openairdocs.org/sdr/ZW0A0102102), May 18, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT HAD CORROSION AT LBL 56 TO 59, STA 1140 AND 1168. INSTALLED NEW FLOOR SUPPORT AT BOTH LOCATION PER SRM 51-30-5. - [SDR ZW0A0101909](https://openairdocs.org/sdr/ZW0A0101909), May 18, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT LBL 8, STA 185 TO 200. REPLACED WITH NEW SUPPORT. - [SDR ZW0A0102006](https://openairdocs.org/sdr/ZW0A0102006), May 17, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT THE FLOOR SUPPORT HAD CORROSION AT STA 1165, LBL 52 TO 55, AND AT STA 1143, LBL 52 TO 55. AT BOTH LOCATIONS, NEW PART PRIMED AND PAINTED PE - [SDR ZW0A0101902](https://openairdocs.org/sdr/ZW0A0101902), May 14, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON TRACK NUMBER 4 AT STA 200 TO 266, IN TRACK AND FLOOR SUPPORT. REPLACED TRACK SECTION STA 200 TO 266 PER DRAWING C03580. - [SDR ZW0A0101901](https://openairdocs.org/sdr/ZW0A0101901), May 14, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT THE CHAIR TRACK AT LBL 34 HAD CORROSION AT STA 1130 TO 1138. REPLACED TRACK PER DRAWING C03580 AND INSTALLED PER SRM 51-30-1. - [SDR ZW0A0101816](https://openairdocs.org/sdr/ZW0A0101816), May 14, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN LONGERON 4L, INBOARD SIDE AT FASTENER, STA 160. REPLACED DAMAGED PORTION OF LONGERON WITH NEW. INSTALLED LONGERON SPLICE PER - [SDR TWAA0013304](https://openairdocs.org/sdr/TWAA0013304), Aug 26, 2000: SLAT. MALFUNCTIONED. UPON FLAP RETRACTION UNABLE TO BRING SLATS UP. NO ASYMMETRY NOTED. EXTENDED SLATS FULLY AND FLT RETURNED TO OKC. OPERATED SLATS NORMALLY ON THE GROUND. LUBED FL - [SDR TWAA0002208](https://openairdocs.org/sdr/TWAA0002208), Feb 6, 2000: MOTOR. FAILED. DURING DESCENT,STABILIZER JAMMED. REPLACED THE PRIMARY AND ALTERNATE TRIM MOTORS. PRIMARY MFG PART NUMBER 9590-5, ALT MFG PART NUMBER D1775-1. - [SDR TWAA9904803](https://openairdocs.org/sdr/TWAA9904803), Mar 25, 1999: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN AROUND THE DRAIN FITTING DAMAGED AT STA 273 BETWEEN LONGERON 29R AND 30. DAMAGE IS .1875 INCH DEEP AND 8 INCHES LO - [SDR TWAA9806704](https://openairdocs.org/sdr/TWAA9806704), Mar 13, 1998: SKIN. DAMAGED. STL - DURING C-CHECK, FOUND SKIN BELOW FWD CARGO DOOR SILL SCRATCHED AT STATION 370 TO 427, L29R TO 28R. MINOR SKIN DAMAGE. ROUNDED OUT AND TAPERED SCRATCHES AN - [SDR TWAA9802604](https://openairdocs.org/sdr/TWAA9802604), Feb 22, 1998: ENGINE. FAILED. PHL - FLT 561 - AT APPROX 3000 FEET, CREW HEARD LOUD POP. THE RT ENGINE EPR DROPPED OFF. CREW REPORTED ENGINE FAILED AND SHUT DOWN. FLT RETURNED TO PHL. REPLACE - [SDR TWAA9751003](https://openairdocs.org/sdr/TWAA9751003), Apr 18, 1997: CONNECTOR. LOOSE. MCI - FLT 669 - DURING LAYOVER, MAINTENANCE FORWARD AND AFT EMERGENCY EGRESS LIGHTS WERE INOP, DUE TO LOOSE CONNECTOR. SECURED CONNECTOR AND OPERATIONAL CHECK N - [SDR TWAA9746001](https://openairdocs.org/sdr/TWAA9746001), Apr 2, 1997: CONNECTOR. LOOSE. MCI - FLT 669 - DURING LAYOVER, MAINTENANCE FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING FOUND INOPERABLE. RECONNECTED LOOSE CONNECTION ON FLOOR STRIP. OPERATIONA - [SDR TWAA9745002](https://openairdocs.org/sdr/TWAA9745002), Apr 1, 1997: BATTERY PACK. DISCHARGED. STL - FLT 280 - DURING CRUISE, ESCAPE LIGHTING REMAINED ON IN THE ARM POSITON. REMOVED AND REPLACED BATTERY PACK, MFG PN 5822-2, MANUFACTURED BY LUMINESCENT SYS - [SDR TWAA9741003](https://openairdocs.org/sdr/TWAA9741003), Mar 20, 1997: SELECTOR. FAILED. STL - FLT 10 - AFTER TAKEOFF, COULD NOT PRESSURIZE CABIN IN EITHER PRIMARY OR STANDBY MODE. NR 1 SYSTEM. NR 2 SYSTEM PREVIOUSLY PLACARDED. FLIGHT RETURNED TO ST - [SDR TWAA9740001](https://openairdocs.org/sdr/TWAA9740001), Mar 19, 1997: CONTROLLER. FAILED. STL - FLT 23 - DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE IN EITHER STANDBY OR PRIMARY MODE. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLER, MFG PN 2117180-2. O - [SDR TWAA9808903](https://openairdocs.org/sdr/TWAA9808903), Mar 7, 1997: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK FOUND RT OTBD CHAIR TRACK CORRODED BEYOND REMOVAL LIMITS AT STA 200 TO STA 800. REMOVED AND REPLACED CHAIR TRACK FS 200 TO - [SDR TWAA9808814](https://openairdocs.org/sdr/TWAA9808814), Mar 7, 1997: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, THE MATERIAL REMOVED WAS BEYOND LIMITS ON CHAIR TRACK RBL 22, STATION 200 TO 212. REPLACED CHAIR TRACK PER SRM 51-01 PAGE - [SDR TWAA9808803](https://openairdocs.org/sdr/TWAA9808803), Mar 7, 1997: WEB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STATION 245, LBL 54, MEMBRANE CRACKED UNDER CHAIR TRACK. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 53-01, PAG - [SDR TWAA9737004](https://openairdocs.org/sdr/TWAA9737004), Mar 7, 1997: MEMBRANE. CRACKED. MCI - DURING OP-16, FOUND MEMBRANE CRACKED UNDER CHAIR TRACK, STATION 245, LBL 54. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M) - [SDR TWAA9737003](https://openairdocs.org/sdr/TWAA9737003), Mar 7, 1997: CHAIR TRACK. CORRODED. MCI - DURING OP 16, FOUND CORROSION ON RT OUTBOARD CHAIR TRACK, STATION 200-800. REMOVED AND REPLACED CHAIR TRACK PER SRM 53-05, FIGURE 4F AND TWA STANDARD PRAC - [SDR TWAA9809605](https://openairdocs.org/sdr/TWAA9809605), Mar 6, 1997: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 1212 TO FS 1331 IN RT FLOOR TRACK. REPLACED WITH NEW FLOOR TRACK PER SRM 51-01, PG 1, ITEM C. TOTAL - [SDR TWAA9808810](https://openairdocs.org/sdr/TWAA9808810), Mar 6, 1997: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON LEFT FLOOR TRACK AT FS 1212 TO 1331. INSTALLED NEW TRACK PER SRM 51-01, AND STD PRACTICES. (M) - [SDR TWAA9808808](https://openairdocs.org/sdr/TWAA9808808), Mar 6, 1997: SUPPORT. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 1267 BETWEEN STRINGER 28L AND 27L, FLOOR SUPPORT BRACE. REPLACED TRACK SUPPORT PER SRM 51-01, PAGE 1 - [SDR TWAA9808807](https://openairdocs.org/sdr/TWAA9808807), Mar 6, 1997: SUPPORT. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FWD CARGO DOOR THRESHOLD SUPPORT STRUCTURE AT FS 370 TO 427. REPLACED THRESHOLD FRAME PER SRM 53-05, PA All 68: https://openairdocs.org/deregistered/N907TW-2007-03-01/reports.md ## Other aircraft with N907TW - [Registered now](https://openairdocs.org/aircraft/N907TW): Orin C Carpenter II ALASKA EXP, S/N 0001, built 2023 --- 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.