# N941AS: 1989 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2012-11-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 19, 2012 - 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: 49925 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 11, 1989 - Last registry action: August 9, 2012 - Mode S code: AD10F0 - Location: [Beverly Hills, CA](https://openairdocs.org/faa-place/CA/Beverly%20Hills) - Owner type: Individual - Owner's area on the map: 34.1005° N, 118.4146° W: Placed by OpenAirDocs at the center of ZIP code 90210, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N941AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=941AS - Page: https://openairdocs.org/deregistered/N941AS-2012-11-19 From the FAA registry file of October 28, 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 (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20050313](https://openairdocs.org/sdr/AALA20050313), May 8, 2005: BATTERY PACK. DISCHARGED. LGA - SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20 INOPERATIVE. REPLACED CHARGER AND BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20. SYSTEM GROUND - [SDR AALA20050027](https://openairdocs.org/sdr/AALA20050027), Jan 14, 2005: BATTERY PACK. INOPERATIVE. DFW - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20041044](https://openairdocs.org/sdr/AALA20041044), Oct 13, 2004: CONNECTOR. CROSSED. DFW - EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS INOPERATIVE. FOUND CONNECTORS CROSS CONNECTED. RECONNECTED CONNECTORS FOR EMERGENCY ESCAPE PATH LIGHTS - [SDR ZW0A0304703](https://openairdocs.org/sdr/ZW0A0304703), May 7, 2003: BATTERY. INOPERATIVE. THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN SEAT ROWS 7 TO 11 AND JUST AFT OF ROW 31, AND THE FIRST CLASS EGRESS LIGHTS WERE DIM. REPLACED THE BATTERI - [SDR ZW0A0203101](https://openairdocs.org/sdr/ZW0A0203101), Mar 13, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FLANGES FROM STATION 160 TO 200, RBL 43. INSTALLED NEW FABRICATED SUPPORT AT STA 160 TO 200, PER SPM 6-70- - [SDR ZW0A0202701](https://openairdocs.org/sdr/ZW0A0202701), Mar 5, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINTENANCE FOUND CORROSION IN LATERAL FLOOR SUPPORT, STATION 181, FROM RBL 9 TO RBL 42. INSTALLED LATERAL SUPPORT AFTER FABRICATION AT STA 181, - [SDR ZW0A0202603](https://openairdocs.org/sdr/ZW0A0202603), Mar 1, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 195, LBL 14. REMOVED CORROSION ON MEMBRANE PER SRM 53-01, PAGE 6, AND SPM 6-80-01, PAGES 1, 2, AND 3. R - [SDR ZW0A0202503](https://openairdocs.org/sdr/ZW0A0202503), Feb 28, 2002: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN LONGITUDINAL FLOOR SUPPORT FROM STA 160 TO 196, LBL 45. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-02. - [SDR ZW0A0202502](https://openairdocs.org/sdr/ZW0A0202502), Feb 27, 2002: SEAT TRACK. CORRODED. DURING CHECK-C MAINT CABIN SEAT TRACK HAD CORROSION IN LT FLANGE OF TRACK, LBL 44.5 INCHES, BETWEEN STA 1117 AND 1174. INSTALLED NEW SECTION OF TRACK FROM STA 1 - [SDR ZW0A0202404](https://openairdocs.org/sdr/ZW0A0202404), Feb 25, 2002: SUPPORT BRACKET. CRACKED. DURING CHECK-C MAINT FOUND A SUPPORT BRACKET CRACKED, 8 INCHES BELOW THE FLOOR TRACK AT STA 845, LBL 22 INCHES. REPLACED SUPPORT PER SPM 6-70-01. - [SDR ZW0A0103101](https://openairdocs.org/sdr/ZW0A0103101), Jun 5, 2001: COUPLING. DEFECTIVE. WHILE CREW WAS TROUBLESHOOTING A CABIN TEMPERATURE PROBLEM THE CABIN BEGAN TO CLIMB UNCONTROLLABLY. THE CREW INITIATED AN EMERGENCY DESCENT, MANUALLY DROPPED TH - [SDR TWAA0015404](https://openairdocs.org/sdr/TWAA0015404), Oct 3, 2000: LIGHT. INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE TAIL COMPARTMENT WAS HANGING DOWN AT AN ANGLE, AND THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. RE-INSTALLED LIGHT A - [SDR TWAA0014901](https://openairdocs.org/sdr/TWAA0014901), Sep 26, 2000: BATTERY PACK. DISCHARGED. THE AFT SECTION OF EGRESS LIGHTS AND THE AFT AIRSTAIR EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-22-00 STL. - [SDR TWAA0011102](https://openairdocs.org/sdr/TWAA0011102), Jul 13, 2000: BLADE. FAILED. THE RT ENGINE FAILED WITH A BANG. CREW ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE AND MADE AN UNSCHEDULED LANDING AT IAD. FOUND TURBINE FAILURE. CHECK-C 2-22-00 ST - [SDR TWAA0010001](https://openairdocs.org/sdr/TWAA0010001), Jun 23, 2000: CSD. FAILED. IN CLIMB, THE RT CSD WENT ABOVE RED LINE AFTER 20 MINUTES OF FLIGHT. CREW DISCONNECTED THE CSD. THE APU WAS STARTED BUT IN CRUISE AT FL350 THE APU SHUT ITSELF D - [SDR TWAA9902601](https://openairdocs.org/sdr/TWAA9902601), Feb 2, 1999: SUPPORT. BROKEN. DURING OP 16 MAINT CHECK, FOUND AFT CABIN FLOOR SUPPORT BROKEN AT STA 1300, BL 0 IN, AFT CABIN FLOOR BOARD NUMBER 94. INSTALLED REPAIR ANGLE PER ARA 15736. - [SDR TWAA9902602](https://openairdocs.org/sdr/TWAA9902602), Jan 31, 1999: FRAME. CORRODED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME LOWER SECTION AT STA 1322, BL 0, WITH CORROSION ABOVE STRINGER. REMOVED CORROSION PER TWA SPM 6-80-01. REPAIRED P - [SDR TWAA9902605](https://openairdocs.org/sdr/TWAA9902605), Jan 28, 1999: SEAT TRACK. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR TRACK RBL 16, BETWEEN STA 1212 AND 1271. INSTALLED NEW FLOOR TRACK PER STANDARD PROCESS - [SDR TWAA9902604](https://openairdocs.org/sdr/TWAA9902604), Jan 28, 1999: INTERCOSTAL. CORRODED. DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL BELOW RT FLOOR TRACK AT STA 1308, RBL 16, WAS CORRODED. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANUAL 6-70 - [SDR TWAA9902603](https://openairdocs.org/sdr/TWAA9902603), Jan 28, 1999: INTERCOSTAL. CORRODED. DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CORRODED BELOW LT FLOOR SUPPORT, BETWEEN STA 1308 AND 1319, LBL 16. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES - [SDR TWAA9901906](https://openairdocs.org/sdr/TWAA9901906), Jan 27, 1999: CASTING. CRACKED. DURING OP 16 MAINT CHECK, THE FWD AIRSTAIRS FORWARD DOOR CASTING WAS CRACKED IN RADIUS APPROXIMATELY 1.5 INCH LONG. REMOVED AND REPLACED CASTING PER STANDARD PR - [SDR TWAA9901905](https://openairdocs.org/sdr/TWAA9901905), Jan 27, 1999: SKIN. DELAMINATED. DURING OP 16 MAINT CHECK, FOUND RUDDER DELAMINATED ON RT SIDE AT AFT SIDE OF CENTER HINGE. REPAIRED PER SRM 51-90-0, PAGE 49, AND 51-70-1A PAGE 21. - [SDR TWAA9901707](https://openairdocs.org/sdr/TWAA9901707), Jan 23, 1999: FITTING. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR FITTING CORRODED AT STA 1193 AT CUSP LINE, RT SIDE OF AFT CARGO BIN. REMOVED LIGHT SURFACE CORROSION USING RUBBER BACK SAN - [SDR TWAA9901708](https://openairdocs.org/sdr/TWAA9901708), Jan 22, 1999: SEAT TRACK. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1099, 44 IN LBL. REMOVED CORROSION PER TWA SPM 6-80-01. INSTALLED NEW TRACK PER SRM 53-05, FIG 4 - [SDR TWAA9901706](https://openairdocs.org/sdr/TWAA9901706), Jan 21, 1999: FRAME. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 1219 APPROXIMATELY RBL 4 IN UNDERNEATH UPPER PART OF FORMER RING. REMOVED CORROSION PER SRM 6-80-01, PG 1 TO 3. - [SDR TWAA9901705](https://openairdocs.org/sdr/TWAA9901705), Jan 21, 1999: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOORBEAM CAP CORRODED AT STA 1156 BETWEEN TRACK LBL 22 AND LBL 42. FABRICATED NEW PART FROM 7075 T6. INSTALLED PER TWA STD PROC - [SDR TWAA9901704](https://openairdocs.org/sdr/TWAA9901704), Jan 21, 1999: WEB. CORRODED. DURING OP 16 MAINT CHECK, FOUND IN CABIN, WEB CRACKED AND CORRODED AT STA 1156 UNDER FLOOR. REMOVED CORROSION PER SRM 51-10-3, PARA 31 TO 42. REPAIRED WEB PER 5 - [SDR TWAA9901703](https://openairdocs.org/sdr/TWAA9901703), Jan 19, 1999: MEMBRANE. CRACKED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE REPAIR DOUBLER CRACKED IN 2 PLACES AT STA 1271 TO 1307. REMOVED OLD DOUBLER AND INSTALLED NEW ONE PER SRM 53-05, - [SDR TWAA9901702](https://openairdocs.org/sdr/TWAA9901702), Jan 19, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE AT STA 927 TO 946, 58.8 LBL. REMOVED 9 INCH BY 13 IN FLOOR MEMBRANE AND INSTALLED NEW 2024-T3 0.040 - [SDR TWAA9901605](https://openairdocs.org/sdr/TWAA9901605), Jan 19, 1999: ANGLE. CORRODED. DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT FLOOR SUPPORT ANGLE ON TOP OF FORMER STA 1212 RBL CORRODED. REMOVED AND REINSTALLED ANGLE PER TWA STD PROCESSES - [SDR TWAA9901604](https://openairdocs.org/sdr/TWAA9901604), Jan 19, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, THE CABIN FLOOR MEMBRANE WAS CORRODED AT STA 743 RT SIDE. REMOVED CORROSION PER STANDARD PROCEDURES MANUAL 6-80-01. FABRICATED AND INS - [SDR TWAA9901606](https://openairdocs.org/sdr/TWAA9901606), Jan 18, 1999: SEAT TRACK. CORRODED. DURNG OP 16 MAINT CHECK, FOUND IN CABIN, CORROSION IN CHAIR TRACK AT RBL 44 IN, STA 237, 262 TO 264, AND STA 275. REPLACED TRACK RBL 44 FROM STA 237 TO 275 PER - [SDR TWAA9901602](https://openairdocs.org/sdr/TWAA9901602), Jan 18, 1999: ANGLE. CRACKED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO VERTICAL STABILIZER TIE ANGLE CRACKED APPROX 1.5 INCH LONG AT STA 1426 BETWEEN LONGERON 1L AND 2L, INSIDE LOWER STAB - [SDR TWAA9901309](https://openairdocs.org/sdr/TWAA9901309), Jan 17, 1999: STRUCTURE. CORRODED. DURING OP 16 MAINT CHECK, FOUND IN FWD LT CABIN DOOR WHERE SEAL CONTROL SHAFT PASSES THRU INTERNAL STRUCTURE TO CONNECT WITH SEAL ACTUATING LINK, STRUCTURE HAS - [SDR TWAA9901307](https://openairdocs.org/sdr/TWAA9901307), Jan 17, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 522 TO 541, RT SIDE. REMOVED CORROSION PER STD PROCESSES MANUAL 6-80-1, PARA B PG 1. REPAIRED PER - [SDR TWAA9901306](https://openairdocs.org/sdr/TWAA9901306), Jan 17, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND SIDEWALL FLOOR MEMBRANE WITH CORROSION BETWEEN LONGERON 655 AND 658. CUT OUT CORRODED AREA, INSTALLED 3 INCH BY 16 INCH 2024T3 0 - [SDR TWAA9901305](https://openairdocs.org/sdr/TWAA9901305), Jan 16, 1999: MEMBRANE. DAMAGED. DURING OP 16 MAINT CHECK, FOUND HOLE IN MEMBRANE AT STA 199, APPROXIMATELY LBL 16 INCHES. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, PAGE 18 FIG 4. - [SDR TWAA9901209](https://openairdocs.org/sdr/TWAA9901209), Jan 15, 1999: INTERCOSTAL. CORRODED. DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL FOOT CORRODED BETWEEN STA 1212 AND 1219, RBL 4 IN. INSTALLED NEW FOOT PER SRM 6-70-0 PG 3 AND USED FASTENERS PER SPM - [SDR TWAA9901208](https://openairdocs.org/sdr/TWAA9901208), Jan 15, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED STA 465 TO 475 ON LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, - [SDR TWAA9901207](https://openairdocs.org/sdr/TWAA9901207), Jan 15, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 400 TO 408, LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, - [SDR TWAA9901206](https://openairdocs.org/sdr/TWAA9901206), Jan 15, 1999: MEMBRANE. CRACKED. DURING OP 16 MAINT CHECK, FOUND I/B EDGE OF MEMBRANE CRACKED BENEATH CHAIR TRACK AT STA 1063, LBL 42 IN. REPAIRED MEMBRANE PER SRM 53-01, PG 9. - [SDR TWAA9901205](https://openairdocs.org/sdr/TWAA9901205), Jan 15, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE WITH CORROSION BETWEEN STA 598 AND 617 AT CABIN SIDEWALL AREA. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER PER SR - [SDR TWAA9901204](https://openairdocs.org/sdr/TWAA9901204), Jan 14, 1999: MEMBRANE. CORRODED. DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORROSION AT STA 484 TO 502 ON RT SIDE. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 53-01, PG 9. - [SDR TWAA9901203](https://openairdocs.org/sdr/TWAA9901203), Jan 14, 1999: SEAT TRACK. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1206, LBL 22 IN. REPLACED CORRODED SECTION OF CHAIR TRACK PER SRM 53-05, PG 10G. - [SDR TWAA9901202](https://openairdocs.org/sdr/TWAA9901202), Jan 13, 1999: SEAT TRACK. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT RBL 22 IN STA 237. REMOVED APPROX 60 INCHES OF SEAT TRACK STARTING AT STA 200. INSTALLED NEW TRACK A - [SDR TWAA9901201](https://openairdocs.org/sdr/TWAA9901201), Jan 12, 1999: RIB. CRACKED. DURING OP 16 MAINT CHECK, FOUND ON RT WING 2 CRACKS ON RIB LOCATED ONE FT O/B OF NR 8 TRACK. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 57-01, FIG 3 SHEE - [SDR TWAA9900604](https://openairdocs.org/sdr/TWAA9900604), Jan 7, 1999: HANGER. CRACKED. DURING OP 16 MAINT CHECK, FOUND LOWER FAIRING T HANGER AT STA 865, 0 IN BL, WAS CRACKED. INSTALLED NEW T HANGER BRACKET (P/N 3936409-505), PER TWA STANDARD PROC - [SDR TWAA9900605](https://openairdocs.org/sdr/TWAA9900605), Jan 4, 1999: HANGER. CRACKED. DURING OP 16 MAINT CHECK, THE LOWER FAIRING T HANGER WAS FOUND CRACKED AT 0 IN BL AND STA 875. INSTALLED NEW BRACKET (P/N 3936409-501) PER TWA STANDARD PROCESSE - [SDR ASAA9880169](https://openairdocs.org/sdr/ASAA9880169), Sep 3, 1998: BOTTLE. DISCHARGED. LAX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE - [SDR ASAA9880165](https://openairdocs.org/sdr/ASAA9880165), Aug 29, 1998: LIGHT. INOPERATIVE. SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON ARM INDICATOR LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMLBY AND OPERATED NO All 72: https://openairdocs.org/deregistered/N941AS-2012-11-19/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA97IA040](https://openairdocs.org/ntsb/SEA97IA040), Dec 21, 1996: McDonnell Douglas MD-80 (N941AS), Seattle, WA, incident, minor damage. Probable cause: The failure of the left wing walker to verify the clearance between the left wing and the fuel truck during taxi, and his delay in signaling the lead marshaller to alert the pilot to stop the… ## 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 19961220045899I](https://openairdocs.org/incident/19961220045899I), Dec 20, 1996: Doug DC982 (N941AS), Seattle, WA, Minor damage. (-5) On December 20, 1996, about 2045 pacific standard time, N941AS, a Mcdonnell Douglas MD-80 airplane, operating as Alaska airlines flight 255, collided with… ## Other aircraft with N941AS - [Registered now](https://openairdocs.org/aircraft/N941AS): Cirrus Design SR20, S/N 11649 --- 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.