# N154SY: 1981 Mcdonnell Douglas DC-10-15, registration cancelled 2004-10-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 26, 2004 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-10-15](https://openairdocs.org/model/mcdonnell-douglas-dc-10-15) (registry code 3022118) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 48259 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 22, 1997 - Certificate issued: July 16, 1997 - Last registry action: September 1, 2004 - Mode S code: A0DAB2 - Owner when cancelled: [Boeing Capital Corporation](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20CORPORATION) - Location: [Renton, WA](https://openairdocs.org/faa-place/WA/Renton) - Owner type: Corporation - Owner's area on the map: 47.4475° N, 122.2016° W: Placed by OpenAirDocs at the center of ZIP code 98055, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N154SY - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=154SY - Page: https://openairdocs.org/deregistered/N154SY-2004-10-26 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-10-15: https://openairdocs.org/model/mcdonnell-douglas-dc-10-15.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SCNA00096](https://openairdocs.org/sdr/SCNA00096), Aug 30, 2000: POWER SUPPLY. INOPERATIVE. AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT CABIN POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECKS GOOD. - [SDR SCNA00092](https://openairdocs.org/sdr/SCNA00092), Aug 29, 2000: POWER SUPPLY. INOPERATIVE. DURING A MAINTENANCE LINE CHECK, THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY. - [SDR SCNA00053](https://openairdocs.org/sdr/SCNA00053), Jun 7, 2000: SLIDE. FAILED. DURING A ROUTINE MAINTENANCE CHECK, THE R4 DOOR SLIDE WAS CHECKED FOR FOR PROPER INFLATION AND SERVICIABILITY. THE SLIDE DID NOT STAY INFLATED AND SHOWED SIGNS - [SDR SCNA00052](https://openairdocs.org/sdr/SCNA00052), Jun 5, 2000: LINE. RUPTURED. AFTER TAKEOFF FROM PVR, THE LANDING GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. THE CREW RETURNED TO POINT OF ORIGIN. A HYDRAULIC LINE WAS FOUND RUPTURED - [SDR SCNA00025](https://openairdocs.org/sdr/SCNA00025), Apr 3, 2000: LIGHT. INOPERATIVE. DURING A LINE MAINTENANCE CHECK, THE EMERGENCY PATH LIGHTING BETWEEN RIGHT HAND ROWS 15 TO 18 WAS FOUND TO BE INOPERATIVE. THE EMERGENCY PATH LIGHTING FROM RIGH - [SDR SCNA99116](https://openairdocs.org/sdr/SCNA99116), Sep 1, 1999: BULB. FAILED. DURING A LINE MAINTENANCE CHECK, AN EMERGENCY TRACK LIGHT BY SEAT ROW 6 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB IN THE EMERGENCY TRACK - [SDR SCNA99080](https://openairdocs.org/sdr/SCNA99080), Jun 1, 1999: LIGHT. INOPERATIVE. DURING A LINE MAINTENANCE CHECK THE FORWARD CABIN OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AND FOUND A - [SDR SCNA99509](https://openairdocs.org/sdr/SCNA99509), May 10, 1999: SWITCH. FAILED. DURING A HEAVY MAINTENANCE VISIT, DURING COMPLETION OF A CABIN LEAK CHECK THE ALTITUDE WARNING HORN FAILED TO GO OFF WHEN THE CABIN ALTITUDE REACHED 12,000 FT. - [SDR SCNA99508](https://openairdocs.org/sdr/SCNA99508), May 10, 1999: SENSOR. MISINSTALLED. DURING A HEAVY MX CHECK TEST FLT, THE LT MAIN GEAR UNSAFE RED LIGHT ILLUM WHILE ROTATING AND EXTINGUISHED IN FLIGHT. THE CREW TROUBLESHOT AND RETURNED TO POINT - [SDR SCNA99506](https://openairdocs.org/sdr/SCNA99506), May 10, 1999: ANGLE. CORRODED. DURING A HEAVY MAINTENANCE CHECK, THE 'L' ANGLE AT STATION 567 TO 595 AT LONGERON 44L WAS FOUND TO HAVE CORROSION AND MATERIAL LOSS WAS GREATER THAN 20 PERCENT - [SDR SCNA99505](https://openairdocs.org/sdr/SCNA99505), May 10, 1999: SPAR. CRACKED. DURING A HEAVY MAINTENANCE CHECK, THE LEFT HORIZONTAL STABILIZER OUTBOARD SECTION UPPER SPAR CAP FORWARD WAS FOUND CRACKED AT THE FORWARD CLOSING RIB PLANE THE - [SDR SCNA99504](https://openairdocs.org/sdr/SCNA99504), May 9, 1999: SKIN. CHAFED. DURING A HEAVY MAINTENANCE CHECK, THE RIGHT LEADING EDGE SKIN ARB1074 WAS FOUND TO BE CHAFED AT STA XOS 551 TO XOS 555 WITH .043 REMAINING OF ORIGINAL THICKNESS - [SDR SCNA99503](https://openairdocs.org/sdr/SCNA99503), May 9, 1999: SWITCH. FAILED. DURING A HEAVY MAINTENANCE CHECK, 2 ANEROID SWITCHES FOR THE PASSENGER OXYGEN SYSTEM FAILED TEST FOR SCA WORK CARD X1036. THE SUBJECT ANEROID SWITCHES 2 WERE RE - [SDR SCNA99507](https://openairdocs.org/sdr/SCNA99507), May 7, 1999: BATTERY PACK. DISCHARGED. DURING A HEAVY MAINTENANCE CHECK, THE EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE FROM SEAT 8L TO 15L AND 8R TO 15R. REMOVED AND REPLACED THE BATTERY PA - [SDR SCNA99502](https://openairdocs.org/sdr/SCNA99502), Apr 21, 1999: SUPPORT. CRACKED. DURING A HEAVY MAINTENANCE CHECK, AFT GALLEY FLOOR SUPPORT AT STA 1902 WAS FOUND TO BE CORRODED ON UPPER AND LOWER SURFACES RHX=8 AND BARE METAL X=1 TO X=23 CRA - [SDR SCNA99501](https://openairdocs.org/sdr/SCNA99501), Apr 18, 1999: SUPPORT. CORRODED. DURING A HEAVY MAINTENANCE CHECK, AFT GALLEY FLOOR SUPPORT AT STA 1910 WAS FOUND TO BE CORRODED BETWEEN X=27.5 AND X=MINUS 27.5 RT. REMOVED CORROSION FOUND TO B - [SDR SCNA99500](https://openairdocs.org/sdr/SCNA99500), Apr 18, 1999: SUPPORT. CRACKED. DURING A HEAVY MAINTENANCE CHECK, 2EA FLOOR SUPPORTS STA Y=1986 CL=0 AND X+27.5 ARE CRACKED AT INBD ENDS AND ALSO WERE FOUND CORRODED. REMOVED FABRICATED ALODIN - [SDR SCNA99047](https://openairdocs.org/sdr/SCNA99047), Mar 11, 1999: SENSOR. FAILED. DURING A LINE MAINTENANCE CHECK, THE RIGHT STALL WARNING FAILED THE SELF TEST. REMOVED AND REPLACED THE ANGLE OF ATTACK SENSOR IAW MM 223301. SYSTEM OPERATIONAL - [SDR SCNA99016](https://openairdocs.org/sdr/SCNA99016), Jan 17, 1999: COALESCER. CONTAMINATED. DURING CLIMB, CABIN FILLED WITH SMOKE. COMPLIED WITH COM AND SMOKE STOPPED WHEN NR 2 PNEUMATIC SUPPLY AND NR 2 PACK SELECTED TO OFF. DIVERTED AIRCRAFT TO ORD FO - [SDR SCNA98147](https://openairdocs.org/sdr/SCNA98147), Dec 4, 1998: SMOKE DETECTOR. NO TEST. DURING A LINE MAINTENANCE CHECK, THE NUMBER 4 CARGO SMOKE DETECTOR DID NOT TEST. REMOVED AND REPLACED THE SMOKE DETECTOR, OPERATIONALLY CHECKED GOOD. - [SDR SCNA98091](https://openairdocs.org/sdr/SCNA98091), Aug 14, 1998: POWER SUPPLY. INOPERATIVE. DURING A LINE MAINTENANCE CHECK, THE MID CABIN EMERGENCY LIGHTING POWER SUPPLY FAILED SELF TEST. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHTING (OVERHEAD) PO - [SDR SCNA98079](https://openairdocs.org/sdr/SCNA98079), Jul 23, 1998: BATTERY. DISCHARGED. DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT TEST FROM THE COCKPIT FAILS TEST. REMOVED AND REPLACED BOTH BATTERY CHARGER UNIT AND BATTERY IN AFT POSITIO ## Other aircraft with N154SY - [Registered now](https://openairdocs.org/aircraft/N154SY): Embraer S A ERJ 170-200 LR, S/N 17000556, built 2016 --- 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.