# N517AT: 1996 Boeing 757-23N, registration cancelled 2010-01-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 27, 2010 - Exported to: United Kingdom - Status when cancelled: Valid registration - Airframe: [Boeing 757-23N](https://openairdocs.org/model/boeing-757-23n) (registry code 1384973) - Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555) - Serial number: 27973 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 25, 1996 - Certificate issued: January 14, 2010 - Last registry action: January 14, 2010 - Mode S code: A67B82 - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N517AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=517AT - Page: https://openairdocs.org/deregistered/N517AT-2010-01-27 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 Boeing 757-23N: https://openairdocs.org/model/boeing-757-23n.md ## Service difficulty reports (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AMTA200700665](https://openairdocs.org/sdr/AMTA200700665), Nov 30, 2007: CONTROL VALVE. INOPERATIVE. RT PACK INOPERATIVE LITE ILLUMINATED. RT PACK BITE MSS ON EICAS. REMOVED AND REPLACED PACK TEMP CONTROL VALVE IAW MM 21-51-12-4. OPS CHECK GOOD, OK FOR SERVICE. - [SDR AMTA200700652](https://openairdocs.org/sdr/AMTA200700652), Nov 27, 2007: CONTROLLER. MALFUNCTIONED. EICAS MSG R PACK OFF AND PACK TEMP DISPLAYED. R INOP AND PACK OFF LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED WHEN PACK RESET SWITCH IN STANDBY. OPS NORMAL IN STUDY - [SDR AMTA200700574](https://openairdocs.org/sdr/AMTA200700574), Oct 31, 2007: COMPUTER. UNSERVICEABLE. DURING ENGINE START LT FMC FAIL ILLUMINATED. (K) PERFORMED BITE OF FMC IAW FIM 34-61-00. NO FAULTS NOTED. REPLACED L. FMC AS PRECAUTIONARY MEASURE. OPS CK GOOD - [SDR AMTA200700477](https://openairdocs.org/sdr/AMTA200700477), Oct 3, 2007: TIRE. DAMAGED. UPON AC ARRIVAL FOUND NR 4 MAIN TIRE MISSING 80 PERCENT OF THE CAP. REMOVED AND REPLACED NR 4 MLG TIRE AND WHEEL IAW MM 32-45-01-4. (K) - [SDR AMTA200700443](https://openairdocs.org/sdr/AMTA200700443), Sep 19, 2007: COMPUTER. UNSERVICEABLE. EICAS MSG L FMC FAIL DISPLAYED. (L) FMC BAD, REMOVED AND REPLACED LT FLIGHT MANAGEMENT COMPUTER IAW MM 34-61-01-4, OPS CHECK`S NORMAL. (K) - [SDR AMTA20070368](https://openairdocs.org/sdr/AMTA20070368), Jul 27, 2007: CIRCUIT BREAKER. TRIPPED. APU AUTO SHUTDOWN WHEN APU ELECTRIC SELECTED. GROUND POWER SOURCE CONNECTED TO AC APU BATTERY BUSS CB POPPED. RESET CB AND REMOVED GROUND POWER SOURCE CB STAYS - [SDR AMTA200700287](https://openairdocs.org/sdr/AMTA200700287), Jun 12, 2007: CONNECTOR. DISCONNECTED. L2 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. PLUGGED EMERGENCY LIGHT RECEPTICAL INTO SIDE WALL SOCKET OPS CHECK GOOD. - [SDR AMTA200700202](https://openairdocs.org/sdr/AMTA200700202), Apr 24, 2007: CONTROL VALVE. UNSERVICEABLE. EICAS MSG L PACK OFF WITH SWITCH IN AUTO POSITION. PACK OFF LIGHT REMAINS ON WITH SWITCH MOVED TO STBY N, C OR W. REMOVED AND REPLACED FLOW CONTROL AND SHUTOFF - [SDR AMTA200700148](https://openairdocs.org/sdr/AMTA200700148), Mar 16, 2007: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGN LIGHT AT ROW 16 CEILING INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-07-2. OPS CHECK GOOD. (K) - [SDR AMTA200700050](https://openairdocs.org/sdr/AMTA200700050), Feb 1, 2007: SENSOR. MALFUNCTIONED. EICAS MSG R PACK OFF AND PACK TEMP DISPLAYED RESET PACK IN STANDBY, OPS NORMAL. REMOVED AND REPLACED COMPRESSOR DISCHARGE TEMP SENSOR PER MM 21-51-06, OPS CHECK - [SDR AMTA200700049](https://openairdocs.org/sdr/AMTA200700049), Feb 1, 2007: VALVE. UNSERVICEABLE. EICAS MSG R ENG BLEED OFF DISPLAYED R ENG BLEED OFF LIGHT ILLUMINATED, CUICT PRESS NO RM 2119Z. REMOVED AND REPLACED FLOW CONTROL AND SHUTOFF VALVE PER AMM 21-5 - [SDR AMTA200600735](https://openairdocs.org/sdr/AMTA200600735), Dec 20, 2006: SHUTOFF VALVE. UNSERVICEABLE. IN CRUISE, AT 390 FL, BLEED AIR DUCT LT INDICATORS SPLIT L=44, R=58, EPR NR 1=159, NR 2=158, N1 NR1 87.1, NR 2 87.9. REMOVED AND REPLACED PRSOV NR 2 ENG SYS CHE - [SDR AMTA200600593](https://openairdocs.org/sdr/AMTA200600593), Oct 2, 2006: COMPUTER. WARNING MESSAGE. FMC MESSAGE ON EICAS, FMC L OUT PUT LOSS BOTH CDU`S OPERATE NORMAL. (M) - [SDR AMTA200600590](https://openairdocs.org/sdr/AMTA200600590), Sep 26, 2006: COMPUTER. MALFUNCTIONED. VTK FLAG IS IN VIEW ON F/O SIDE SELECTING ALTN FMC CORRECTS THE FAULT. REMOVED AND REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01-4. OPS CHECK GOOD. - [SDR AMTA200600485](https://openairdocs.org/sdr/AMTA200600485), Aug 3, 2006: MODULE. MALFUNCTIONED. LOWER EICAS CRT SCRAMBLES, SWITCHING TO OTHER EICAS COMPUTER NO HELP. REMOVED AND REPLACED LOWER EICAS CRT SWITCHING MODULE, OPS CHECKS NORMAL IAW. (K) - [SDR AMTA200600392](https://openairdocs.org/sdr/AMTA200600392), Jun 11, 2006: WARNING MESSAGE. ILLUMINATED. WXR SYS STATUS MSG. PERFORMED BITE CHECK IAW MM 34-43-00. OPS CHECKED OK. (K) - [SDR AMTA200600282](https://openairdocs.org/sdr/AMTA200600282), Apr 18, 2006: WARNING SYSTEM. FALSE INDICATION. EICAS STATUS MSG. (APU BAT NO STBY) STARTED/ RAN OK. PERFORMED T/S IAW FIM. THE SYS IS OK. (K) - [SDR AMTA200600176](https://openairdocs.org/sdr/AMTA200600176), Mar 17, 2006: TRANSMITTER. INOPERATIVE. LT HF TRANSMISSION INOPERATIVE AT ALL STA. DEFERRED. (K) - [SDR AMTA200501219](https://openairdocs.org/sdr/AMTA200501219), Dec 23, 2005: FLOOR SUPPORT. CORRODED. AFT PIT FLOOR SUPPORT HAS SURFACE CORRODED STA 1445 TO STA 1490 LBL 2.5. REMOVED AND REPLACED FLOOR SUPPORT SECTION FROM STA 1445 TO STA 1490 IAW SRM. (K) - [SDR AMTA200501207](https://openairdocs.org/sdr/AMTA200501207), Dec 22, 2005: FLOOR SUPPORT. TOOL DAMAGE. AFT PIT 3 EA DRILL MARKS, ONE WHICH IS CRACKED THRU FLOOR SUPPORT, STA 1317 TO 1320, RBL 11. REMOVED DAMAGED AFT PIT FLOOR SUPPORT FROM SAT 1342-1309 RBL 11, IA - [SDR AMTA200501175](https://openairdocs.org/sdr/AMTA200501175), Dec 18, 2005: FLOOR SUPPORT. CRACKED. IN THE AFT GALLEY AT STA 1661 TO 1681, BL 10 INCH, RT AT FLOOR SUPPORT IS CRACKED ON ITS UPPER FLANGE AT 3 FASTENER HOLE. REMOVED FLOOR SUPPORT FAB NEW SUPPORT - [SDR AMTA200501187](https://openairdocs.org/sdr/AMTA200501187), Dec 18, 2005: SILL. CORRODED. FWD CARGO COMPT CUTOUT SILL AREA NET TIEDOWN FITTING SUPPORT CORRODED AT AFT POSITION. REMOVED AND REPLACED FITTING. (K) - [SDR AMTA200501186](https://openairdocs.org/sdr/AMTA200501186), Dec 18, 2005: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOOR STRUCTURE STA 365, RBL 0 TO RBL 50. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORG MTL .125 LOW READING, .079 REPAIRED SECTION OF FLO - [SDR AMTA200501179](https://openairdocs.org/sdr/AMTA200501179), Dec 18, 2005: FLOORBEAM. CORRODED. IN THE AFT GALLEY 1640 BL0 TO 60, THERE IS CORROSION AROUND FASTENER HOLES ON THE TOP AND BOTTOM OF THE UPPER TEE CAP OF THE FLOORBEAM. REMOVED CORROSION FROM F - [SDR AMTA200501177](https://openairdocs.org/sdr/AMTA200501177), Dec 18, 2005: FLOOR SUPPORT. CORRODED. IN THE AFT GALLEY AREA STA 1664 TO STA 1681.8 BL0 THERE IS CORROSION ON UPPER SURFACE FLOOR SUPPORT BEAM. REMOVED CORROSION FROM FLOOR SUPPORT BEAM AT STA 1664- - [SDR AMTA200501176](https://openairdocs.org/sdr/AMTA200501176), Dec 18, 2005: BEAM. CORRODED. REMOVED CORROSION FROM BEAM IAW CPM 20-40-00, FOUND TO BE OUT OF LIMITS IAW 757, SRM 53-60-13. REMOVED AND REPLACED BEAM IAW SRM 51-40-02 OVER 50 PERCENT MATERI - [SDR AMTA200501178](https://openairdocs.org/sdr/AMTA200501178), Dec 18, 2005: FLOORBEAM. CORRODED. IN THE AFT GALLEY AT STA 1681 B/O THERE IS CORROSION ON THE UPPER SURFACE ON A FLOORBEAM CLIP. REMOVED CORROSION FROM FLOORBEAM THE CLIP AT 1681 BL0 IS LESS THA - [SDR AMTA200501169](https://openairdocs.org/sdr/AMTA200501169), Dec 17, 2005: SILL. CORRODED. FWD C COMPT DOOR CUTOUT SILL AREA NET TIEDOWN FITTING SUPPORT CORRODED AT AFT POSITION. REMOVED CORRODED FITTING INSTALLED NEW FITTING PN 69-45555-9 IAW SRM 51- - [SDR AMTA200501173](https://openairdocs.org/sdr/AMTA200501173), Dec 17, 2005: INTERCOSTAL. CORRODED. CORROSION ON UPPER SURFACE OF INTERCOSTAL AROUND FASTENER HOLES AT THE R-4 DOOR SILL STA 1681 TO 1661. REMOVED CORROSION FROM INTERCOSTAL AT R-4 DOOR SILL IAW S - [SDR AMTA200501167](https://openairdocs.org/sdr/AMTA200501167), Dec 16, 2005: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOOR STRUCTURE STA 377.35, RBL 5 TO LBL20. REMOVED CORROSION 377 LBL 20 WITHIN LIMITS 2 AREAS OUT OF LIMITS LBL 10, LBL18 CUTOUT DAMAGE FAB - [SDR AMTA200501103](https://openairdocs.org/sdr/AMTA200501103), Nov 25, 2005: FUSE. BLOWN. R4 SLIDE LIGHT INOPERATIVE. TROUBLESHOT, FOUND NO VOLTAGE TO LIGHT ASSY REPLACED FUSE ON BATTERY CHARGER. OPS CHECK GOOD. (K) - [SDR AMTA200501067](https://openairdocs.org/sdr/AMTA200501067), Nov 15, 2005: UNKNOWN. UNKNOWN. AT FL390, LT ENGINE COMMAND THRUST LEVEL SHOWED .07 EPR ABOVE ACTUAL EOR AT ALL TIMES ABOVE 35,000 FT. LT THRUST LEVER REQUIRED 1/2 KNOW FORWARD TO ALIGN EPR AL - [SDR AMTA200501057](https://openairdocs.org/sdr/AMTA200501057), Nov 12, 2005: GLOWSTRIP. MISSING. SMALL SECTION OF PHOTOLUMINESCENT ESCAPE PATH LIGHT STRIP MISSING AT APPROX ROW 12. INSTALLED PHOTOLUMINESCENT LIGHT STRIP IAW AMM. (K) - [SDR AMTA200500851](https://openairdocs.org/sdr/AMTA200500851), Oct 11, 2005: BATTERY PACK. UNSERVICEABLE. EMERGENCY EXIT LIGHTS INOPERATIVE AT L2 DOOR AND AFT. REPLACED L2 EMERGENCY BATTERY PACK. ALL EMERGENCY LIGHTS. OPS CHECK GOOD. (K) - [SDR AMTA200500374](https://openairdocs.org/sdr/AMTA200500374), Apr 17, 2005: MODULE. MALFUNCTIONED. LOWR EICAS DISPLAY FLICKERS FOR SEVERAL SECONDS INTERMITTENTLY WITH EIAS DISPLAY MESSAGE DISPLAYED LOWER EICAS INFORMAION ALSO COMPACTED ON UPPER SCREEN DURING - [SDR AMTA200401384](https://openairdocs.org/sdr/AMTA200401384), Nov 7, 2004: WARNING LIGHT. ILLUMINATED. LT BLEED (ENGINE) LIGHT CAME ON AT 80 KIAS ALSO ON EICAS ABORTED AC TAKEOFF. DEFERRED. - [SDR AMTA200401312](https://openairdocs.org/sdr/AMTA200401312), Oct 25, 2004: WIRE. LOOSE. EGRESS TRACK HAS LIGHTS INOPERATIVE BETWEEN SEATS 28 DEF AND 30 DEF. CONNECTED LOOSE WIRE. OPS CHECK NORMAL. OK FOR SERVICE. - [SDR AMTA200401322](https://openairdocs.org/sdr/AMTA200401322), Oct 25, 2004: SWITCH. OUT OF LIMITS. (R TURB OH DET 2) STATUS MSG CAME ON MOMENTARLY, JUST PRIOR TO LANDING. PERFORMED FIM 26-13-00, FIG 103 AND 104, NO DEFECTS NOTED. IAW FIM 26-13-00, FIG 103, BL - [SDR AMTA200400922](https://openairdocs.org/sdr/AMTA200400922), Jul 26, 2004: SOCKET. INOPERATIVE. FOUND 9 DEF EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT SOCKET ASSEMBLY IAW MM 33-51-11-403-059. (M) - [SDR AMTA200400803](https://openairdocs.org/sdr/AMTA200400803), Jun 25, 2004: STRUCTURE. CRACKED. LIGHTING HOLE CRACKED AT L2 DOOR JUST FORWARD OF TORQUE TUBE, BEHIND DOOR ESCAPE SLIDE INDICATOR. REMOVED CRACKED WEB FOUND TO BE OUT OF LIMITS ON L2 DOOR FORWA - [SDR AMTA200400801](https://openairdocs.org/sdr/AMTA200400801), Jun 25, 2004: PLATE. CRACKED. FOUND RIGHT WING T/E LOWER SPAR WIGGLE PLATE CRACKED AND PULLED FASTENERS BETWEEN WS 328 TO WS 336. FOUND CRACK TO BE OUT OF LIMITS. REMOVED AND REPLACED THE RT - [SDR AMTA200400710](https://openairdocs.org/sdr/AMTA200400710), Jun 10, 2004: SLIDE. OUT OF ADJUST. FOUND R4 DOOR SLIDE WOULD NOT ENGAGE PROPERLY. ADJUSTED AND LUBED IAW MM, OPS CHECK NORMAL PER 52-11-04-822-056. (M) - [SDR AMTA200400440](https://openairdocs.org/sdr/AMTA200400440), Apr 14, 2004: CONTROLLER. MALFUNCTIONED. ON TAKEOFF LT ENGINE BLEED OFF LIGHT ILLUMINATER. RESET UPON ARRIVAL AT KMDW SYSTEM NORMAL . REMOVED AND REPLACED REVERSE FLOW CHECK CONTROLLER IAW AMM - [SDR AMTA20040005](https://openairdocs.org/sdr/AMTA20040005), Jan 4, 2004: WIRE. DISCONNECTED. FOUND FOUR EMERGENCY FLOOR LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED WIRES, OPS CHECK GOOD. (M) - [SDR AMTA200301174](https://openairdocs.org/sdr/AMTA200301174), Sep 16, 2003: INDICATOR. INACCURATE. TOTAL FUEL DIFFERS FROM CAPTAIN. TOTAL FUEL DIFFERS FROM CAPTAIN AND F/O CALCULATED FUEL QUANITY FUEL QTY ERROR, PROG 2/2. ALT MESSAGE. (M) - [SDR AMTA200300899](https://openairdocs.org/sdr/AMTA200300899), Jul 7, 2003: WIRE. DISCONNECTED. FLT 584 - EMERGENCY FLOOR TRACK LIGHTS ROW'S 22 THROUGH 24 INOPERATIVE. RECONNECTED WIRING AT ROW 24, OPS CHECK GOOD. (M) - [SDR AMTA200300770](https://openairdocs.org/sdr/AMTA200300770), Jun 12, 2003: WIRE. DISCONNECTED. EGRESS FLOOR LIGHTING INOPERATIVE FROM SEAT ROW 22 TO 31. RECONNECTED WIRES TO EGRESS LIGHT AT ROW 28 AND AT ROW 30. OPS CHECK GOOD. (M) - [SDR AMTA200300637](https://openairdocs.org/sdr/AMTA200300637), May 11, 2003: LIGHT. INOPERATIVE. R1 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED R1 FORWARD GIRT BAR PROX SENSOR PER MM 25-66-11 AND SWPM CHAP 20. OPS NORMAL. (M) - [SDR AMTA200300576](https://openairdocs.org/sdr/AMTA200300576), Apr 29, 2003: WIRE. LOOSE. RED EGRESS LIGHT INOPERATIVE AT 29D. RECONNECTED LOOSE WIRE TO LAMP ASSEMBLY. OPS CHECK NORMAL. (M) - [SDR AMTA200300357](https://openairdocs.org/sdr/AMTA200300357), Mar 16, 2003: CONNECTOR. LOOSE. EGRESS LIGHTS BETWEEN ROWS 22-23, INOPERATIVE. SECURED LOOSE CONNECTION AT ROW 22. OPS CHECK NORMAL. (M) All 70: https://openairdocs.org/deregistered/N517AT-2010-01-27/reports.md ## Other aircraft with N517AT - [Registered now](https://openairdocs.org/aircraft/N517AT): Austin Andrew J RV-10, S/N 41237, built 2017 --- 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.