# N918UW: 1982 Boeing 757-225, registration cancelled 2011-08-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 22, 2011 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 757-225](https://openairdocs.org/model/boeing-757-225) (registry code 1384959) - Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs) - Serial number: 22196 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 22, 1982 - Certificate issued: February 14, 2005 - Last registry action: September 15, 2009 - Mode S code: ACB63A - Owner when cancelled: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE) - Location: [Boston, MA](https://openairdocs.org/faa-place/MA/Boston) - Owner type: Corporation - Owner's area on the map: 42.3582° N, 71.0519° W: Placed by OpenAirDocs at the center of ZIP code 02110, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N918UW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918UW - Page: https://openairdocs.org/deregistered/N918UW-2011-08-22 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 Boeing 757-225: https://openairdocs.org/model/boeing-757-225.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA20090817BB124](https://openairdocs.org/sdr/USAA20090817BB124), Aug 17, 2009: HARNESS. FRAYED. PHL - HARNESS FRAYED. MAINTENANCE REPLACED SLIDE. - [SDR USAA20090817BB123](https://openairdocs.org/sdr/USAA20090817BB123), Aug 16, 2009: LIGHT. INOPERATIVE. SJU-PHL WHILE INBOUND TO PHL, THE FLIGHT SHOWED A RT MLG UNSAFE LIGHT ON. CAPTAIN USED ALT EXTENSION PROCEDURE AND DID A FLY BY TO CONFIRM GEAR WAS DOWN BECAUSE - [SDR USAA20090519BB084](https://openairdocs.org/sdr/USAA20090519BB084), May 16, 2009: CHARGER. FAULTY. PHL - EMERGENCY LIGHTS AT ROW 13 RIGHT AND 19 LEFT ARE INOP. MAINTENANCE INSTALLED A NEW CHARGER ASSY. - [SDR USAA20090403BB056](https://openairdocs.org/sdr/USAA20090403BB056), Mar 31, 2009: ACTUATOR. FAULTY. CLT FLT 1085 EN ROUTE CLT TO MCO. AFTER TAKEOFF, WHEN GEAR HANDLE PLACED UP, RECEIVED EICAS MESSAGE "GEAR DISAGREE", AND "GEAR DOORS". AIRFRAME VIBRATION WAS EX - [SDR USAA20090224BB039](https://openairdocs.org/sdr/USAA20090224BB039), Feb 20, 2009: GCU. FAULTY. STT FLT 1041 EN ROUTE STT TO CLT. DURING CLIMBOUT FROM STT, AT APPROXIMATELY 800 FEET, THE CAPTAIN'S COCKPIT INSTRUMENTS WENT BLANK. THE CREW PERFORMED A CROSS - [SDR USAABB08174](https://openairdocs.org/sdr/USAABB08174), Dec 7, 2008: BOLT. LOOSE. FLT 816 EN ROUTE. DURING DESCENT, FLT RECEIVED AN INDICATION OF NO OIL PRESSURE IN NR 2 ENGINE. CREW SHUTDOWN NR 2 ENGINE. LANDED WITHOUT FURTHER INCIDENT. SING - [SDR USAA920081933](https://openairdocs.org/sdr/USAA920081933), Oct 21, 2008: PANEL. CRACKED. CLT C3 MAJOR REPAIR NR 19C51057012/001 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 30 INCHES FROM OTBD END. REPAIRED NR 1 SLAT CLOVE PANEL AT OTBD SLAT TRAC - [SDR USAA920081934](https://openairdocs.org/sdr/USAA920081934), Oct 21, 2008: PCU. CRACKED. CLT C3 MAJOR REPAIR NR 19C51057012/004 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 27 INCHES FROM OTBD END. REPAIRED NR 1 SLAT COVE PANEL AT OTBD SLAT TRACK - [SDR USAABB08076](https://openairdocs.org/sdr/USAABB08076), Apr 29, 2008: BEARING. SPALLED. AUA FLT 854 AUA TO PHL. SHORTLY AFTER TAKEOFF, THE LEFT ENGINE OIL PRESSURE DROPPED TO 10 PSI AND HAD A RESPECTIVE DROP IN OIL QUANTITY. THE CREW SHUT DOWN THE - [SDR BB08076](https://openairdocs.org/sdr/BB08076), Apr 29, 2008: ENGINE. UNKNOWN. AUA - FLT 854 AUA TO PHL. SHORTLY AFTER TAKEOFF, THE LEFT ENGINE OIL PRESSURE DROPPED TO 10 PSI AND HAD A RESPECTIVE DROP IN OIL QUANTITY. THE CREW SHUT DOWN TH - [SDR USAA920080702](https://openairdocs.org/sdr/USAA920080702), Mar 26, 2008: FRAME. CRACKED. CLT - MAJOR REPAIR - CRACKED FRAME WEB, BS 560, S22R - S23R. REPAIRED FRAME WEB, BS 560, S22R - S23R IAW B737 SRM 53-00-07 REPAIR 2. - [SDR BB07105](https://openairdocs.org/sdr/BB07105), Dec 27, 2007: CONTROLLER. FAILED. FLIGHT 815, CLT-CUN: DURING CLIMB, CREW REPORTED FAILURE OF LEFT PACK WHILE THE RIGHT PACK WAS ALREADY ON MEL. INITIATED EMERGENCY DESCENT TO 10,000 FEET AND RE - [SDR BB07100](https://openairdocs.org/sdr/BB07100), Dec 17, 2007: DUCT. LEAKING. FLIGHT 790, CLT-BOS: AIRCRAFT DIVERTED TO PHL DUE TO A NUMBER 2 ENGINE OVERHEAT MESSAGE. CREW REDUCED THROTTLE TO IDLE AND WARNING WENT AWAY. MAINTENANCE REPLAC - [SDR USAA920071121](https://openairdocs.org/sdr/USAA920071121), Nov 10, 2007: SHEAR TIE. CORRODED. CLT - MAJOR REPAIR - CORROSION ON SHEAR TIE, BS 480, S24R - S25R. REPLACED SHEAR TIE, BS 480, S24R - S25R IAW B757 SRM 51-40-02. - [SDR USAA920071120](https://openairdocs.org/sdr/USAA920071120), Nov 10, 2007: SHEAR TIE. CORRODED. CLT - MAJOR REPAIR - CORROSION ON SHEAR TIE, BS 480, S23R - S24R. REPLACED SHEAR TIE, BS 480, S23R - S24R IAW B757 SRM 51-40-02. - [SDR USAA920071110](https://openairdocs.org/sdr/USAA920071110), Nov 10, 2007: STRINGER. CORRODED. CLT - MAJOR REPAIR - CORROSION ON STRINGER, BS 457, S25R. REPAIRED STRINGER, BS 457, S25R IAW USAIRWAYS EA 100010. - [SDR USAA070251](https://openairdocs.org/sdr/USAA070251), Mar 30, 2007: FRAME. CORRODED. BS 900, WL 138.5 ON FRAME HAS CORROSION. FAB'D REPAIR ANGLES, T-CHORDS, INSTALLED ALL PARTS PER SRM 51-70-12, 51-40-02; DEFECT SIZE: 12"L X 1.70"W X .041"D. - [SDR USAA070252](https://openairdocs.org/sdr/USAA070252), Mar 30, 2007: STRINGER. CORRODED. STA 446 STR 22R HAS CORROSION. FAB'D & INSTALLED REPAIR PARTS PER SRM 53-00-03, FIG 201, 53-00-03, FIG 101, DEFECT SIZE: .900" L X .700'W X .700"D. --- 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.