# N526NA: 1990 Boeing 757-236, registration cancelled 2018-03-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 8, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 757-236](https://openairdocs.org/model/boeing-757-236) (registry code 1384971) - Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (OpenAirDocs) - Serial number: 24794 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 8, 2000 - Certificate issued: September 24, 2013 - Last registry action: September 24, 2013 - Mode S code: A6A065 - Owner when cancelled: [Executive Jet Group I LLC](https://openairdocs.org/faa-owner/EXECUTIVE%20JET%20GROUP%20I%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N526NA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=526NA - Page: https://openairdocs.org/deregistered/N526NA-2018-03-08 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 757-236: https://openairdocs.org/model/boeing-757-236.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RYNA2011052300014](https://openairdocs.org/sdr/RYNA2011052300014), May 23, 2011: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT BATTERY PACKS WEAK AT L3 AND R3 DOORS. REMOVED AND REPLACED BATTERY PACKS PER AMM 33-51-07. OPERATIONAL CHECKED NORMAL. - [SDR RYNA2011010500002](https://openairdocs.org/sdr/RYNA2011010500002), Jan 3, 2011: GLOWSTRIP. BROKEN. PHOTO LUMINESCENT LIGHT IN FRONT OF AFT LAVATORY DOOR DAMAGED. REMOVED AND REPLACED BROKEN SECTION OF PHOTO LUMINESCENT LIGHT PER GMM 33-RY-02. - [SDR 2010FA0001248](https://openairdocs.org/sdr/2010FA0001248), Dec 16, 2010: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR LIGHT INOP. (EMERGENCY EXIT SLIDE LIGHT) - [SDR RYNA2010009020033](https://openairdocs.org/sdr/RYNA2010009020033), Sep 29, 2010: COVER. CRACKED. SEVERAL AREAS OF FLOOR PATH LIGHTING GLOW STRIPS MISSING LENS COVER OR COVER CRACKED. LENS COVER INSTALLED ON MISSING AREAS AND REPLACED WHERE CRACKED. - [SDR RYNA201000401010](https://openairdocs.org/sdr/RYNA201000401010), Mar 30, 2010: SLIDE. UNWANTED DEPLOY. L-2 DOOR SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED THE L-2 DOOR SLIDE PER AMM 25-66-07. OK FOR SERVICE. - [SDR RYNA201001190001](https://openairdocs.org/sdr/RYNA201001190001), Jan 19, 2010: RELAY. FAULTY. ON CLIMBOUT EQUIPMENT OVERHEAT CAME ILLUMINATED. TROUBLESHOOT PER THE FIM 21-58-00 FIG 108, REMOVED AND REPLACED THE AFT FAN SUPPLY 1 RELAY K10324 AND OPS CHECK - [SDR RYNA200912300030](https://openairdocs.org/sdr/RYNA200912300030), Dec 18, 2009: SUPPORT. CRACKED. DURING INSPECTION OF THE FORWARD BAGGAGE BIN AT THE AFT BULKHEAD THE VERTICAL SUPPORTS AT LBL STA 845 THE RBL 18 WERE FOUND CRACKED AT THE LOWER ATTACH FITTINGS - [SDR RYNA200912180028](https://openairdocs.org/sdr/RYNA200912180028), Dec 14, 2009: FLOORBEAM. CORRODED. DURING INSPECTION OF FLOORBEAMS AT STA 377 CORROSION WAS FOUND AT LBL 3.25 TO LT END OF FLOORBEAM. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PE - [SDR RYNA2009](https://openairdocs.org/sdr/RYNA2009), Dec 14, 2009: FLOORBEAM. CORRODED. DURING INSPECTION OF FLOORBEAMS AT STA 365 CORROSION WAS FOUND AT RBL 3.25 TO RBL 10.25. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PE - [SDR RYNA200912180026](https://openairdocs.org/sdr/RYNA200912180026), Dec 14, 2009: FLOORBEAM. CORRODED. DURING INSPECTION OF FLOORBEAMS AT STA 345 CORROSION WAS FOUND AT LBL 53.00 TO RBL 4.25. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PE - [SDR RYNA200909020018](https://openairdocs.org/sdr/RYNA200909020018), Aug 30, 2009: ACTUATOR. BYPASSING. AFTER TAKEOFF AIRCRAFT RETURNED TO RFD DUE TO MULTIPLE EICAS MESSAGES PROBE HEAT, TAT PROBE, AUTO THRUST MESSAGES APPEARED. TROUBLESHOT AIRCRAFT FOUND THE LT MA - [SDR RYNA200908310017](https://openairdocs.org/sdr/RYNA200908310017), Aug 30, 2009: PRESSURE SWITCH. FAILED. AFTER LIFTOFF PROBE HEAT, TAT AND AUTO THRUST EICAS MESSAGES APPEARED. T/S AIR/GND DISAGREE PER FIM 32-09-00 FIGURE 104 PAGE 114, 115, FIG 105 PAGES 116, 117, F - [SDR RYN2008F00018](https://openairdocs.org/sdr/RYN2008F00018), Sep 11, 2008: SLIDE. UNWANTED DEPLOY. F/O ACCIDENTALLY BLEW L1 DOOR SLIDE. C/A IN WORK. (K) - [SDR RYN2008F00021](https://openairdocs.org/sdr/RYN2008F00021), Sep 10, 2008: LINE. BROKEN. PILOT REPORT LT ENGINE NOT MAKING POWER AT FL 20000 WITH THE ENGINE POWER LEVER FULLY FWD AND N1 WAS ONLY 71 PERCENT. REPLACED THE LT ENGINE P1 PROBE BROKEN SEN - [SDR RYN2008F00011](https://openairdocs.org/sdr/RYN2008F00011), Aug 6, 2008: WINDSHIELD. CRACKED. ACFT RETURNED TO BUD. FLIGHT CREW ADVISED THAT THE LT NR 1 WINDSHIELD IS CRACKED ALONG THE LOWER SECTON OF THE WINDOW. WAITING FOR PARTS. OPEN. (S) - [SDR RYN2008F00009](https://openairdocs.org/sdr/RYN2008F00009), Jul 23, 2008: WINDSHIELD. CRACKED. LEFT NR 1 WINDSHIELD CRACKED. REPLACED LEFT NR 1 WINDSHIELD AND WINDOW HEAT CONTROLLER IAW AMM 56-11-01 AND AMM 50-41-01 OPS CHECKED NORMAL. (A) - [SDR RYN2008F00000](https://openairdocs.org/sdr/RYN2008F00000), Jul 1, 2008: COMPUTER. MALFUNCTIONED. AIR TURN BACK, DUE TO LOSS OF ALL 3 AUTO PILOTS AND THE CAPTAIN`S FLIGHT DIRECTOR, COULD NOT ENTER RVSM AIRSPACE. RESET LT FCC AND ACCOMPLISHED TEST 2 AND 10 IA - [SDR RYN2008F00004](https://openairdocs.org/sdr/RYN2008F00004), Jun 27, 2008: CONTROL PANEL. MALFUNCTIONED. AIR TURNBACK TO RFD FOR PRESSURE CONTROLLER PROBLEM, BOTH AUTO 1 AND AUTO 2 ARE SPIKING 200 TO 300 CABIN DIFFERENTIAL DURING CLIMB. REPLACED OVERHEAD CONTROL PA - [SDR RYN2008F00005](https://openairdocs.org/sdr/RYN2008F00005), Jun 20, 2008: STRUCTURE. DAMAGED. REPAIR SECTION 48 TAIL SKID DAMAGE. REPAIRED SECTION 48 IAW 6-1171-RE-01647. - [SDR RYNA200600007](https://openairdocs.org/sdr/RYNA200600007), Sep 5, 2006: PCU. FAILED. LOST LT SYSTEM HYDRAULIC FLUID DURING FLIGHT. REMOVED AND REPLACED RT ELEVATOR, CENTER POWER CONTROL UNIT (PCU) IAW MM 27-31-05. OPERATIONAL/FUNCTIONAL AND LEAK - [SDR RYNA200600006](https://openairdocs.org/sdr/RYNA200600006), Jul 10, 2006: SOFTWARE. MALFUNCTIONED. IRS - SOFTWARE MALFUNCTION NAV ERROR ON ALL 3 IRS'S. RELOADED NAV DATA, RE-ALIGNED IRS AND NO MALFUNCTION NOTED. - [SDR RYNA200600004](https://openairdocs.org/sdr/RYNA200600004), Mar 19, 2006: BOTTLE. LOW PRESSURE. R3 DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW, IN RED. REMOVED AND REPLACED EVACUATION SLIDE. - [SDR RYNA200500021](https://openairdocs.org/sdr/RYNA200500021), Jun 29, 2005: SKIN. DENTED. LT WING NR 3 LEADING EDGE SLAT TRAILIING EDGE WEDGE OUTBOARD FORWARD SURFACE HAS A DENT AT APPROX WS 560. REPAIRED DENT AT NR 3 SLAT TRAILING EDGE OUTBOARD LOWE - [SDR RYNA200500025](https://openairdocs.org/sdr/RYNA200500025), Jun 24, 2005: SHEAR PLATE. CORRODED. SHEAR SKIN HAS CORRISION AT BS 1720 TO 1681 RBL 50 TO LBL 50 AFT CABIN. CLEANED CORROSION BELOW SHEAR PLATE AND FLOORBEAM IAW B757 SRM 51-40-2 (LIGHT CORRISION) - [SDR RYNA200500024](https://openairdocs.org/sdr/RYNA200500024), Jun 24, 2005: SKIN. SEPARATED. TRAILING EDGE OF LEFT ELEVATOR AT STATION 76.547 IS SEPARATED APPROXIMATELY 1 INCH. ELEVATOR REPAIRED PER B757 SRM 51-70-04. - [SDR RYAN200500019](https://openairdocs.org/sdr/RYAN200500019), May 25, 2005: FLOORBEAM. CORRODED. FLOORBEAM HAS CORROSION AT UPPER CAP BS 1640 RBL48. - [SDR RYNA200500001](https://openairdocs.org/sdr/RYNA200500001), Dec 30, 2004: MODULE. FOD. LEFT ENGINE FIRE LOOP NR 2 STATUS MESSAGE ILLUMINATED ON DESCENT. CLEANED FOD FROM AFOLTS CARD FILE MODULE. OPERATIONAL CHECK NORMAL. - [SDR 02070901](https://openairdocs.org/sdr/02070901), Jul 9, 2002: CONTROL UNIT. MALFUNCTIONED. AFTER DISCONNECT, BEGAN TO TAXI, HEARD MUFFLED POPPING NOISE. LEFT ENGINE QUIT. RETURNED TO GATE. BVCU BITE FAILED, BVCU REMOVED AND REPLACED. FUNCTIONAL CHECK - [SDR 2002F00070](https://openairdocs.org/sdr/2002F00070), Dec 22, 2001: FLOORBEAM. CORRODED. DURING C-CHECK, FLOORBEAM UPPER CHORD FOUND CORRODED, BS 324, RBL 58, WL 208. REPAIRED UPPER CHORD PER SRM. (M) - [SDR 2002F00069](https://openairdocs.org/sdr/2002F00069), Dec 22, 2001: SKIN. CHAFED. RIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 3 INCHES FROM END CHAFFED. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTED USING HFEC EVERY C-CHECK. - [SDR 2002F00068](https://openairdocs.org/sdr/2002F00068), Dec 22, 2001: SKIN. CHAFED. LEFT FORWARD OUTBOARD FLAP, OUTBOARD END, LEADING EDGE CHAFED. DRESSED OUT AND INSTALLED REPAIR EPR SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M) - [SDR 2002F00067](https://openairdocs.org/sdr/2002F00067), Dec 22, 2001: SKIN. CHAFED. RIGHT OUTBOARD MAIN FLAP, INBOARD END, LEADING EDGE GOUGE 24 INCHES LONG. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTION USING HFEC EVERY C-CHECK. (M) - [SDR 2002F00066](https://openairdocs.org/sdr/2002F00066), Dec 22, 2001: SKIN. CHAFED. RIGHT OUTBOARD MAIN FLAP, OUTBOARD END, LEADING EDGE 56 INCHES FROM INBOARD END. DRESSED OUT AND INSTALLED REPAIR PER SRM. REINSPECTION USING HFEC EVERY C-CHECK - [SDR 2002F00061](https://openairdocs.org/sdr/2002F00061), Dec 22, 2001: FLOOR SUPPORT. CORRODED. DURING C-CHECK, L1 DOOR THRESHOLD FLOOR SUPPORT WAS FOUND CORRODED. REPLACED SUPPORT PER SRM. (M) - [SDR 2002F00065](https://openairdocs.org/sdr/2002F00065), Dec 4, 2001: ANGLE. CORRODED. DURING COMPLIANCE WITH CPCP TASK CORROSION FOUND ON KEEL BEAM LOWER L ANGLE BRACKETS AT BS 1139, LBL 4 TO RBL 4, WL 143. MANUFACTURED AND REPLACED L ANGLE PER S - [SDR 20010425AP008](https://openairdocs.org/sdr/20010425AP008), Mar 16, 2001: HOSE. RUPTURED. LOST LEFT HYDRAULIC SYSTEM IN FLIGHT, RETURNED TO STATION AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED BURST HOSE ASSEMBLY IN LEFT MLG WHEEL WELL. REPLAC - [SDR 20010214SG002](https://openairdocs.org/sdr/20010214SG002), Jan 7, 2001: TRANSDUCER. INOPERATIVE. AIR RETURN DUE TO AFTER TAKEOFF CREW O2 DROPPED TO 10 PSI. RETURNED TO NORMAL AFTER LANDING. PLACARDED CREW 02 PRESS INDICATION ON EICAS PER MEL 35-11-02 SIT 1. ## Other aircraft with N526NA - [Registered now](https://openairdocs.org/aircraft/N526NA): Zipline International P2 ZIP, S/N 18735P2871 --- 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.