# N757NA: 1990 Boeing 757-23A, registration cancelled 2005-06-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 28, 2005
- Exported to: Iceland
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967)
- Engine: [Rolls-Royce RB211-535E437](https://openairdocs.org/engine/rolls-royce-rb211-535e437) (registry code 54053)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Serial number: 24567
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, showing compliance
- Airworthiness date: June 9, 2005
- Certificate issued: October 9, 2001
- Last registry action: October 19, 2004
- Mode S code: AA3537
- Owner when cancelled: [Awms I](https://openairdocs.org/faa-owner/AWMS%20I)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7586° N, 73.9679° W: Placed by OpenAirDocs at the center of ZIP code 10022, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N757NA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=757NA
- Page: https://openairdocs.org/deregistered/N757NA-2005-06-28

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 757-23A: https://openairdocs.org/model/boeing-757-23a.md

## Service difficulty reports (32)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 02061802](https://openairdocs.org/sdr/02061802), Jun 15, 2002: STRINGER. DENTED. STRINGER 16L DENTED AT BS 612 AND BS 617. REPAIRED AS PER SRM 53-00-03 FIGURE 201 AND ER 02-0687.
- [SDR 02061801](https://openairdocs.org/sdr/02061801), Jun 14, 2002: SKIN. DENTED. TWO DENTS IN SKIN, BS 611 AND 615 AT STR 16L LBL 65. INSTALLED DOUBLER OVER DAMAGE; CUTOUT PER SRM 53-00-01 AND ER 02-0687.
- [SDR 02042901](https://openairdocs.org/sdr/02042901), Apr 27, 2002: LIGHT. Seat 16C Emergency Light INOP. Deferred I.A.W. MEL 33-51-03 Situation 1 Category C Authorization Number 57-0233. Removed and Replaced Light Assembly; Light Asse
- [SDR 2002F00104](https://openairdocs.org/sdr/2002F00104), Jan 14, 2002: WIRE HARNESS. DAMAGED. EMERGENCY ESCAPE PATH LIGHTING SEAT 27ABC INOPERATIVE. INVESTIGATION REVEALED WIRES BROKEN AND BURNED AT PLUG. REPLACED WIRING HARNESS. (M)
- [SDR 2001F00050](https://openairdocs.org/sdr/2001F00050), Jun 3, 2001: WIRE. CUT. FOUND FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT AT ROW 18 INOPERATIVE, WIRES CUT AT LIGHT. SPLICED WIRES AND RESTOWED CORRECTLY. (M)
- [SDR 20010320SG002](https://openairdocs.org/sdr/20010320SG002), Jan 14, 2001: FSEU. FAILED. ON APPROACH, WHEN FLAPS 30 WAS SELECTED FLAPS WOULD NOT EXTEND BEYOND 25, LEADING EDGE LIGHT CAME ON. NORMAL FLAPS 25 LANDING ACCOMPLISHED. ADJUSTED SLAT 5 LOSS
- [SDR 20010316SG002](https://openairdocs.org/sdr/20010316SG002), Jan 14, 2001: FSEU. FAILED. ON APPROACH WHEN FLAPS 30 WAS SELECTED FLAPS WOULD NOT EXTEND BEYOND 25, LEADING EDGE LIGHT CAME ON. NORMAL FLAPS 25 LANDING ACCOMPLISHED. ADJUSTED SLAT 5 LOSS 
- [SDR N8TA00051701](https://openairdocs.org/sdr/N8TA00051701), May 17, 2000: HOSE. LEAKING. THREE MINUTES AFTER TAKEOFF, CREW OBSERVED EICAS MESSAGE, LEFT HYDRAULIC SYSTEM QUANTITY AND QUANTITY DROPPED TO .20; SYSTEM WAS DEPRESSURIZED. ALL GEAR EXTENSI
- [SDR 99ZZZM805](https://openairdocs.org/sdr/99ZZZM805), Oct 6, 1999: CONTROL. FAILED. DURING TRANSITION FROM HIGH CLIMB POWER TO CRUISE POWER LT ENGINE APPEARED TO SURGE. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO AND AFTER SURGE EVENT. REMOVED 
- [SDR N8TA990801](https://openairdocs.org/sdr/N8TA990801), Aug 1, 1999: FUEL NOZZLE. DISPLATED. DURING TALKEOFF, FIRE WARING ACTIVATED FOR NR 2 ENGINE. CREW INITIATED FIRE EXTINGUISHER AND ENGINE SHUT DOWN PROCEDURES. PRELIMINARY INVESTIGATION REVEALED COM
- [SDR NOCA0299](https://openairdocs.org/sdr/NOCA0299), Feb 21, 1999: LIGHT. INOPERATIVE. JFK - FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR FOUND INOPERATIVE DURING INSPECTION. REPLACED FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR. OPS CHECK
- [SDR NOCA0199C](https://openairdocs.org/sdr/NOCA0199C), Jan 18, 1999: TEMP SENSOR. INOPERATIVE. DURING FLIGHT, CABIN TEMP INCREASE, CREW ATTEMPTED TO REGULATE BY USING TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT . CABIN ALTITUDE STARTED TO CLIMB. CREW C
- [SDR NOCA0199B](https://openairdocs.org/sdr/NOCA0199B), Jan 18, 1999: VALVE. INOPERABLE. DURING FLIGHT, CABIN TEMP INCREASE, CREW ATTEMPTED TO REGULATE BY USING TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT. CABIN ALTITUDE STARTED TO CLIMB. CREW CO
- [SDR NOCA0199A](https://openairdocs.org/sdr/NOCA0199A), Jan 18, 1999: WATER NOZZLE. INOPERATIVE. DURING FLIGHT, CABIN TEMPERATURE INCREASE, CREW ATTEMPTED TO REGULATE BY USING THE TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT. CABIN ALTITUDE STARTED TO CLI
- [SDR NOCA2598](https://openairdocs.org/sdr/NOCA2598), Nov 19, 1998: SCREEN. CONTAMINATED. IN FLIGHT APU START SCHEDULED BY MAINTENANCE. APU IN FLIGHT START UNSUCCESSFUL. ON GROUND INSPECTION OF APU INLET PLENUM FOUND DEBRIS ON INLET SCREEN. DEBRIS RE
- [SDR NOCA2298](https://openairdocs.org/sdr/NOCA2298), Oct 5, 1998: SLIDE. MALFUNCTIONED. ON CREW TRAINING OF EMERGENCY EVACUATION, THE R-3 DOOR EVACUATION SIDE DID NOT DEPLOY AUTOMATICALLY ON DOOR OPENING, IT HAD TO BE MANUALLY DEPLOYED. ESCAPE SLID
- [SDR NOCA2198](https://openairdocs.org/sdr/NOCA2198), Oct 2, 1998: VALVE. INOPERATIVE. SNN - ACCOMPLISHED HIGH ENERGY STOP INSPECTION. NO DISCREPANCIES NOTED. PERFORMED RIGHT ENGINE RUN UP. BLEED LIGHT CAME ON AT 90 PERCENT. BLEED SWITCH POSITIONE
- [SDR NOCA2098](https://openairdocs.org/sdr/NOCA2098), Sep 27, 1998: ELT. INOPERATIVE. EMERGENCY LOCATOR TRANSMITTER SIGNAL INTERMITTENTLY TRANSMITTING DURING FLIGHT. SIGNAL CAN BE HEARD ON 121.5. REPLACED ELT TRANSMITTER. (M)
- [SDR NOCA1398](https://openairdocs.org/sdr/NOCA1398), May 6, 1998: GOVERNOR. MALFUNCTIONED. ON TAKEOFF, MAX EPR ATTAINABLE FROM LEFT ENGINE WAS 1.46. TAKEOFF REJECTED. REPLACED LEFT ENGINE FUEL FLOW GOVERNOR. OPS CHECK NORMAL. (M)
- [SDR 98ZZZX2021](https://openairdocs.org/sdr/98ZZZX2021), Apr 13, 1998: TRACK COVER. DISLODGED. THREE INCH SECTION OF E-PATH TRACK COVER DISLODGED FROM AFT END OF TRACK. SECURED E-PATH TRACK COVER. OPERATIONAL CHECK OK.
- [SDR NOCA0898](https://openairdocs.org/sdr/NOCA0898), Mar 26, 1998: ELT. MALFUNCTIONED. EMERGENCY LOCATOR TRANSMITTER SIGNAL ACTIVATED ON DESCENT, SIGNAL CAN BE ON 121.5. REMOVED AND REPLACED ELT TRANSMITTER. OPERATIONAL CHECK OF ELT OK. (M)
- [SDR NOCA0798](https://openairdocs.org/sdr/NOCA0798), Mar 13, 1998: RESERVOIR. MALFUNCTIONED. R-4 DOOR SLIDE INADVERTENTLY DEPLOYED ON GROUND AT JFK. SLIDE/RAFT OPERATION NORMAL. INSPECTED AREA AND REPLACED R-4 DOOR SLIDE/RAFT. REPLACED DOOR ASSIST RESER
- [SDR NOCA0498](https://openairdocs.org/sdr/NOCA0498), Jan 12, 1998: ACTUATOR. FAILED. GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENDED. FOUND RIGHT MLG DOOR OPEN APPROXIMATELY 18 INCHES. VISUALLY INSPECTED RT MLG DOOR, DOOR SEALS, AND SUR
- [SDR NOCA1197](https://openairdocs.org/sdr/NOCA1197), Dec 6, 1997: WIRE. DISCONNECTED. EMERGENCY PATH LIGHTS INOP AT ROWS 31, 32 AND 34 THROUGH 37. FOUND WIRE DISCONNECTED AT ROW 33. RECONNECTED AND SECURED, OPS CHECKED OK. (M)
- [SDR NOCA1097](https://openairdocs.org/sdr/NOCA1097), Nov 27, 1997: BULB. FAILED. EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. RELAMPED EXTERIOR LIGHT AT DOOR 2L, OPS CHECKED OK. ITEM FOUND DURING DAILY CHECK AT JFK. (M)
- [SDR NOCA0997](https://openairdocs.org/sdr/NOCA0997), Nov 14, 1997: WIRE. LOOSE. ON A DAILY CHECK, FOUND E-PATH LIGHTS IN ROWS 10 TO 12 INOPERATIVE. FOUND LOOSE WIRE IN ROW 12C. RECONNECTED LOOSE WIRE, SYSTEM RETURNED TO NORMAL. (M)
- [SDR NOCA0897](https://openairdocs.org/sdr/NOCA0897), Oct 22, 1997: LAMP. BROKEN. 'E' PATH SEAT 16C LAMP INOP. REPLACED LAMP. (M)
- [SDR NOCA0297](https://openairdocs.org/sdr/NOCA0297), Feb 5, 1997: SLIDE. DEPLOYED. BWI - L4 DOOR SLIDE/RAFT INADVERTENTLY DEPLOYED BY GROUND SERVICE PERSONNEL, DUE TO SLIDE/RAFT BEING LEFT IN THE ENGAGED POSITION. INSPECTED THE AREA AND REPLAC
- [SDR NOCA0896](https://openairdocs.org/sdr/NOCA0896), Sep 19, 1996: LIGHT. LOOSE. RED LIGHT ASSEMBLY E-PATH AT DOOR 1L REQUIRED TO BE RESECURED. SECURED LIGHT ASSEMBLY, CHECKS OK. (M)
- [SDR NOCA0796](https://openairdocs.org/sdr/NOCA0796), Sep 19, 1996: LIGHT. INOPERATIVE. L1 RED LAMP ASSEMBLY INOP AT DOOR 1L. REPLACED LAMP ASSEMBLY, CHECKS OK. (M)
- [SDR 96ZZZM1384](https://openairdocs.org/sdr/96ZZZM1384), Aug 11, 1996: LIGHT. INOP. E-PATH LIGHT AT 31-33 ABC INOP. REPAIRED WIRES, CHECKED OK. EXTERIOR EMERGENCY LIGHT AT 3L DOOR INOP. RELAMPED, CHECKED OK. E-PATH LIGHT AT 5ABC INOP. RELAMPED,
- [SDR 95ZZZW433](https://openairdocs.org/sdr/95ZZZW433), Mar 28, 1995: PIVOT BOLT. MISSING. JFK - L4 DOOR SLIDE POSITION RETRACTABLE DOOR INDICATOR FAILED TO EXTEND WHEN DOOR IN ENGAGED POSITION. REPLACED PIVOT BOLT ASSEMBLY PER MM. OPERATIONAL CHECK O

## 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 BFO93IA175](https://openairdocs.org/ntsb/BFO93IA175), Sep 13, 1993: Boeing 757-200ER (N757NA), Jamaica, NY, incident, no damage. Probable cause: THE FAILURE OF THE LEFT HYDRAULIC PRESSURE SWITCH, WHICH CAUSED THE LEFT YAW DAMPER MODULE TO BECOME INOPERATIVE RESULTING IN UNCOMMANDED RUDDER MOVEMENTS DURING FLIGHT.

## FAA accident and incident reports (4)

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 20000107002559I](https://openairdocs.org/incident/20000107002559I), Jan 7, 2000: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. Flight 351 enroute from dfw to las on decent to Las Vegas could not deploy leading edge slats. Pliot and first officer followed in their qrh declaredan…
- [Incident 19990826024829I](https://openairdocs.org/incident/19990826024829I), Aug 26, 1999: Boeing 75723A (N757NA), Las Vegas, NV, Minor damage. During rotation a fire bell sounded and fire warning light illuminated on right engine. Smoke and fire was reported to the crew by ATC. Two f/a's aboard…
- [Incident 19940403009589I](https://openairdocs.org/incident/19940403009589I), Apr 3, 1994: Boeing 75723A (N757NA), Des Moines, IA. Lost oil presure. Secured NR1 engine. Found P3 sealing air tube had failed.
- [Incident 19930913038109I](https://openairdocs.org/incident/19930913038109I), Sep 13, 1993: Boeing 75723A (N757NA), New York, NY. Rudder ratio eicas message came on at alitude. Returned. Landed safely. Replaced righ rudder contro module.

## Other aircraft with N757NA

- [Registered now](https://openairdocs.org/aircraft/N757NA): Schempp Hirth Flugzeugbau ARCUS M, S/N 137, built 2016
- [Cancelled 1980-04-18](https://openairdocs.org/deregistered/N757NA-1980-04-18): Cessna 152, S/N 15279862. Exported to Iceland. Owner: [Maine Aviation Corp](https://openairdocs.org/faa-owner/MAINE%20AVIATION%20CORP), [Portland, ME](https://openairdocs.org/faa-place/ME/Portland)

---
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.