# N801MA: 2004 Embraer ERJ 170-100SU, registration cancelled 2017-06-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 2, 2017
- Exported to: Bermuda
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 170-100SU](https://openairdocs.org/model/embraer-erj-170-100su) (registry code 3260403)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A56NM](https://openairdocs.org/tcds/A56NM) (OpenAirDocs)
- Serial number: 17000012
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 2004
- Certificate issued: March 5, 2004
- Last registry action: June 22, 2016
- Mode S code: AAE6A8
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N801MA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801MA
- Page: https://openairdocs.org/deregistered/N801MA-2017-06-02

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 Embraer ERJ 170-100SU: https://openairdocs.org/model/embraer-erj-170-100su.md

## Service difficulty reports (108, newest 50)

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

- [SDR R61A201511150839](https://openairdocs.org/sdr/R61A201511150839), Nov 15, 2015: UNKNOWN. ODOR. CREW REPORTED A BURNING ODOR IN THE COCKPIT FROM THE AIR CONDITIONING PACK 1. INSPECTED THE HEAT EXCHANGER AND ACM, RAN PACK OFF APU AND ENGINE AT POWER IAW AMM
- [SDR R61A201511040781](https://openairdocs.org/sdr/R61A201511040781), Nov 4, 2015: CONNECTOR. DISCONNECTED. CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 2 WAS NOT LIGHTING UP. MAINTENANCE RECONNECTED ROW 2 CEILING PANEL C/P IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201505120287](https://openairdocs.org/sdr/R61A201505120287), May 12, 2015: AUTOTHROTTLE SYS. FAILED. CREW REPORTED THAT THE AUTOPILOT AND AUTOTHROTTLES DISENGAGED AND CREW RECEIVED AN AVNX MAU1A FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY. WITH PASSENG
- [SDR R61A201504110236](https://openairdocs.org/sdr/R61A201504110236), Apr 11, 2015: RAMP. OUT OF ADJUST. PASSING THRU 8500 FT CREW RECEIVED AN AFT DOOR OPEN INDICATION. CREW LEVELED OFF AT 10000 FT, RAN QRH AND NOTED THAT THE PRESSURIZATION WAS NOT OPERATING NORMAL
- [SDR R61A201503300224](https://openairdocs.org/sdr/R61A201503300224), Mar 30, 2015: RIB. CORRODED. DURING HEAVY CHECK, FIXED T/E RIB 10 LT WING REQUIRES ALTERNATE MEANS OF REPAIR. MX FIXED T/E RIB 10 LT WING REQUIRES ALTERNATE MEANS OF REPAIR, IAW SB 170-57-0
- [SDR R61A201503250226](https://openairdocs.org/sdr/R61A201503250226), Mar 25, 2015: RIB. CRACKED. DURING HEAVY CHECK, LT WING, RIB 10 CRACKED CHORD WISE JOINT, SPLICE GOING FWD, CRACK LIKE INDICATIONS IN FASTENER HOLE JUST OTBD OF SKIN SPLICES IAW ETD 2013-1
- [SDR R61A201503250225](https://openairdocs.org/sdr/R61A201503250225), Mar 25, 2015: RIB. CRACKED. DURING HEAVY CHECK, RT WING AFT RIB 10 HOLE IN INBD LOWER FLANGE JUST FWD OF SPAR 2 IS CRACKED CRACKS RADIATING INBD AND OTBD FROM HOLE. MAINTENANCE REPAIRED HO
- [SDR R61A201503240199](https://openairdocs.org/sdr/R61A201503240199), Mar 24, 2015: FITTING. CRACKED. DURING HEAVY CHECK, LT WING STUBB FITTING AT SPAR 3 , RIVET REPLACEMENT HOLE HAS CRACK LIKE INDICATION. MAINTENANCE UP SIZED HOLE SIZED PLUGS, INSTALLED IAW ETD
- [SDR R61A201503240198](https://openairdocs.org/sdr/R61A201503240198), Mar 24, 2015: FITTING. CRACKED. DURING HEAVY CHECK, RT WING STUB FITTING AT SPAR 3 RIVET REPLACEMENT HOLE HAS CRACKED. MAINTENANCE UP SIZED HOLE TO 560, IAW SB-170-57-0038. AND OVER SIZED PLUG
- [SDR R61A201503230223](https://openairdocs.org/sdr/R61A201503230223), Mar 23, 2015: BUSHING. CORRODED. DURING HEAVY CHECK, NR 5 HINGE MOUNT INBD BUSHING, LT ELEVATOR IS CORRODED. MAINTENANCE R & R NR 5 HINGE MOUNT INBD BUSHING LT ELEVATOR IAW AMM 20-10-08. PN PE6
- [SDR R61A201503230222](https://openairdocs.org/sdr/R61A201503230222), Mar 23, 2015: BUSHING. CORRODED. WHILE IN HEAVY CHECK WAS REPORTED THAT NR 1 HINGE FITTING INBD BUSHING ON LT ELEVATOR IS CORRODED. MAINTENANCE R & R NR 1 HINGE FITTING INBD BUSHING ON LT ELEVA
- [SDR R61A201503230221](https://openairdocs.org/sdr/R61A201503230221), Mar 23, 2015: NIPPLE. CORRODED. DURING HEAVY CHECK AFT MOST REAR FUSELAGE DRAIN TUBE NIPPLE AND NUT ARE CORRODED. MAINTENANCE R & R AFT MOST REAR FUSELAGE DRAIN TUBE NIPPLE AND NUT IAW AMM 53-
- [SDR R61A201503220213](https://openairdocs.org/sdr/R61A201503220213), Mar 22, 2015: BOLT. CORRODED. DURING HEAVY CHECK, HYDRAULIC SYSTEM NR 2 DUMP VALVE BOLT CORRODED. MX R & R HYDRAULIC SYSTM NR 2 DUMP VALVE BOLT IAW AMM 29-11-26.
- [SDR R61A201503220205](https://openairdocs.org/sdr/R61A201503220205), Mar 22, 2015: SEAT TRACK. CORRODED. DURING HEAVY CHECK, FWD FUSELAGE FLOOR STRUCTURE AT FRAME 19 IS CORRODED. MAINTENANCE R & R LT INBD FF SEAT TRACK EXTENSION IAW SRM 51-40-02, 51-43-01, 51-43-02
- [SDR R61A201503210212](https://openairdocs.org/sdr/R61A201503210212), Mar 21, 2015: DAMPENER. CORRODED. DURING HEAVY CHECK FWD SERVICE DOOR DAMPENER HAS CORROSSION. MX R & R FWD SERVICE DOOR DAMPENER IAW AMM 52-41-27.
- [SDR R61A201503210211](https://openairdocs.org/sdr/R61A201503210211), Mar 21, 2015: BOLT. CORRODED. DURING HEAVY CHECK, L1 DOOR FWD SIDE BOLTS ON DOORS LOCKING AND ACTUATING MECHANISM HANDLE ARE CORRODED. MAINTENANCE R & R L1 DOOR FWD SIDE BOLTS ON DOORS LOCKI
- [SDR R61A201503210210](https://openairdocs.org/sdr/R61A201503210210), Mar 21, 2015: BOLT. CORRODED. DURING HEAVY CHECK, LT WING NR 3 SPOILER HARDWARE IS CORRODED. MAINTENANCE R & R LT WING NR 3 SPOILER HARDWARE IAW AMM 27-65-0-1, PN NAS6212-31D, BOLT. ACFT REM
- [SDR R61A201503210209](https://openairdocs.org/sdr/R61A201503210209), Mar 21, 2015: BOLT. CORRODED. DURING HEAVY CHECK, LT WING SPOILER, NR 4 ACTUATOR HARDWARE IS CORRODED. MAINTENANCE R & R LT WING SPOILER NR 4 ACTUATOR HARDWARE IAW AMM 27-05-01.
- [SDR R61A201503210208](https://openairdocs.org/sdr/R61A201503210208), Mar 21, 2015: BOLT. CORRODED. DURING HEAVY CHECK, RT WING NR 2 GROUND SPOILER HARDWARE AT ACTUATOR IS CORRODED. MX R & R RT WING NR 2 GROUND SPOILER HARDWARE AT ACTUATOR IAW AMM 27-61-01.
- [SDR R61A201503210207](https://openairdocs.org/sdr/R61A201503210207), Mar 21, 2015: SPIGOT. CORRODED. DURING HEAVY CHECK, AFT GALLEY SPIGOT IS CORRODED. MAINTENANCE R & R AFT GALLEY SPIGOT IAW CMM 25-33-55. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
- [SDR R61A201503220206](https://openairdocs.org/sdr/R61A201503220206), Mar 20, 2015: SEAT. CRACKED. DURING HEAVY CHECK, SEAT PAN CRACKED. MAINTENANCE R & R THE SEAT PAN.
- [SDR R61A201410181123](https://openairdocs.org/sdr/R61A201410181123), Oct 18, 2014: FLASHLIGHT. INOPERATIVE. CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS INOPERATIVE. R & R THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201409211067](https://openairdocs.org/sdr/R61A201409211067), Sep 21, 2014: PROCESSOR. FAILED. CREW RECEIVED NUMEROUS MESSAGES, AVNX MAU 3B FAIL, SPOILER FAULT, RUDDER FAIL, RT ELEV FAIL AND ENG 1 & ENG 2, NO DISPATCH. CREW RAN THE QRH, DISCONNECTED THE A
- [SDR R61A201409111052](https://openairdocs.org/sdr/R61A201409111052), Sep 11, 2014: BLEED VALVE. FAILED. AROUND 6000 FEET, CREW RECEIVED A BLEED 1 OVERPRESSURE MESSAGE. CREW RAN QRH, HOWEVER MESSAGE REMAINED. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WHE
- [SDR R61A201403020355](https://openairdocs.org/sdr/R61A201403020355), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, RT WING FUEL TUBE INSIDE PANEL 631EB IS CORRODED. MX R & R RT WING FUEL TUBE IAW AMM 20-10-03, PN 170-06041-403 TUBE.
- [SDR R61A201403020351](https://openairdocs.org/sdr/R61A201403020351), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, RT WING FUEL PANEL 621AB HAS FUEL TUBE CORRODED. MX R & R FUEL TUBE IAW AMM 20-10-03.
- [SDR R61A201403020350](https://openairdocs.org/sdr/R61A201403020350), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, RT WING FUEL TUBE INSIDE PANEL 621EB FOUND CORRODED. MX R & R RT WING FUEL TUBE INSIDE PANEL IAW AMM 20-10-03.
- [SDR R61A201403020349](https://openairdocs.org/sdr/R61A201403020349), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, RT WING FUEL TUBE INSIDE PANEL 621BB IS CORRODED. MX R & R RT WING FUEL TUBE INSIDE PANEL 621BB IAW AMM 20-10-13.
- [SDR R61A201403020348](https://openairdocs.org/sdr/R61A201403020348), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, RT WING, THREE FUEL TUBES INSIDE FUEL PANEL 631AB ARE CORRODED. MX R & R RT WING 3 EACH, FUEL TUBES INSIDE FUEL PANEL 631AB IAW AMM 20-10-13
- [SDR R61A201403020347](https://openairdocs.org/sdr/R61A201403020347), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LT WING 3 FUEL TUBES CLAMPS INSIDE PANEL 521AB HAVE CORROSION. MX R & R LT WING 3 FUEL TUBES CLAMPS INSIDE PANEL 521AB IAW AMM 20-10-13, R &
- [SDR R61A201403020346](https://openairdocs.org/sdr/R61A201403020346), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LT WING 4 FUEL TUBES CLAMPS INSIDE PANEL 521BB HAVE CORROSION. MX R & R LT WING 4 FUEL TUBES CLAMPS INSIDE PANEL 521BB IAW AMM 20-10-13, R &
- [SDR R61A201403020345](https://openairdocs.org/sdr/R61A201403020345), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LT WING PANEL 521DB 5 FUEL TUBE CLAMPS HAVE CORROSION. MAINTENANCE R & R LT WING PANEL 521DB 5 FUEL TUBE CLAMPS IAW AMM 170 20-10-13. R & R 
- [SDR R61A201403020344](https://openairdocs.org/sdr/R61A201403020344), Mar 2, 2014: TUBE. CORRODED. DURING HEAVY CHECK, LT WING FUEL TUBE AND CLAMP LOCATED FUEL PANEL 521EB HAVE CORROSION. MAINTENANCE R & R LT WING FUEL TUBE AND CLAMP IAW AMM 20-10-13. R & R C
- [SDR R61A201403020343](https://openairdocs.org/sdr/R61A201403020343), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LT WING FUEL PANEL 531AB, FUEL TUBE CLAMP HAVE CORROSION. MX R & R LT WING FUEL PANEL 531AB FUEL TUBE CLAMP IAW AMM 20-10-13. R & R CONNECTI
- [SDR R61A201403020342](https://openairdocs.org/sdr/R61A201403020342), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LEFT WING FUEL TUBE CLAMP UNDER WING PANEL 531BB IS CORRODED. MX R & R CLAMP IAW AMM 20-10-13.
- [SDR R61A201403020341](https://openairdocs.org/sdr/R61A201403020341), Mar 2, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, LT WING FUEL TUBE CLAMP UNDER PANEL 531EB IS CORRODED. MX R & R LT WING FUEL TUBE CLAMP UNDER PANEL 531EB IAW AMM 20-10-13. PN 14C16-24A, CL
- [SDR R61A201403010340](https://openairdocs.org/sdr/R61A201403010340), Mar 1, 2014: RIB. CRACKED. DURING HEAVY CHECK, FWD FLANGE ON RT HORIZONTAL STABILIZER, RIB 11A IS CRACKED AT LAST RIVET. MX REPAIRED CRACKED RIB 11A FWD LOWER FLANGE IAW ETD 2014-170-0177
- [SDR R61A201402280354](https://openairdocs.org/sdr/R61A201402280354), Feb 28, 2014: BOLT. CORRODED. DURING HEAVY CHECK WAS REPORTED THAT L1 DOOR STOPS HARDWARE IS CORRODED. MX R & R L1 DOOR STOPS HARDWARE IAW AMM 52-11-23. PN PE20194-4010A, BOLT.
- [SDR R61A201402270352](https://openairdocs.org/sdr/R61A201402270352), Feb 27, 2014: RIB. CRACKED. DURING HEAVY CHECK, LT HORIZONTAL STAB L/E SECOND AND THIRD INBD RIBS HAVE CRACKS. MX REWORKED LT HORIZONTAL STAB L/E RIBS IAW ETD 2014-170-015280.
- [SDR R61A201402270335](https://openairdocs.org/sdr/R61A201402270335), Feb 27, 2014: BRACKET. CRACKED. DURING HEAVY CHECK, STEERING MANIFOLD BRACKET IN NLG WELL IS CRACKED. MX R & R STEERING MANIFOLD BRACKET IN NLG WELL IAW SRM 51-40-02,51-43-03,
- [SDR R61A201402270353](https://openairdocs.org/sdr/R61A201402270353), Feb 14, 2014: BEAM. CORRODED. DURING HEAVY CHECK FOUND A SPLIT BEAM ON BACK SIDE OF AFT GALLEY ALONG COUNTER HAS CORROSION. R & R ALL CORRODED TRIM PIECES ON BOTH SECTIONS OF AFT GALLEY WHER
- [SDR R61A201312251352](https://openairdocs.org/sdr/R61A201312251352), Dec 25, 2013: FLASHLIGHT. INOPERATIVE. CAPTAIN'S COCKPIT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR R61A201312061302](https://openairdocs.org/sdr/R61A201312061302), Dec 6, 2013: SLIDE. OUT OF ADJUST. L1 DOOR JAMMED AND SLIDE LEVER WOULD NOT DISARM. ADJUSTED THE DOOR SLIDE AND IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201309240914](https://openairdocs.org/sdr/R61A201309240914), Sep 24, 2013: MECHANISM. LACK OF LUBE. CREW REPORTED THAT THE L1 DOOR WAS HARD TO OPEN. MX LUBED THE L1 DOOR LOCKING MECHANISM IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201309060845](https://openairdocs.org/sdr/R61A201309060845), Sep 6, 2013: DEFLECTOR. DAMAGED. CREW REPORTED A LOUD BUZZING COMING FROM THE RT SIDE OF THE ACFT, POSSIBLY FROM THE R1 DOOR. CREW STATEED IT STARTED AT ABOUT 5 PSI AND STOPPED AROUND 4.5 PSI. 
- [SDR R61A201309050841](https://openairdocs.org/sdr/R61A201309050841), Sep 5, 2013: DOOR. OUT OF ADJUST. CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO OPEN. MX ADJUSTED AND LUBRICATED DOOR IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201309050840](https://openairdocs.org/sdr/R61A201309050840), Sep 5, 2013: DOOR. UNKNOWN. CREW REPORTED THAT THE R1 DOOR IS MAKING NOISE IN FLIGHT. AN EMERGENCY WAS NOT DECLARED AND CREW LANED WITHOUT INCIDENT. MX INSPECTED DEFLECTOR AND PERFORMED PR
- [SDR R61A201309030835](https://openairdocs.org/sdr/R61A201309030835), Sep 3, 2013: SEAL. NOISY. CREW REPORTED THAT THE R1 DOOR SEAL HUMS IN FLIGHT. MX INSPECTED DOOR SEAL AND UPPER DOOR DEFLECTOR IAW AMM AND PERFORMED GVI ON DOOR AND NO DEFECTS WERE NOTED.
- [SDR R61A201309010829](https://openairdocs.org/sdr/R61A201309010829), Sep 1, 2013: SEAL. DIRTY. CREW REPORTED A LOUD NOISE WAS COMING FROM THE R1 DOOR DURING CLIMB AND DESCENT. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MX INSPECTED AN
- [SDR R61A201308240774](https://openairdocs.org/sdr/R61A201308240774), Aug 24, 2013: SEAL. DIRTY. CREW REPORTED THAT THE R1 DOOR WAS MAKING A LOUD BUZZING NOSE IN FLIGHT. MX CLEANED DOOR SEAL AND FRAME IAW AMM AND DEFECTS WERE NOTED. ACFT OK FOR SERVICE.

All 108: https://openairdocs.org/deregistered/N801MA-2017-06-02/reports.md

## FAA accident and incident reports (1)

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 20070206001559I](https://openairdocs.org/incident/20070206001559I), Feb 6, 2007: Emb ERJ170100SU (N801MA), Portland, ME. (-23) This office notified by new england region operations center that republic 3360, E170 inbound to Portland, Maine reported a problem with the slats. Pilot…

## Other aircraft with N801MA

- [Cancelled 2000-12-05](https://openairdocs.org/deregistered/N801MA-2000-12-05): Smith AEROSTAR 600, S/N 60-0433-147. Exported to Namibia. Owner: [Wayne, PA](https://openairdocs.org/faa-place/PA/Wayne)

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