# N804MD: 2004 Embraer ERJ 170-100SU, registration cancelled 2017-07-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 18, 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: 17000016
- 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 12, 2004
- Last registry action: June 22, 2016
- Mode S code: AAF1D0
- 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/N804MD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=804MD
- Page: https://openairdocs.org/deregistered/N804MD-2017-07-18

From the FAA registry file of October 28, 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 (114, newest 50)

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

- [SDR R61A201604180254](https://openairdocs.org/sdr/R61A201604180254), Apr 18, 2016: CONNECTOR. UNSECURE. CREW REPORTED THAT THE COCKPIT TO CABIN AND EMERGENCY RAINBOW LIGHTS WERE NOT TESTING. SECURED CONNECTOR P0551 IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201603090179](https://openairdocs.org/sdr/R61A201603090179), Mar 9, 2016: WINDSHIELD. FAILED. CREW REPORTED THAT THE F/O WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND CREW DIVERTED, WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE R & R F/O`S WINDSH
- [SDR R61A201504040228](https://openairdocs.org/sdr/R61A201504040228), Apr 4, 2015: LIGHT. DETACHED. CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP WAS DETACHED AT ROW 16. MAINTENANCE RESECURED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201502080082](https://openairdocs.org/sdr/R61A201502080082), Feb 8, 2015: BUTTON. MISSING. MAINTENANCE REPORTED THAT THE VOLUME CONTROL BUTTON ON THE MEGAPHONE WAS MISSING. MAINTENANCE R & R MEGAPHONE IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201501190041](https://openairdocs.org/sdr/R61A201501190041), Jan 19, 2015: BRACKET. CRACKED. DURING HEAVY CHECK, LT BRACKET IS CRACKED. MAINTENANCE REMOVED CRACKED BRACKET FABRICATED NEW BRACKET, MATCH DRILLED REPLACEMENT PARTS, ALL WORK PERFORMED IAW E
- [SDR R61A201501120038](https://openairdocs.org/sdr/R61A201501120038), Jan 12, 2015: TORQUE TUBE. CORRODED. DURING HEAVY CHECK, LT WING FLAP TORQUE TUBE F6 HAS CORRODED ON MALE END. MAINTENANCE R & R LT WING FLAP TORQUE TUBE F6 IAW AMM 27-51-03, PN 5912949-3, TORQUE T
- [SDR R61A201501120037](https://openairdocs.org/sdr/R61A201501120037), Jan 12, 2015: SUPPORT. CORRODED. DURING HEAVY CHECK RT WING FLAP 5-6 TORQUE TUBES BEARINGS SUPPORT HAVE CORROSION. MAINTENANCE R & R RT WING FLAP 5-6 TORQUE TUBES BEARINGS SUPPORT IAW AMM 27-51
- [SDR R61A201501110042](https://openairdocs.org/sdr/R61A201501110042), Jan 11, 2015: ANGLE. CRACKED. DURING HEAVY CHECK, APU RT BULKHEAD 351BZ INBD ANGLE BOTTOM CORNER IS CRACKED. MAINTENANCE REPAIRED CRACK IAW SRM 53-31-21, FIG 202.
- [SDR R61A201501110036](https://openairdocs.org/sdr/R61A201501110036), Jan 11, 2015: NUT. CORRODED. DURING HEAVY CHECK, R1 DOOR NUT ON STOP BELLCRANKS IS CORRODED. MAINTENANCE R & R R1 DOOR NUT ON STOP BELL CRANKS IAW AMM 52-41-20. PN AN316-4R, NUT.
- [SDR R61A201501110034](https://openairdocs.org/sdr/R61A201501110034), Jan 11, 2015: BULKHEAD. CRACKED. DURING A HEAVY CHECK, THE LT MLG WHEEL WELL FWD BULKHEAD CRACKED VERTICALLY ALONG UPPER RADIUS, 6" FROM OTBD EDGE. MX R & R FWD BULKHEAD IAW SRM 51-41-01 AND ET
- [SDR R61A201501100035](https://openairdocs.org/sdr/R61A201501100035), Jan 10, 2015: SUPPORT. CRACKED. DURING HEAVY CHECK, RIB SUPPORT ANGLE AT LT WHEEL WELL FWD BULKHEAD HAS CRACK RADIATING FROM BOTH DIRECTIONS FROM OTBD FASTENER. MAINTENANCE R & R RIB SUPPORT A
- [SDR R61A201412071229](https://openairdocs.org/sdr/R61A201412071229), Dec 7, 2014: LIGHT. UNSECURE. MAINTENANCE REPORTED THAT PART OF THE EMERGENCY LIGHT STRIP AT SEAT 4C WAS LOOSE. MAINTENANCE SECURED THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201411121172](https://openairdocs.org/sdr/R61A201411121172), Nov 12, 2014: LIGHT. INOPERATIVE. CREW REPORTED THAT THREE EMERGENCY LIGHTS IN THE FWD CABIN WERE NOT FULLY ILLUMINATING. MAINTENANCE R & R IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE
- [SDR R61A201409011023](https://openairdocs.org/sdr/R61A201409011023), Sep 1, 2014: LIGHT. LOOSE. CREW REPORTED THAT THE EMERGENCY LIGHT AT SEAT 2A OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED EMERGENCY LIGHTIAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201408301024](https://openairdocs.org/sdr/R61A201408301024), Aug 30, 2014: BATTERY PACK. INOPERATIVE. CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201407060853](https://openairdocs.org/sdr/R61A201407060853), Jul 6, 2014: ACTUATOR. FAILED. CREW RECEIVED A FLAP FAIL MESSAGE. DIVERTED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE R & R FLAP ACTUATOR IAW AMM AND OPS CHECKED GOOD. AC
- [SDR R61A201407060852](https://openairdocs.org/sdr/R61A201407060852), Jul 6, 2014: ACTUATOR. FAILED. CREW SELECTED FLAPS 3 AND RECEIVED A FLAPS FAIL MESSAGE. CREW DISCONTINUED APPROACH TO RUN THE QRH WITH NO SUCCESS. CREW DECLARED AN EMERGENCY AND LANDED WITHOU
- [SDR R61A201404180553](https://openairdocs.org/sdr/R61A201404180553), Apr 18, 2014: LIGHT. LOOSE. CREW REPORTED THAT THE EMEGENCY LIGHT AT ROW 10 WAS LOOSE. MAINTENANCE SECURED THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
- [SDR R61A201404090513](https://openairdocs.org/sdr/R61A201404090513), Apr 9, 2014: SHEAR TIE. DAMAGED. DURING HEAVY CHECK, DAMAGE ON SHEAR CLIP FRAME 88 BETWEEN STRINGERS 26-27R. MX R & R SHEAR CLIP IAW SRM 51-40-02, 51-41-01.
- [SDR R61A201404090503](https://openairdocs.org/sdr/R61A201404090503), Apr 9, 2014: SHEAR TIE. DAMAGED. DURING HEAVY CHECK, DAMAGE FOUND ON SHEAR TIE FRAME 88 BETWEEN STRINGERS 26-27R. MX R & R SHEAR TIE IAW SRM 51-40-02, 51-41-01. MAJOR REPAIR
- [SDR R61A201404070523](https://openairdocs.org/sdr/R61A201404070523), Apr 7, 2014: ANGLE. CORRODED. DURING HEAVY CHECK, FLOORBEAM AT FRAME 17 RT SIDE CORRODED. MX R & R FLOORBEAM FRAME 17 IAW SRM 51-41-01.
- [SDR R61A201404070520](https://openairdocs.org/sdr/R61A201404070520), Apr 7, 2014: SHEAR WEB. CORRODED. DURING HEAVY CHECK, CORROSION WAS FOUND ON THE SHEAR WEB AT FRAME 19, LT SIDE. MAINTENANCE R & R THE SHEAR WEB IAW SRM 51-43-02 & 51-41-02.
- [SDR R61A201404060508](https://openairdocs.org/sdr/R61A201404060508), Apr 6, 2014: BOLT. CORRODED. DURING HEAVY CHECK, FWD CARGO LT & RT CENTER DOOR FITTING HARDWARE CORRODED. MAINTENANCE R & R FWD CARGO LT, RT CENTER DOOR FITTINGS HARDWARE IAW AMM 53-21-29, 
- [SDR R61A201404050519](https://openairdocs.org/sdr/R61A201404050519), Apr 5, 2014: RIVET. CORRODED. DURING HEAVY CHECK, CORROSION WAS FOUND ON RIVETS OF THE WASTE BOX DOUBLER FORWARD SIDE. MAINTENANCE R & R RIVETS IAW ETD 2014-170-028885 AND SRM 51-41-02.
- [SDR R61A201404010510](https://openairdocs.org/sdr/R61A201404010510), Apr 4, 2014: RIB. CRACKED. DURING HEAVY CHECK, RT HORIZONTAL STAB AFT OF FWD SPAR, RIB 11 FWD LOWER FLANGE IS CRACKED. MX TRIMMED DAMAGE OUT ON RT HORIZONTAL STAB AFT OF FWD SPAR RIB FWD 
- [SDR R61A201404030518](https://openairdocs.org/sdr/R61A201404030518), Apr 3, 2014: SHEAR TIE. CRACKED. DURING HEAVY CHECK, MAINTENANCE REPORTED A CRACK ON THE VERTICAL STAB T/E SHEAR TIE LOCATED BETWEEN RIBS 9 & 10 ON THE RT SIDE AT FORWAD FLANGE AFT END AND AFT 
- [SDR R61A201404030507](https://openairdocs.org/sdr/R61A201404030507), Apr 3, 2014: SEAL DEPRESSOR. DAMAGED. DURING HEAVY CHECK, L1 DOOR FWD CUT OUT SEAL DEPRESSOR AREA OF THICKNESS REDUCTION DAMAGE. MAINTENANCE R & R L1 DOOR FWD CUT OUT SEAL DEPRESSOR SRM 51-40-02, 51
- [SDR R61A201404030497](https://openairdocs.org/sdr/R61A201404030497), Apr 3, 2014: SEAL DEPRESSOR. DAMAGED. DURING HEAVY CHECK, L1 DOOR CUTOUT FWD SEAL DEPRESSOR ONE AREA OF THICKNESS REDUCTION DAMAGE. MX MEASURED DAMAGE AND DETERMINED THAT IT IS UNSERVICABLE IAW SRM 
- [SDR R61A201404030494](https://openairdocs.org/sdr/R61A201404030494), Apr 3, 2014: DOOR SILL. CORRODED. DURING HEAVY CHECK, FWD CARGO LOWER DOOR SILL HAS 5 NUTPLATES STAND OFF BRACKETS CORRODED WITH 1 CRACKED, 1 DENTED. MAINTENANCE R & R FWD CARGO LOWER SILL HAS 5
- [SDR R61A201404020522](https://openairdocs.org/sdr/R61A201404020522), Apr 2, 2014: FIREWALL. CRACKED. RT APU FIRWALL IS CRACKED. MX REMOVED CRACKED AREAS AT THE UPPER AND LOWER INBD RADIUS IAW ETD 2014-170-030302.
- [SDR R61A201404020516](https://openairdocs.org/sdr/R61A201404020516), Apr 2, 2014: DOOR. CORRODED. DURING HEAVY CHECK, LAVATORY WASTE DUMP DOOR BY HINGE IS CORRODED. MX R & R LAV WASTE DUMP DOOR IAW AMM 21-10-01, SRM 51-40-00, PN 170-86668-403 SERVICE PANEL.
- [SDR R61A201404020511](https://openairdocs.org/sdr/R61A201404020511), Apr 2, 2014: THRESHOLD. CORRODED. DURING HEAVY CHECK, R2 DOOR THRESHOLD BETWEEN FRAMES 85-87 AT GIRT BAR FITTING IS CORRODED. MAINTENANCE REMOVED CORROSION IAW ETD 2014-170-028504.
- [SDR R61A201404020505](https://openairdocs.org/sdr/R61A201404020505), Apr 2, 2014: THRESHOLD. CORRODED. DURING HEAVY CHECK, L2 DOOR THRESHOLD BETWEEN FRAMES 85-87 AT GIRT BAR FITTINGS IS CORRODED. MAINTENANCE R & R L2 DOOR THRESHOLD BETWEEN FRAMES 85-87 AT GIRTBAR
- [SDR R61A201404020504](https://openairdocs.org/sdr/R61A201404020504), Apr 2, 2014: GIRT BAR. CORRODED. DURING HEAVY CHECK, SPLICE BAR INBD OF FWD L2 DOOR GIRT BAR FITTING AFT OF FRAME 5 CORRODED. MX R & R SPLICE BAR IAW SRM 51-40-02, 51-43-03.
- [SDR R61A201404020502](https://openairdocs.org/sdr/R61A201404020502), Apr 2, 2014: RIB. GOUGED. DURING HEAVY CHECK, TWO GOUGES ON TOP OF VERTICAL STAB RIB 14. MAINTENANCE R & R VERTICAL STAB RIB 14 IAW SRM 51-41-02, 51-42-01, 51-42-02. MAJOR REPAIR
- [SDR R61A201404020496](https://openairdocs.org/sdr/R61A201404020496), Apr 2, 2014: ATTACH BRACKET. CRACKED. DURING HEAVY CHECK, FLOORBOARD CLIP NUT ATTACH BRACKET BETWEEN LT CENTER FLOORBEAM AND L2 DOOR THRESHOLD AT FRAME 85 IS CRACKED. MAINTENANCE R & R FLOORBOARD CL
- [SDR R61A201404020495](https://openairdocs.org/sdr/R61A201404020495), Apr 2, 2014: BOLT. CORRODED. DURING HEAVY CHECK, AFT SERVICE DOOR STOP FITTINGS MOUNT HARDWARE STOP FITTINGS ARE CORRODED. MAINTENANCE R & R AFT SERVICE DOOR STOP FITTINGS MOUNT HARDWARE IA
- [SDR R61A201404020493](https://openairdocs.org/sdr/R61A201404020493), Apr 2, 2014: STOP FITTING. CORRODED. DURING HEAVY CHECK, AFT SERVICE DOOR STOP FITTING, DOOR STOP LOCKNUT ON 3 FITTINGS 1, 2, 4 IS CORRODED. MX R & R AFT SERVICE DOOR STOP FITTING DOOR STOP LOCKNUT
- [SDR R61A201404020476](https://openairdocs.org/sdr/R61A201404020476), Apr 2, 2014: NUT PLATE. LOOSE. DURING HEAVY CHECK, FWD CARGO DOOR SCUFF PLATE HAS NUMEROUS NUT PLATES THAT ARE LOOSE AND ONE NUTPLATE NEEDED TO BE REPLACED BOTTOM OF SCUFF PLATE BETWEEN FRAME
- [SDR R61A201404010512](https://openairdocs.org/sdr/R61A201404010512), Apr 1, 2014: SUPPORT. CORRODED. DURING HEAVY CHECK, LT WING FLAP TRACK SUPPORT 2, 3, 4 FWD ATTACH POINTS HARDWARE IS CORRODED. MX R & R LT WING FLAP TRACK SUPPORT 2, 3, 4 FWD ATTACH POINTS HAR
- [SDR R61A201404010509](https://openairdocs.org/sdr/R61A201404010509), Apr 1, 2014: RIB. CRACKED. DURING HEAVY CHECK, LT HORIZONTAL STAB AFT OF FWD SPAR RIB 11 CRACKED ON FWD UPPER FLANGE AT AFT END. MAINTENANCE REPAIRED LT HORIZONTAL STAB RIB 11 IAW ETD2014
- [SDR R61A201404010492](https://openairdocs.org/sdr/R61A201404010492), Apr 1, 2014: RIB. CRACKED. DURING HEAVY CHECK, RT HORIZONTAL STAB AFT OF FWD SPAR RIB 12 FWD UPPER FLANGE AFT END IS CRACKED. MX PERFORMED PERMANENT REPAIR RT HORIZONTAL STAB AFT OF FWD S
- [SDR R61A201403310514](https://openairdocs.org/sdr/R61A201403310514), Mar 31, 2014: CHANNEL. CRACKED. DURING HEAVY CHECK, VERTICLE STABILIZER L/E RT LOWER GANG CHANNEL IS CRACKED. MX R & R CHANNEL IAW SRM 51-41-02.
- [SDR R61A201403310506](https://openairdocs.org/sdr/R61A201403310506), Mar 31, 2014: STRUCTURE. CORRODED. DURING HEAVY CHECK, AFT GALLEY ON FRONT EDGE AROUND COFFEEMAKER IS CORRODED. MX R & R ALL CORRODED PIECES ON FRONT EDGE AROUND COFFEEMAKER IN AFT GALLEY IAW AMM
- [SDR R61A201403300515](https://openairdocs.org/sdr/R61A201403300515), Mar 30, 2014: SUPPORT BRACKET. CRACKED. DURING HEAVY CHECK, RT RAM AIR DUCT SUPPORT BRACKET IS CRACKED. MX R & R RT RAM AIR DUCT SUPPORT BRACKET IAW SRM 51-40-00, PN 171-06435-401, SUPPORT BRACKET.
- [SDR R61A201401030026](https://openairdocs.org/sdr/R61A201401030026), Jan 3, 2014: DOOR. STUCK. MAIN CABIN DOOR STUCK AND WOULD NOT OPEN. UNBOUND L1 DOOR, OPS CHECKED OK IAW AMM 52-11-00.
- [SDR R61A201311211231](https://openairdocs.org/sdr/R61A201311211231), Nov 21, 2013: FLASHLIGHT. INOPERATIVE. CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FORWARD F/A FLASHLIGHT IAW AMM. OPS CHECKED GOOD.
- [SDR R61A201309230908](https://openairdocs.org/sdr/R61A201309230908), Sep 23, 2013: SMOKE DETECTOR. DEFECTIVE. CREW RECEIVED A SMOKE MESSAGE IN FLIGHT. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MX FOUND THREE HITS ON THE CMC FOR THE SMOKE DETECTOR DURING
- [SDR R61A201305070450](https://openairdocs.org/sdr/R61A201305070450), May 7, 2013: SEAL. DIRTY. CREW REPORTED HEARING A HISSING NOISE COMING FROM THE L2 DOOR DURING DESCENT BELOW 10,000 FEET. CREW DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. M
- [SDR R61A201304300439](https://openairdocs.org/sdr/R61A201304300439), Apr 30, 2013: INDICATOR. OBSTRUCTED. CREW REPORTED THAT THE L2 DOOR LATCH INDICATOR IS INOPERATIVE. MAINTENANCE REMOVED DEBRIS FROM LATCH INDICATOR PER EMB AMM AND OPS CHECKED GOOD.

All 114: https://openairdocs.org/deregistered/N804MD-2017-07-18/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 20050815017589I](https://openairdocs.org/incident/20050815017589I), Aug 15, 2005: Emb ERJ170100SU (N804MD), Houston, TX, Minor damage. (-23) The captain stated that "upon landing, the aircraft started shaking severely. At that point I noticed the parking brake handle not fully down and then…

## Other aircraft with N804MD

- [Registered now](https://openairdocs.org/aircraft/N804MD): Cirrus Design SF50, S/N 0715, built 2025

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