# N807MD: 2004 Embraer ERJ 170-100SU, registration cancelled 2021-05-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 8, 2021 - Status when cancelled: Registration expired, pending cancellation - 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: 17000020 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 28, 2004 - Certificate issued: January 4, 2018 - Last registry action: January 4, 2018 - Mode S code: AAFCF5 - Owner when cancelled: [Aar Supply Chain Inc](https://openairdocs.org/faa-owner/AAR%20SUPPLY%20CHAIN%20INC) - Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale) - Owner type: Corporation - Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N807MD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807MD - Page: https://openairdocs.org/deregistered/N807MD-2021-05-08 From the FAA registry file of November 3, 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 (78, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR R61A201603190203](https://openairdocs.org/sdr/R61A201603190203), Mar 19, 2016: LIGHT. LOOSE. CREW REPORTED THAT A PIECE OF EMERGENCY LIGHT STRIP IN THE FWD CABIN CAME OFF THE FLOOR. MAINTENANCE SECURED THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201601020014](https://openairdocs.org/sdr/R61A201601020014), Jan 2, 2016: LIGHT. LOOSE. CREW REPORTED THAT A SMALL SECTION OF EMERGENCY LIGHT STRIP IN THE FORWARD GALLEY WAS LOOSE. MAINTENANCE RESECURED EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED - [SDR R61A201512160935](https://openairdocs.org/sdr/R61A201512160935), Dec 16, 2015: LIGHT. INOPERATIVE. CREW REPORTED THAT THE ENTRY EMERGENCY LIGHT STRIP WAS WORN AND INOPERATIVE. MAINTENANCE R & R THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201511090793](https://openairdocs.org/sdr/R61A201511090793), Nov 9, 2015: HANDLE. BROKEN. CREW REPORTED THAT THE MEGAPHONE HANDLE WAS BROKEN. MAINTENANCE R & R MEGAPHONE IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201509020597](https://openairdocs.org/sdr/R61A201509020597), Sep 2, 2015: FLASHLIGHT. BROKEN. CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT MOUNT WAS BROKEN. MAINTENANCE R & R FORWARD F/A FLASHLIGHT ASSY AND HOLDER IAW AMM. OPS CHECKED GOOD. - [SDR R61A201503130215](https://openairdocs.org/sdr/R61A201503130215), Mar 13, 2015: ATTACH FITTING. CORRODED. DURING HEAVY CHECK, AFT BELLY PANEL 195NL FWD ATTACH CENTER ATTACH STRIP IS CORRODED. MX R & R AFT BELLY PANEL, 195NL FWD ATTACH CENTER ATTACH STRIP IAW AMM 53- - [SDR R61A201503120219](https://openairdocs.org/sdr/R61A201503120219), Mar 12, 2015: UPPER SHEET. CORRODED. DURING HEAVY CHECK, LT UPPER SHEET AT FRAME 85-86 IS CORRODED. MAINTENANCE R & R LT UPPER SHEET AT FRAME 85-86 IAW SRM 51-43-07, 51-41-01. - [SDR R61A201503120218](https://openairdocs.org/sdr/R61A201503120218), Mar 12, 2015: FLOOR SUPPORT. CORRODED. DURING HEAVY CHECK, LT PANEL SUPPORT FRAME 88-90 IS CORRODED. MAINTENANCE R & R LT PANEL SUPPORT FRAME 88-90 IAW SRM 51-41-01, 51-42-01, 51-43-03. - [SDR R61A201503120217](https://openairdocs.org/sdr/R61A201503120217), Mar 12, 2015: GUSSET. CORRODED. DURING HEAVY CHECK, CENTER GUSSET AT FRAME 90 IS CORRODED. MAINTENANCE R & R CENTER GUSSET AT FRAME 90 IAW SRM 51-43-90. - [SDR R61A201503120216](https://openairdocs.org/sdr/R61A201503120216), Mar 12, 2015: GUSSET. CORRODED. DURING HEAVY CHECK, RT FRAME 91, Y10.78 GUSSET IS CORRODED. MAINTENANCE R & R RT FRAME 91, Y10.78 GUSSET IAW SRM 51-41-02. - [SDR R61A201503120197](https://openairdocs.org/sdr/R61A201503120197), Mar 12, 2015: SPLICE PLATE. CORRODED. DURING HEAVY CHECK, SPLICE PLATE RT SHEAR PLATE AT FRAMES 87-88. MAINTENANCE R & R SPLICE PLATE RT SHEAR PLATE AT FR 88/87 IAW SRM 51-21-02, 51-40-02, PN 170-65 - [SDR R61A201503120195](https://openairdocs.org/sdr/R61A201503120195), Mar 12, 2015: GUSSET. CORRODED. DURING HEAVY CHECK LT GUSSET AT FRAME 91 IS CORRODED. MAINTENANCE R & R LT GUSSET AT FRAME 91 IAW SRM 51-41-02. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED. - [SDR R61A201503120194](https://openairdocs.org/sdr/R61A201503120194), Mar 12, 2015: UPPER SHEET. CORRODED. DURING HEAVY CHECK, RT UPPER SHEET AT FRAME 85-86 IS CORRODED. MAINTENANCE R & R RT UPPER SHEET AT FRAME 85-86 IAW 51-43-03, 51-41-01. AIRCRAFT REMAINS UNTIL HE - [SDR R61A201503110231](https://openairdocs.org/sdr/R61A201503110231), Mar 11, 2015: STRINGER. CORRODED. DURING HEAVY CHECK, STRINGER 27R AT FRAME 88 IS CORRODED. MX R & R STRINGER 27R AT FRAME 88 IAW ETD 2015--170--027169, REV A. ACFT REMAINS UNTIL HEAVY CHECK IS - [SDR R61A201503110204](https://openairdocs.org/sdr/R61A201503110204), Mar 11, 2015: CLOSEOUT PANEL. CORRODED. WHILE IN HEAVY CHECK WAS REPORTED THAT AFT CARGO DOOR THRESHOLD CLOSE OUT PANEL IS CORRODED. MAINTENANCE R & R AFT CARGO DOOR THRESHOLD CLOSE OUT PANEL IAW SRM - [SDR R61A201503110203](https://openairdocs.org/sdr/R61A201503110203), Mar 11, 2015: SEAT TRACK. CORRODED. DURING HEAVY CHECK, LT FWD SEAT TRACK FRAME 12/20 AT FRAME 17 HAS CORROSSION. MAINTENANCE R & R LT SEAT TRACK FRAME 12/20 AT FRAME 17 IAW SRM 51-40-01, 51-41-03 - [SDR R61A201503110202](https://openairdocs.org/sdr/R61A201503110202), Mar 11, 2015: BRACKET. CORRODED. DURING HEAVY CHECK, WING TO FUSELAGE FAIRING ATTACH BRACKET AIR FRAME SIDE WHERE FAIRING 191FL IS CORRODED. MAINTENANCE R & R 4 EACH ATTACH FAIRING BRACKETS IAW - [SDR R61A201503110196](https://openairdocs.org/sdr/R61A201503110196), Mar 11, 2015: GUSSET. CORRODED. DURING HEAVY CHECK, CENTER STRESS PANEL AT GALLEY MOUNTHOLE BETWEEN FRAME 87-88 IS CORRODED. MAINTENANCE R & R SHEAR PANEL, PN 170-65928-001, GUSSET. AIRCRAFT R - [SDR R61A201501020007](https://openairdocs.org/sdr/R61A201501020007), Jan 2, 2015: LIGHT. INOPERATIVE. CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT ROW 1 WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY LIGHT STRIP AT ROW 1 IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201412201249](https://openairdocs.org/sdr/R61A201412201249), Dec 20, 2014: WARNING MESSAGE. FALSE ACTIVATION. AFTER SELECTING FLAPS FROM 2 TO 3 CREW RECEIVED A FLAPS FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTE - [SDR R61A201405290731](https://openairdocs.org/sdr/R61A201405290731), May 29, 2014: STIFFENER. CRACKED. DURING HEAVY CHECK, RT PYLON STIFFENER ON OTBD SIDE CRACKED, MX R & R STIFFENER IAW SRM 51-43-02, 51-41-02. - [SDR R61A201405280736](https://openairdocs.org/sdr/R61A201405280736), May 28, 2014: STRUCTURE. CORRODED. DURING HEAVY CHECK, AREA BETWEEN FWD AND AFT SECTION OF GALLEY HAS CORROSION. MX R & R ALL CORRODED PIECES ON AFT GALLEY WHERE 2 HALVES MEET IAW AMM 25-00-23, 2 - [SDR R61A201405270732](https://openairdocs.org/sdr/R61A201405270732), May 27, 2014: DOOR FRAME. GOUGED. DURING HEAVY CHECK, FWD SERVICE DOOR AFT OF FRAME 17 AFT DOOR FRAME GOUGED. MAINTENANCE R & R IAW SRM 51-41-02. - [SDR R61A201405270725](https://openairdocs.org/sdr/R61A201405270725), May 27, 2014: LEAF SPRING. CORRODED. DURING HEAVY CHECK LEAF SPRING AND NUT R1 DOOR NR 4 FWD STOP FITTING AND NUT NR 3 FWD STOP FITTING ARE CORRODED. MX R & R LEAF SPRING AND NUT R1 DOOR NR 4 FWD S - [SDR R61A201405270724](https://openairdocs.org/sdr/R61A201405270724), May 27, 2014: NUT. CORRODED. DURING HEAVY CHECK, L1 DOOR STOP SCREW NUT ON DOOR STOP FITTINGS NR 3, & 4 SHOW SIGNS OF CORROSION. MX R & R L1 DOOR STOP SCREW NUT ON DOOR STOP FITTING IAW AMM - [SDR R61A201405270710](https://openairdocs.org/sdr/R61A201405270710), May 27, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, FOUND BETWEEN RIBS 1 AND 2 LT AND RT HORIZONAL STAB THERE ARE SEVERAL HARNESS ADEL CLAMPS AND HARDWARE CORRODED. MX R & R ADEL CLAMPS AND HA - [SDR R61A201405270708](https://openairdocs.org/sdr/R61A201405270708), May 27, 2014: SPRING. CORRODED. DURING HEAVY CHECK, FOUND LEAF SPRING AND NUT AT NR 3 AND 4 FWD STOP FITTING ON R1 DOOR CORRODED. MX R & R LEAF SPRINGS IAW AMM 52-11-23. - [SDR R61A201405270707](https://openairdocs.org/sdr/R61A201405270707), May 27, 2014: STOP. CORRODED. DURING HEAVY CHECK, FOUND THE LOWEST TWO DOOR STOPS ON FWD SERVICE DOOR FWD EDGE CORRODED. MAINTENANCE R & R DOOR STOPS HARDWARE IAW AMM 52-41-23. - [SDR R61A201405270706](https://openairdocs.org/sdr/R61A201405270706), May 27, 2014: CLAMP. CORRODED. DURING HEAVY CHECK, FOUND CORROSION BETWEEN HORZIONAL STAB LT AND RT RIBS 1 & 2 THERE ARE SEVERAL HYDRAULIC LINE CLAMPS AND HARDWARE CORRODED. MAINTENANCE R & R - [SDR R61A201405260734](https://openairdocs.org/sdr/R61A201405260734), May 26, 2014: PANEL. CRACKED. DURING HEAVY CHECK, PANEL 351BZ CORNERS ARE CRACKED. MAINTENANCE TRIMED OUT DAMAGE WITH NO REINENFORCEMENT INSTALLATION ON PANEL 351BZ, HFEC NO CRACKS NOTED IAW - [SDR R61A201405260733](https://openairdocs.org/sdr/R61A201405260733), May 26, 2014: SUPPORT. CORRODED. DURING HEAVY CHECK, LT WING NR 3 MIDDLE FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE IS CORRODED. MX R & R LT WING 3 MIDDLE FLAP TRACK SUPPORT FWD ATTACHM - [SDR R61A201405260731](https://openairdocs.org/sdr/R61A201405260731), May 26, 2014: BOLT. CORRODED. DURING HEAVY CHECK, RT WING SPOILER ACTUATORS NR 4, & 5 INBD AND OTBD HARDWARE IS CORRODED. MX R & R HARDWARE IAW AMM 27-65-01. - [SDR R61A201405260730](https://openairdocs.org/sdr/R61A201405260730), May 26, 2014: BOLT. CORRODED. DURING HEAVY CHECK, LT WING SPOILER ACTUATORS NR 4, & 5 INBD-OTBD HARWARE IS CORRODED. MX R & R LT WING SPOILER ACTUATOR HARWARE IAW AMM 27-65-01. PN NAS6121-31 - [SDR R61A201405260727](https://openairdocs.org/sdr/R61A201405260727), May 26, 2014: DOOR. CORRODED. DURING HEAVY CHECK, WASTE WATER DOOR INSIDE HAS CORROSION. MX R & R WASTE WATER DOOR IAW AMM 53-03-60. PN 170-86668-403 PANEL. - [SDR R61A201405260709](https://openairdocs.org/sdr/R61A201405260709), May 26, 2014: WASHER. CORRODED. DURING HEAVY CHECK FOUND RT WING NR 3 MIDDLE, FLAP TRACK SUPPORT FWD ATTACHMENT TO WING HARDWARE CORRODED. MX R & R RT WING NR 3, MIDDLE, FLAP TRACK SUPPORT FWD - [SDR R61A201405250737](https://openairdocs.org/sdr/R61A201405250737), May 25, 2014: RIB. CRACKED. DURING HEAVY CHECK, RT HORIZONTAL STAB L/E HAS RIB ON INBD SIDE CRACKED. MX CUT OUT DAMAGE INSTALLED FILLER AND DOUBLER IAW ETD 2014-170-045417. - [SDR R61A201405250729](https://openairdocs.org/sdr/R61A201405250729), May 25, 2014: RIB. CRACKED. DURING HEAVY CHECK, INBD RIB OF LT L/E OF HORIZONTAL STAB IS CRACKED. MAINTENANCE REMOVED DAMAGED SECTION OF RIB FABRICATED AND INSTALLED. - [SDR R61A201405250728](https://openairdocs.org/sdr/R61A201405250728), May 25, 2014: BRACKET. CRACKED. DURING HEAVY CHECK BRACKET ON FUSELAGE PANEL 195ER IS CRACKED. MX R & R BRACKET ON FUSELAGE PANEL 195ER IAW SRM 51-41-01, PN 170-15840-003 PROFILE. - [SDR R61A201405250726](https://openairdocs.org/sdr/R61A201405250726), May 25, 2014: BRACKET. CORRODED. DURING HEAVY CHECK, AFT LAV TOILET BOWL MOUNTING BRACKET AND HARDWARE IS CORRODED. MX R & R AFT LAV TOILET BOWL MOUNTING BRACKET AND HARDWARE IAW CMM 25-42-03, - [SDR R61A201309030836](https://openairdocs.org/sdr/R61A201309030836), Sep 3, 2013: DOOR. LACK OF LUBE. CREW REPORTED THAT THE L1 DOOR IS HARD TO OPEN FROM THE OUTSIDE. MX LUBED L1 DOOR AND PERFORMED OPS TEST IAW AMM. DOOR OPS CHECK GOOD. - [SDR R61A201307230653](https://openairdocs.org/sdr/R61A201307230653), Jul 23, 2013: GLOWSTRIP. LOOSE. CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP JUST AFT OF THE FRONT GALLEY IS LOOSE. MX REINSTALLED PHOTO LUMINESCENT STRIP IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201305090454](https://openairdocs.org/sdr/R61A201305090454), May 9, 2013: LIGHT. INOPERATIVE. CREW REPORTED THAT THE CAPTAINS FLASHLIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BULB PER EMB AMM 33-51-01, OPS CHECKED GOOD. - [SDR R61A201302270193](https://openairdocs.org/sdr/R61A201302270193), Feb 27, 2013: GLOWSTRIP. UNSECURE. CREW DISCOVERED PHOTO LUMINESCENT STRIP COMING UP AT ROW 18, SEATS D & F. MAINTENANCE RE-INSTALLED STRIP PER EMB AMM 33-50-2 AND OPS CHECKED GOOD. - [SDR R61A201302140162](https://openairdocs.org/sdr/R61A201302140162), Feb 14, 2013: SUPPORT BRACKET. CRACKED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND SUPPORT BRACKET AT FRAME 86 BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT FRAME 86 IAW EMB 170 SRM - [SDR R61A201302120161](https://openairdocs.org/sdr/R61A201302120161), Feb 12, 2013: BEAM. CRACKED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND BEAM CRACKED FOR OUTBOARD TCAS MOUNTING BRACKET. MAINTENANCE REMOVED AND REPLACED BEAM IAW EMB 170 SRM 51-41 - [SDR R61A201302070163](https://openairdocs.org/sdr/R61A201302070163), Feb 7, 2013: SUPPORT. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT PANEL SUPPORT AFT OF R2 DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE PANEL SUPPORT AFT OF T - [SDR R61A201302070160](https://openairdocs.org/sdr/R61A201302070160), Feb 7, 2013: RIB. CRACKED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING RIB 10 CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT WING RIB 10 IAW EMB 170 SRM 51-40-02 - [SDR R61A201302070159](https://openairdocs.org/sdr/R61A201302070159), Feb 7, 2013: CLAMP. CRACKED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT ACM INLET DUCT SUPPORT CLAMP CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM INLET DUCT CL - [SDR R61A201302070158](https://openairdocs.org/sdr/R61A201302070158), Feb 7, 2013: STRUCTURE. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE AFT WASTE BOX CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT WASTE BOX IAW EMB 170 SB 170-53-0095. T - [SDR R61A201302070151](https://openairdocs.org/sdr/R61A201302070151), Feb 7, 2013: SHEAR PLATE. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT SHEAR PLATE AT FRAMES 87 AND 88 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT SHEAR PLATE AT All 78: https://openairdocs.org/deregistered/N807MD-2021-05-08/reports.md --- 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.