# Service difficulty reports: N801MA, cancelled Jun 2, 2017

A list on [N801MA, cancelled Jun 2, 2017](https://openairdocs.org/deregistered/N801MA-2017-06-02.md).

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

Page 1 of 3 · 108 reports

- [SDR R61A201511150839](https://openairdocs.org/sdr/R61A201511150839.md): Unknown · odor · Nov 15, 2015 · N801MA · Emb ERJ170100SU · Cabin Cooling System
  > 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 WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201511040781](https://openairdocs.org/sdr/R61A201511040781.md): Connector · disconnected · Nov 4, 2015 · N801MA · Emb ERJ170100SU · Light System Wiring
  > 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.md): Autothrottle Sys · failed · May 12, 2015 · N801MA · Emb ERJ170100SU · Auto Throttle System
  > CREW REPORTED THAT THE AUTOPILOT AND AUTOTHROTTLES DISENGAGED AND CREW RECEIVED AN AVNX MAU1A FAIL MESSAGE. CREW RAN QRH AND DECLARED AN EMERGENCY. WITH PASSENGERS BRACING, CREW LANDED WITHOUT INCIDENT. AFTER BEING CHECKED OUT BY EMERGENCY VEHICLES, CREW ALLO
- [SDR R61A201504110236](https://openairdocs.org/sdr/R61A201504110236.md): Ramp · out of adjust · Apr 11, 2015 · N801MA · Emb ERJ170100SU · Service Doors
  > 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 NORMALLY. CREW DID NOT DECLARE AN EMERGENCY AND ELECTED TO RETURN TO WHERE THEY LANDED WITHOUT INCIDENT.
- [SDR R61A201503300224](https://openairdocs.org/sdr/R61A201503300224.md): Rib · corroded · Mar 30, 2015 · N801MA · Emb ERJ170100SU · Wing, Rib/Bulkhead
  > 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 170-57-0047, ALSO ETD 2015-170-028796, REV H. CONTINUATION CARD C1-C3 FOR DETAILS OF WORK. ACFT REMAINS U
- [SDR R61A201503250226](https://openairdocs.org/sdr/R61A201503250226.md): Rib · cracked · Mar 25, 2015 · N801MA · Emb ERJ170100SU · Wing, Rib/Bulkhead
  > 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 2013-170-000186. MAINTENANCE REPAIRED HOLE IAW ETD 2015-170-028597. FINAL HOLE SIZE.503 INSTALLED BUSHI
- [SDR R61A201503250225](https://openairdocs.org/sdr/R61A201503250225.md): Rib · cracked · Mar 25, 2015 · N801MA · Emb ERJ170100SU · Wing, Rib/Bulkhead
  > 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 HOLE IAW ETD 2015-170-028597 FINAL HOLE REAMED TO 504 INSTALLED BUSHING. C1-C2 FOR WORK DETAILS. AC
- [SDR R61A201503240199](https://openairdocs.org/sdr/R61A201503240199.md): Fitting · cracked · Mar 24, 2015 · N801MA · Emb ERJ170100SU · Wing Main, Frame Structure
  > 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 2015-170-028607, REV A, SEE CONTINUATION CARDS C1-C4 FOR WORK DETAILS. ACFT REMAINS UNTIL HEAY CH
- [SDR R61A201503240198](https://openairdocs.org/sdr/R61A201503240198.md): Fitting · cracked · Mar 24, 2015 · N801MA · Emb ERJ170100SU · Wing Main, Frame Structure
  > 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 PLUGS ARE INSTALLED IAW ETD2015-170, CONTINUATION CARDS C1-C6 FOR DETAILS. AIRCRAFT REMAINS UNTIL H
- [SDR R61A201503230223](https://openairdocs.org/sdr/R61A201503230223.md): Bushing · corroded · Mar 23, 2015 · N801MA · Emb ERJ170100SU · Elevator Structure
  > 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 PE64046H5-016-060C, BUSHING. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
- [SDR R61A201503230222](https://openairdocs.org/sdr/R61A201503230222.md): Bushing · corroded · Mar 23, 2015 · N801MA · Emb ERJ170100SU · Elevator Structure
  > 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 ELEVATOR IAW AMM 20-10-08.
- [SDR R61A201503230221](https://openairdocs.org/sdr/R61A201503230221.md): Nipple · corroded · Mar 23, 2015 · N801MA · Emb ERJ170100SU · Fuselage Miscellaneous Structure
  > 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 53-05-73.
- [SDR R61A201503220213](https://openairdocs.org/sdr/R61A201503220213.md): Bolt · corroded · Mar 22, 2015 · N801MA · Emb ERJ170100SU · Hydraulic System, Main
  > 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.md): Seat Track · corroded · Mar 22, 2015 · N801MA · Emb ERJ170100SU · Fuselage, Seat/Cargo Attach Fittings
  > 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 RESTORED TOPCOAT AND CIC IAW 51-25-00. PN 170-03264-001 TRACK. AIRCRAFT REMAINS UNTIL HEAVY CHECK
- [SDR R61A201503210212](https://openairdocs.org/sdr/R61A201503210212.md): Dampener · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Service Doors
  > 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.md): Bolt · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Passenger/Crew Doors
  > 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 LOCKING AND ACTUATING MECHANISM HANDLE IAW AMM 52-11-20.
- [SDR R61A201503210210](https://openairdocs.org/sdr/R61A201503210210.md): Bolt · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Spoilers
  > 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 REMAINS UNTIL HEAVY CHECK IS COMPLETED.
- [SDR R61A201503210209](https://openairdocs.org/sdr/R61A201503210209.md): Bolt · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Spoilers
  > 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.md): Bolt · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Spoilers
  > 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.md): Spigot · corroded · Mar 21, 2015 · N801MA · Emb ERJ170100SU · Buffet/Galleys
  > 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.md): Seat · cracked · Mar 20, 2015 · N801MA · Emb ERJ170100SU · Passenger Compartment Equipment
  > DURING HEAVY CHECK, SEAT PAN CRACKED. MAINTENANCE R & R THE SEAT PAN.
- [SDR R61A201410181123](https://openairdocs.org/sdr/R61A201410181123.md): Flashlight · inoperative · Oct 18, 2014 · N801MA · Emb ERJ170100SU · Emergency Equipment
  > 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.md): Processor · failed · Sep 21, 2014 · N801MA · Emb ERJ170100SU · Central Computers
  > 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 AUTOPILOT AN DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. FIRE DEPARTMENT ADVISED THE OTBD BRA
- [SDR R61A201409111052](https://openairdocs.org/sdr/R61A201409111052.md): Bleed Valve · failed · Sep 11, 2014 · N801MA · Emb ERJ170100SU · Pneumatic Distribution System
  > AROUND 6000 FEET, CREW RECEIVED A BLEED 1 OVERPRESSURE MESSAGE. CREW RAN QRH, HOWEVER MESSAGE REMAINED. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WHERE THEY LANDED WITHOUT INCIDENT. REPLACED THE BLEED VALVE.
- [SDR R61A201403020355](https://openairdocs.org/sdr/R61A201403020355.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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, 20-10-01.
- [SDR R61A201403020347](https://openairdocs.org/sdr/R61A201403020347.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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 & R CONNECTING FUEL TUBES, PN 170-08807-401, 170-08806-403, 170-06026-401 IAW AMM 20-10-03.
- [SDR R61A201403020346](https://openairdocs.org/sdr/R61A201403020346.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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 & R CONNECTING FUEL TUBES, PN 170-06027-401, 170-06024-401, 170-06025-401 IAW AMM 20-10-03. PN 170
- [SDR R61A201403020345](https://openairdocs.org/sdr/R61A201403020345.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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 CONNECTIONG FUEL TUBES.
- [SDR R61A201403020344](https://openairdocs.org/sdr/R61A201403020344.md): Tube · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Aircraft Fuel Distribution System
  > 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 CONNECTION FUEL TUBES, PN 170-06022-401 IAW AMM 20-10-03, PN 170-06022-401.
- [SDR R61A201403020343](https://openairdocs.org/sdr/R61A201403020343.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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 CONNECTION FUEL TUBES, PN 170-06037-401 IAW AMM 20-10-03, PN 170-06037-401 TUBE.
- [SDR R61A201403020342](https://openairdocs.org/sdr/R61A201403020342.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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.md): Clamp · corroded · Mar 2, 2014 · N801MA · Emb ERJ170100SU · Wing, Attach Fittings
  > 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, CLAMP.
- [SDR R61A201403010340](https://openairdocs.org/sdr/R61A201403010340.md): Rib · cracked · Mar 1, 2014 · N801MA · Emb ERJ170100SU · Horizontal Stabilizer, Spar/Rib
  > 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 2014-170-017791, REV A DATED MARCH 7,2014 SEE CONTINUATION CARDS C1,C2 FOR ALL WORK PERFORMED ISSUED DMI 467748/
- [SDR R61A201402280354](https://openairdocs.org/sdr/R61A201402280354.md): Bolt · corroded · Feb 28, 2014 · N801MA · Emb ERJ170100SU · Passenger/Crew Doors
  > 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.md): Rib · cracked · Feb 27, 2014 · N801MA · Emb ERJ170100SU · Horizontal Stabilizer, Spar/Rib
  > 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.md): Bracket · cracked · Feb 27, 2014 · N801MA · Emb ERJ170100SU · Fuselage Main, Attach Fittings
  > 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.md): Beam · corroded · Feb 14, 2014 · N801MA · Emb ERJ170100SU · Fuselage Main, Structure
  > 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 WHERE THE 2 HALVES MEET IAW AMM 25-0023,20-10-01,25-00-05. PN CDSP2200-11 SPLIT JOINT.
- [SDR R61A201312251352](https://openairdocs.org/sdr/R61A201312251352.md): Flashlight · inoperative · Dec 25, 2013 · N801MA · Emb ERJ170100SU · Emergency Equipment
  > CAPTAIN'S COCKPIT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR R61A201312061302](https://openairdocs.org/sdr/R61A201312061302.md): Slide · out of adjust · Dec 6, 2013 · N801MA · Emb ERJ170100SU · Escape Slide
  > 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.md): Mechanism · lack of lube · Sep 24, 2013 · N801MA · Emb ERJ170100SU · Passenger/Crew Doors
  > 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.md): Deflector · damaged · Sep 6, 2013 · N801MA · Emb ERJ170100SU · Service Doors
  > 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. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MX INSPECTED AND TRIMMED DOOR DEFLE
- [SDR R61A201309050841](https://openairdocs.org/sdr/R61A201309050841.md): Door · out of adjust · Sep 5, 2013 · N801MA · Emb ERJ170100SU · Passenger/Crew Doors
  > 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.md): Door · unknown · Sep 5, 2013 · N801MA · Emb ERJ170100SU · Service Doors
  > 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 PRESSURIZATION CHECK IAW AMM, WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201309030835](https://openairdocs.org/sdr/R61A201309030835.md): Seal · noisy · Sep 3, 2013 · N801MA · Emb ERJ170100SU · Service Doors
  > 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. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201309010829](https://openairdocs.org/sdr/R61A201309010829.md): Seal · dirty · Sep 1, 2013 · N801MA · Emb ERJ170100SU · Service Doors
  > 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 AND CLEANED THE R1 DOOR FRAME, SEAL AND DEFLECTOR IAW AMM. OPS CHECKED GOOD AND ACFT IS GOOD FOR SE
- [SDR R61A201308240774](https://openairdocs.org/sdr/R61A201308240774.md): Seal · dirty · Aug 24, 2013 · N801MA · Emb ERJ170100SU · Service Doors
  > 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.

Next page: https://openairdocs.org/deregistered/N801MA-2017-06-02/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N801MA' AND deregistration_id = 'N801MA-2017-06-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N801MA-2017-06-02/reports

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