# Service difficulty reports: N16987

A list on [N16987](https://openairdocs.org/aircraft/N16987.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 2 · 81 reports

- [SDR ASOA20191115112](https://openairdocs.org/sdr/ASOA20191115112.md): Fuse · failed · Nov 11, 2019 · N16987 · Emb EMB145LR · Emergency Lighting
  > MX REPORTED MULTIPLE EXTERNAL EMERGENCY LIGHTS INOP. MX FOUND EMERGENCY LIGHT TRAY #1 FUSE BLOWN TO LH WING FUSELAGE FRONT AND CEILING PANEL LIGHT AISLE AND AT BATTERY TRAY #2 FOR RH WING. REPLACED FUSES WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA2019062065078](https://openairdocs.org/sdr/ASOA2019062065078.md): Unknown · odor · Jun 16, 2019 · N16987 · Emb EMB145LR · Air Distribution System
  > CREW REPORTED BURNING SMELL WHEN COFFEE MAKER #2 IN OPERATION. ITEM PLACED ON MEL. MX PERFORMED OPERATIONAL CHECK GOOD WITH NO BURNING SMELL NOTED.
- [SDR ASOA201905237050](https://openairdocs.org/sdr/ASOA201905237050.md): Frame · chafed · May 23, 2019 · N16987 · Emb EMB145LR · Fuselage Main, Frame
  > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CHAFFING FROM A SCREW AT FRAME 70 BETWEEN STRINGER 12R AND 13R. MAINTENANCE REPAIRED THE CHAFE AREA FROM STR.12R TO 13R IAW ETD 2019-145-066859. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201905237049](https://openairdocs.org/sdr/ASOA201905237049.md): Trunnion · cracked · May 23, 2019 · N16987 · Emb EMB145LR · Fuselage, Landing Gear Attach Fittings
  > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE LT MLG AFT TRUNION CRACKED. MAINTENANCE REMOVED AND REPLACED THE LT TRUNION ON THE LT MLG AFT SIDE IAW ECTC ETD 2019-145-068830. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK.
- [SDR ASOA201905147046](https://openairdocs.org/sdr/ASOA201905147046.md): Rib · cracked · May 14, 2019 · N16987 · Emb EMB145LR · Wing, Rib/Bulkhead
  > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND RIB 21 INSIDE ACCESS PANEL 551CB CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND FAB. A FILLER AND DOUBLER FOR RIB 21 IAW SRM 57-20-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201905147045](https://openairdocs.org/sdr/ASOA201905147045.md): Rib · cracked · May 14, 2019 · N16987 · Emb EMB145LR · Wing, Rib/Bulkhead
  > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND A CRACK AT RIB 21 INSIDE ACCESS PANEL 651CB. MAINTENANCE REMOVED THE DAMAGED AREA OF RIB 21 AND REPLACED WITH FILLER AND DOUBLER IAW SRM 57-20-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201901023001](https://openairdocs.org/sdr/ASOA201901023001.md): Coffeemaker · faulty · Jan 2, 2019 · N16987 · Emb EMB145LR · Buffet/Galleys
  > THE CREW REPORTED ELECTRICAL SMELL COMING FROM GALLEY, WENT AWAY WHEN COFFEE MAKERS WERE SHUT OFF. MAINTENANCE REPLACED COFFEE BREWER IN LT POSITION. OPS CHECK GOOD
- [SDR ASOA201705113145](https://openairdocs.org/sdr/ASOA201705113145.md): Stringer · cracked · May 11, 2017 · N16987 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > LEFT REAR FUSELAGE STRINGER 2L CRACKED AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR ASOA201705093143](https://openairdocs.org/sdr/ASOA201705093143.md): Channel · corroded · May 9, 2017 · N16987 · Emb EMB145LR · Service Doors
  > SERVICE DOOR CHANNEL CORRODED. CHANNEL REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705093142](https://openairdocs.org/sdr/ASOA201705093142.md): Structure · corroded · May 9, 2017 · N16987 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > PAX DOOR SILL AFT "U" SHAPE CORRODED. AFT "U" SHAPE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705093141](https://openairdocs.org/sdr/ASOA201705093141.md): Structure · corroded · May 9, 2017 · N16987 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > PAX DOOR SILL FORWARD U SHAPE CORRODED. FORWARD U SHAPE REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201705073140](https://openairdocs.org/sdr/ASOA201705073140.md): Seat Track · corroded · May 7, 2017 · N16987 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK LT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073139](https://openairdocs.org/sdr/ASOA201705073139.md): Seat Track · corroded · May 7, 2017 · N16987 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK RT NR 3 INBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073138](https://openairdocs.org/sdr/ASOA201705073138.md): Seat Track · corroded · May 7, 2017 · N16987 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK RT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.
- [SDR ASOA201705073137](https://openairdocs.org/sdr/ASOA201705073137.md): Bearing · corroded · May 7, 2017 · N16987 · Emb EMB145LR · Main Landing Gear
  > RT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-CO2-A00.
- [SDR ASOA201705073136](https://openairdocs.org/sdr/ASOA201705073136.md): Bearing · corroded · May 7, 2017 · N16987 · Emb EMB145LR · Main Landing Gear
  > LT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-C02-A00.
- [SDR ASOA201705053135](https://openairdocs.org/sdr/ASOA201705053135.md): Doubler · corroded · May 5, 2017 · N16987 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON DOUBLER AROUND POTABLE WATER NIPPLES. DOUBLER REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705053134](https://openairdocs.org/sdr/ASOA201705053134.md): Stringer · corroded · May 5, 2017 · N16987 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 15R BETWEEN FRAMES 40 AND 41 CORRODED BEYOND LIMITS. REPLACED IAW SRM 53-10-02.
- [SDR ASOA201705043133](https://openairdocs.org/sdr/ASOA201705043133.md): Door Sill · corroded · May 4, 2017 · N16987 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SERVICE DOOR AFT SILL CORRODED. SERVICE DOOR AFT SILL REPAIRED AS PER SRM 53-21-10 ITEM 5 FIG 204 SHEET 3. HFEC PERFORMED WITH NO FAULT FOUND.
- [SDR ASOA201705023128](https://openairdocs.org/sdr/ASOA201705023128.md): Floorbeam · corroded · May 2, 2017 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > CENTER FUSELAGE MIDDLE FLOORBEAM CORRODED AROUND ANCHOR NUT HOLES. FLOORBEAM REPLACED IAW SRM 51-40-02.
- [SDR ASOA201705023127](https://openairdocs.org/sdr/ASOA201705023127.md): Channel · cracked · May 2, 2017 · N16987 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT WEB CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEELWELL. CHANNEL REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704203096](https://openairdocs.org/sdr/ASOA201704203096.md): Crossbeam · cracked · Apr 20, 2017 · N16987 · Emb EMB145LR · Fuselage Main, Structure
  > NLG UPLOCK AFT CROSSBEAM CRACKED. THE UPLOCK CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201704203095](https://openairdocs.org/sdr/ASOA201704203095.md): Crossbeam · cracked · Apr 20, 2017 · N16987 · Emb EMB145LR · Fuselage Main, Structure
  > NLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201612223088](https://openairdocs.org/sdr/ASOA201612223088.md): Battery Pack · inoperative · Dec 22, 2016 · N16987 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING AFT EMERENGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA20150305007](https://openairdocs.org/sdr/ASOA20150305007.md): Rib · cracked · Mar 5, 2015 · N16987 · Emb EMB145LR · Wing, Rib/Bulkhead
  > ACFT IS IN C-CHECK WHEN INSPECTION FOUND A CRACK ON THE LT WING AT RIB NR 5 IN AREA FWD OF PREVIOUS SB MOD. CRACK RUNS FROM LOWER FLANGE OTBD THRU THE HYLOCK HOLE AND CONTINUOUS VERTICALLY 6". R & R THE NR 5 RIB IAW EC5710-01239. ALL WORK ACCOMPLISHED AND
- [SDR ASOA20150305006](https://openairdocs.org/sdr/ASOA20150305006.md): Skin · gouged · Mar 5, 2015 · N16987 · Emb EMB145LR · Wing, Plate/Skin
  > ACFT IS IN A C-CHECK STATUS WHEN INSPECTION FOUND TOOLING MARKS ON THE LT WING ZONE 532 UPPER SKIN, THAT SHOWED A GROOVE CUT INTO THE SKIN. MAINTENANCE INSTALLED A REPAIR TO THE UPPER SKIN IAW EC5710-01240. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE EN
- [SDR ASOA20140124022](https://openairdocs.org/sdr/ASOA20140124022.md): Engine · smoke · Jan 24, 2014 · N16987 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > STRONG SMELL AND A SMOKE HAZE WAS PRESENT IN CABIN WHEN PACK 1 WAS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE IAW MM.
- [SDR ASOA20130812062](https://openairdocs.org/sdr/ASOA20130812062.md): Valve · leaking · Aug 12, 2013 · N16987 · Emb EMB145LR · Fuel Storage
  > THE CREW REPORTED A SUSPECTED FUEL LEAK IN OTBD LT WING DURING FLIGHT. MX INSPECTED AND REPLACED A LT WING FUEL FLAP VALVE. OPS CHECKS WERE GOOD.
- [SDR ASOA20130525052](https://openairdocs.org/sdr/ASOA20130525052.md): Control Unit · faulty · May 25, 2013 · N16987 · Emb EMB145LR · Landing Gear Brake System
  > CREW REPORTED OTBD BRAKE INOPERATIVE. MX R & R THE BRAKE CONTROL UNIT WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130423152](https://openairdocs.org/sdr/ASOA20130423152.md): Door Frame · corroded · May 11, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Structure
  > DURING A-CHECK, PAX DOOR CUTOUT WAS FOUND CORRODED AT FRAME 18 BETWEEN STRINGERS 15-16L. MX REMOVED THE CORRODED SECTION AND PERFORMED A SPLICE REPAIR IAW EC5310-01690. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR V0XR201303100178](https://openairdocs.org/sdr/V0XR201303100178.md): Floorbeam · damaged · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04, 51-21-05, AND 51-21-06.
- [SDR V0XR201303100177](https://openairdocs.org/sdr/V0XR201303100177.md): Floorbeam · damaged · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.
- [SDR V0XR201303100176](https://openairdocs.org/sdr/V0XR201303100176.md): Floorbeam · damaged · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02,CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.
- [SDR V0XR20130310J0175](https://openairdocs.org/sdr/V0XR20130310J0175.md): Fairing · loose · Mar 7, 2013 · N16987 · Emb EMB145LR · Aerodynamic Fairings
  > LOOSE FASTENERS AT FRAME BETWEEN 59/60 BETWEEN STR 21L AND 21R. INSTALLED DOUBLERS IAW EC5320-01761 AND INSTALLED RT AND LT FAIRINGS IAW SRM 51-40-02.
- [SDR V0XR201303100174](https://openairdocs.org/sdr/V0XR201303100174.md): Door Frame · corroded · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Structure
  > SURFACE UNDER LOWER AFT MAIN DOOR GUIDE AT FRAME 18 BS 5417 CORRODED. BLENDED CORRODED AREA, FOUND WITHIN LIMITS AT FRAME 18 STA. 5417 IAW EC5310-01684 (TEMPORARY REPAIR OF 600 FC'S PERMANENT REPAIR EC5310-01690)
- [SDR V0XR201303100173](https://openairdocs.org/sdr/V0XR201303100173.md): Floorbeam · corroded · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > PAX FLOORBEAM CORRODED AT FS 693.80 R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100172](https://openairdocs.org/sdr/V0XR201303100172.md): Floorbeam · corroded · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > PAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100171](https://openairdocs.org/sdr/V0XR201303100171.md): Floorbeam · corroded · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Floor Beam
  > PAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.
- [SDR V0XR201303100170](https://openairdocs.org/sdr/V0XR201303100170.md): Skin · scratched · Mar 7, 2013 · N16987 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > MULTIPLE SCRATCHES (3) FRAME 59 STR.17R AND FRAME 78 STR. 18R. PERFORMED REPAIR ON SCRATCH AT FRAME 59 STR 17R IAW EC 5330-02788.TWO OTHER SCRATCHES AT FRAME 22-23 STR. 20L AND ON FRAME 78 STR. 18R ARE STRUCTURALLY EXCEPTABLE IAW ETD2012-145-017252-A (REF. W/
- [SDR ASOA20121017093R](https://openairdocs.org/sdr/ASOA20121017093R.md): Bolt · unsecure · Oct 17, 2012 · N16987 · Emb EMB145LR · Passenger/Crew Doors
  > CREW REPORTED MAIN CABIN DOOR LEVER PRODUCES LOUD METAL POP SOUND WHEN OPENING AND FEELS UNUSUALLY HARD TO OPEN. MX INSPECTED AND FOUND HARDWARE LOOSE, RESECURED THE INTERNAL HANDLE BOX BOLTS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE
- [SDR C2XA11CL228](https://openairdocs.org/sdr/C2XA11CL228.md): Connector · loose · Oct 11, 2011 · N16987 · Emb EMB145LR · Landing Gear System Wiring
  > ORD FLT 5983 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED PROXIMITY SWITCH INSPECTION OF BOTH THE MAIN AND NOSE GEAR. FOUND THE NOSE GEAR WOW PROXIMI
- [SDR C2XA11CL212](https://openairdocs.org/sdr/C2XA11CL212.md): Wire Harness · chafed · Sep 20, 2011 · N16987 · Emb EMB145LR · Fire Protection System Wiring
  > THE CREW REPORTED AN ENGINE NR 2 FIRE DETECT FAIL MESSAGE ONLY DURING DESCENT, LOW PITCH ATTITUDE AND THRUST LEVER AT IDLE. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE FIRE DETECT HARNESS. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11IA169](https://openairdocs.org/sdr/C2XA11IA169.md): Unknown · odor · Aug 2, 2011 · N16987 · Emb EMB145LR · Air Distribution System
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND GROUND RAN THE ENGINES ALL WITH NO DEFECTS OR SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI048](https://openairdocs.org/sdr/C2XA11RI048.md): Unknown · smoke · Mar 24, 2011 · N16987 · Emb EMB145LR · Air Distribution System
  > FLIGHT 2540 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN AND PERFORMED AIR RETURN UNEVENTFULLY. EWR MX PERFORMED ENGINE RUNUP (1 & 2) AT HIGH POWER WITH BLEED SYSTEM ON FOR 5 MIN. NO SMOKE NOTICED. ACFT APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11SHO54](https://openairdocs.org/sdr/C2XA11SHO54.md): Skin · cracked · Mar 5, 2011 · N16987 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK CRACK AROUND RIVET FRAME 75 STRINGER 2L-3L (VERIFIED WITH EDDY CURRENT). MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 75 STRINGER 2L-3L IAW EC5330-02353. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI008](https://openairdocs.org/sdr/C2XA11RI008.md): Unknown · smoke · Jan 21, 2011 · N16987 · Emb EMB145LR · Air Distribution System
  > FLIGHT 2513 - MHT - FLIGHT CREW REPORTED LAV FIRE WARNING ON CLIMB - SMOKE IN THE LAV - CREW PERFORMED AIR RETURN AND LANDED SAFELY - NO EMERGENCY DECLARED. CONTRACTED MX INSPECTED LAV - NO DEFECTS FOUND - AND PERFORMED ENGINE FULL POWER RUN, APU AND PACKS CH
- [SDR C2XA10IA347](https://openairdocs.org/sdr/C2XA10IA347.md): Skin · cracked · Dec 27, 2010 · N16987 · Emb EMB145LR · Wing, Plate/Skin
  > DURING MAINTENANCE INSPECTION THE LEFT WING SKIN WAS FOUND TO BE CRACKED AT THE INBOARD SPOILER CENTER HINGE POINT CUTOUT. MAINTENANCE STOP DRILLED THE CRACK, AND PLACED THE AIRCRAFT ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE PE
- [SDR C2XA09CL157](https://openairdocs.org/sdr/C2XA09CL157.md): Carbon Seal · malfunctioned · Dec 11, 2009 · N16987 · Emb EMB145 · Turbine Engine Oil System
  > CLE FLT 2542 THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. TEAR DOWN REPORT FROM ROLLS ROYCE INDICATED THE NR 0 CARBON SEAL RUNNER WA
- [SDR C2XA09IA144](https://openairdocs.org/sdr/C2XA09IA144.md): Drain · damaged · May 28, 2009 · N16987 · Emb EMB145LR · Pitot/Static System
  > IAH - FLIGHT 2627 DURING CLIMB THE CREW REPORTED, LOST IAS INDICATIONS ON BOTH SIDES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED DAMAGED PITOT DRAINS ON NR 1 & 2 SIDES, LEAK CHECK WITH NO DEFECTS NOTED. T
- [SDR C2XA09IA143](https://openairdocs.org/sdr/C2XA09IA143.md): Ahrs · malfunctioned · May 28, 2009 · N16987 · Emb EMB145LR · Integrated Flight System
  > IAH - FLIGHT 2627 - DURING CLIMB THE CREW REPORTED THAT BOTH THE PILOT AND COPILOT ATT AND HDG FAILED. THE AIRCRAFT RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AHRS COMPUTER, OPERATIONALLY TESTED

Next page: https://openairdocs.org/aircraft/N16987/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 = 'N16987' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N16987/reports

---
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.