# Service difficulty reports: N27190

A list on [N27190](https://openairdocs.org/aircraft/N27190.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 · 109 reports

- [SDR JJBA20260908002](https://openairdocs.org/sdr/JJBA20260908002.md): Door · binding · Sep 3, 2026 · N27190 · Emb EMB145XR · Passenger/Crew Doors
  > MCD DIFFICULT TO CLOSE AND OPEN. WHEN DOOR IS CLOSED IT SHOWS OPEN UNTIL OPENED AND CLOSED SEVERAL TIMES TO ACTUALLY CLOSE WITH CLOSED INDICATION. INSPECTED MICROSWITCHES. OPS CHECKED MCD. OPS CHECK SAT. NO FAULTS NOTED AT THIS TIME.
- [SDR JJBA20260819014](https://openairdocs.org/sdr/JJBA20260819014.md): Engine · failed · Aug 16, 2026 · N27190 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > E1 OUT IN FLIGHT AT FLIGHT LEVEL 300. OCCURRED AT 30000, IT WAS SMOOTH AND THEN SEEMED LIKE TURBULENCE AND #1 ENGINE SHUTDOWN WITH EICAS MESSAGE. ATTEMPTED #1 ENGINE START WITH NO N2 AND NO FUEL FLOW. OIL AT 11 QTS, NORMAL ENGINE VIBRATION AND OIL TEMPS IN THE
- [SDR JJBA20251125108](https://openairdocs.org/sdr/JJBA20251125108.md): Control Unit · inoperative · Nov 22, 2025 · N27190 · Emb EMB145XR · Elevator Control System
  > PITCH TRIM INOPERATIVE MESSAGE AT V1. REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT. OPS/INDICATION CHECK SAT.
- [SDR JJBA20250911010](https://openairdocs.org/sdr/JJBA20250911010.md): Skin · cracked · Sep 5, 2025 · N27190 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > EXTERNAL REAR FUSELAGE SKIN, DENT FOUND 8 INCHES AFT FRAME 77, BTW STR 14L-15L. REPAIR DOUBLER ON LH REAR FUSE II SKIN, BTW FR 77-80 AND BTW STR 13L-16L
- [SDR JJBA20250911009](https://openairdocs.org/sdr/JJBA20250911009.md): Skin · cracked · Sep 5, 2025 · N27190 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FF1 RH SKIN CRACKED AT FR 4 AND EDGE OF SKIN AT NLG CUTOUT. REPAIR DOUBLER ON RH FWD FUSE I SKIN, AT FR 4 AND ON LOWER EDGE.
- [SDR JJBA20250904005](https://openairdocs.org/sdr/JJBA20250904005.md): Fitting · cracked · Aug 22, 2025 · N27190 · Emb EMB145XR · Cargo/Baggage Doors
  > ON BAGGAGE DOOR LIFTING AND LOWERING MECHANISM, FWD AND AFT SUPPORTS FOUND WITH CRACKS. BAGGAGE DOOR LIFTING AND LOWERING MECHANISM REMOVED FOR ACCESS. ON BAGGAGE DOOR LIFTING AND LOWERING MECHANISM FWD SUPPORT ANGLE REMOVED FOR REPLACEMENT. ON BAGGE DOOR LIFT
- [SDR JJBA20250911020](https://openairdocs.org/sdr/JJBA20250911020.md): Shear Tie · cracked · Aug 13, 2025 · N27190 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > CF1, SHEAR CLIP ON FR15 BTW STR 15R-16R FOUND CRACKED. CF1, ON EXTERNAL SKIN AT FR 15 BTW STR 15R-16R REMOVED AND REPLACED.
- [SDR JJBA20250916022](https://openairdocs.org/sdr/JJBA20250916022.md): Support · corroded · Aug 12, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE IV. LH SILL CORRODED BTW FRAME 60-61. CENTER FUSELAGE IV, LH SILL CORRODED BTW FRAME 60-61 BLENDED OUT OF LIMIT. CENTER FUSELAGE IV, LH SILL AT FR 60-61 REMOVED AND REPLACED
- [SDR JJBA20250909008](https://openairdocs.org/sdr/JJBA20250909008.md): Crossbeam · corroded · Aug 12, 2025 · N27190 · Emb EMB145XR · Fuselage Main, Structure
  > CF1, CENTER CROSSBEAM AT FR20 FOUND CORRODED. CF1 CENTER CROSSBEAM AT FR20 BLENDED AND FOUND OUT OF LIMIT. CF1 CENTER CROSSBEAM AT FR20 INSTALLED
- [SDR JJBA20250904003](https://openairdocs.org/sdr/JJBA20250904003.md): Support · corroded · Aug 12, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RIGHT SIDE SILL BTW FR 22-24 FOUND CORRODED. CF1, RH SIDE SILL BTW FR 22-24 BLENDED OUT OF LIMIT. SILL REMOVED AND REPLACED.
- [SDR JJBA20250902001](https://openairdocs.org/sdr/JJBA20250902001.md): Web · cracked · Aug 12, 2025 · N27190 · Emb EMB145XR · Wing Miscellaneous Structure
  > RH AFT MLG WEB CRACKED. RH AFT MLG WEB REPLACED.
- [SDR JJBA20250829064](https://openairdocs.org/sdr/JJBA20250829064.md): Seat Track · damaged · Aug 12, 2025 · N27190 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK BTW FR29-30 BLENDED OUT OF LIMITS. R/H SIDE WALL SEAT TRACK BTW FR29-30 REMOVED AND REPLACED.
- [SDR JJBA20250829063](https://openairdocs.org/sdr/JJBA20250829063.md): Seat Track · damaged · Aug 12, 2025 · N27190 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SAT TRACKS BTW FR31-32 FLENDED OUT OF LIMITS. L/H FLOOR SEAT TRACK BTW FR30-31 AND FR41-32 REOVED AND REPLACED.
- [SDR JJBA20250904006](https://openairdocs.org/sdr/JJBA20250904006.md): Channel · corroded · Aug 11, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL FOUND CORRODED. CF1, SERVICE DOOR CUT OUT, ENTRANCE CHANNEL BLENDED OUT OF LIMIT. CF1, SERVICE DOOR CUTOUT, ENTRANCE CHANNEL REMOVED FOR REPLACEMENT. CF1, SERVICE DOOR CUT-OUT, ENTRANCE CHANNEL REPLACED.
- [SDR JJBA20250827058](https://openairdocs.org/sdr/JJBA20250827058.md): Gusset · corroded · Aug 11, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 CORRODED OUT OF LIMITS CENTER FUSELAGE IV, CENTER GUSSET BTW FR59-61 REPLACED.
- [SDR JJBA20250827057](https://openairdocs.org/sdr/JJBA20250827057.md): Gusset · corroded · Aug 11, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE IV, RH GUSSET BTW FRAME 59-61 CORRODED. R/H GUSSET BLENDED OUT OF LIMITS. TH GUSSET BTW FR59-61 REMOVED FOR REPLACEMENT. CENTER FUSELAGE IV, R/H GUSSET BTW FR 59-61 REPLACED.
- [SDR JJBA20250827061](https://openairdocs.org/sdr/JJBA20250827061.md): Bracket · cracked · Aug 8, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > AFTER GUSSET REMOVAL, ANGLE BRACKET FOUND CRACKED BTW FR 20-21 ON CENTER BEAM HAT SECTION AT FR 20-21 ANGLE REMOVED FOR REPLACEMENT. ANGLE BRACKET REPLACED WITH MADE REPAIR PART INLAY FABRICATED. INSTALLED. FLUORESCENT PENETRANT INSPECTION CARRIED OUT ON LOCAL
- [SDR JJBA20250827060](https://openairdocs.org/sdr/JJBA20250827060.md): Gusset · corroded · Aug 8, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER GUSSET BTW FR18-24 FOUND CORRODED. CF1 CENTER GUSSET BTW FR18-24 BLENDED AND FOUND OUT OF LIMITS. CF1, CENTER GUSSET BTW FR18-24 REMOVED. CENTER GUSSET BTW FR18-24 REPLACED.
- [SDR JJBA20250827059](https://openairdocs.org/sdr/JJBA20250827059.md): Angle · corroded · Aug 8, 2025 · N27190 · Emb EMB145XR · Trailing Edge Flaps
  > RIGHT INBD FLAP INBD TIP, ONE ANGLE IS CORRODED. RT INBD FLAP INBD TIP, ONE ANGLE BLENDED OUT OF LIMITS. RH INBD FLAP INBD TIPO, ANGLE REMOVED AND REPLACED.
- [SDR JJBA20250827056](https://openairdocs.org/sdr/JJBA20250827056.md): Shear Tie · cracked · Aug 8, 2025 · N27190 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > SHEAR CLIP ON FR16 BTW STR15R-16R FOUND CRACKED. REMOVED AND REPLACED CF1 SHEAR CLIP ON FR16 BTW STR15R-16R.
- [SDR JJBA20250904004](https://openairdocs.org/sdr/JJBA20250904004.md): Support · corroded · Aug 7, 2025 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RH SILL BTW FR 41-48 FOUND CORRODED. CF3, RH SILL BTW FR 41-48 IS OUT OF LIMIT. CF3, RH SILL BTW FR 41-48 REMOVED AND INSTALLED.
- [SDR JJBA20250825054](https://openairdocs.org/sdr/JJBA20250825054.md): Shear Tie · cracked · Aug 7, 2025 · N27190 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > FR30 BTW STR15-16 SHEAR CLIP CRACKED FR30 BTW STR15-16 SHEAR CLIP REMOVED, FR30 BTW STR15-16 SHEAR CLIP REPLACED
- [SDR JJBA20250203025](https://openairdocs.org/sdr/JJBA20250203025.md): Engine · faulted · Jan 29, 2025 · N27190 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > ENG 1 SHUTDOWN IN FLIGHT. REMOVED AND REPLACED #1 ENGINE. OPS AND LEAK CHECK SAT.
- [SDR JJBA20240822015](https://openairdocs.org/sdr/JJBA20240822015.md): Control Unit · inoperative · Aug 18, 2024 · N27190 · Emb EMB145XR · Landing Gear Brake System
  > BRAKE OUTBOARD INOPERATIVE EICAS MESSAGE. BRAKES NOT ENGAGING 100% ON LANDING ROLL. LEFT INBOARD BRAKE TEMP IN YELLOW. FOUND NO BRAKE RELATED CMC MESSAGES. REMOVED ALL 4 HUB CAPS AND INSPECTED TRANSDUCERS, FOUND NO VIABLE FAULT, REINSTALLED HUB CAPS. REMOVED A
- [SDR JJBA20240807010](https://openairdocs.org/sdr/JJBA20240807010.md): Stop Fitting · missing · Aug 5, 2024 · N27190 · Emb EMB145XR · Passenger/Crew Doors
  > MCD FWD TOP STOP MISSING, WITH SHIMS FELL OUT. FWD TOP STOP FOUND TO BE IN SERVICEABLE CONDITION. FOUND AFT MIDDLE STOP TO BE MISSING INSTEAD. INSTALLED AND ADJUSTED AFT MIDDLE STOP. PERFORMED PRESSURIZATION TEST. LEAK CHECK SAT.
- [SDR JJBA20231204001](https://openairdocs.org/sdr/JJBA20231204001.md): Unknown · unknown · Dec 1, 2023 · N27190 · Emb EMB145XR · Air Distribution System
  > LAV SMOKE WARNING ON EICAS IN FLIGHT. INSPECTED AND PERFORMED OPS CHECK OF LAV LIGHTS AND BALLAST. OPS CHECK SAT, NO SINGS OF BURNING/DAMAGE. PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYSTEM. OPS CHECK SAT. UNABLE TO DUPLICATE FAULT AT THIS TIME. NO FAULTS F
- [SDR JJBA20231204040](https://openairdocs.org/sdr/JJBA20231204040.md): Unknown · unknown · Nov 30, 2023 · N27190 · Emb EMB145XR · Air Conditioning System
  > WHEN IN VISABLR MOISTURE ELECTRICAL SMELL THROUGHOUT CABIN IN COCKPIT CENTER FLOOR BOARD FELT WARM. FOUND EVIDENCE OF DE-ICING FLUID RESIDUE. CLEANED UP FLUID. NO ADDITIONAL DEFECTS NOTED.
- [SDR JJBA20230804003](https://openairdocs.org/sdr/JJBA20230804003.md): Unknown · unknown · Aug 4, 2023 · N27190 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHT LAMP ABOVE SERVICE DOOR INOPERATIVE. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM. LIGHT OPS CHECK GOOD.
- [SDR JJBA20230703022](https://openairdocs.org/sdr/JJBA20230703022.md): Actuator · leaking · Jun 27, 2023 · N27190 · Emb EMB145XR · Trailing Edge Flap Actuator
  > FLAP FAIL ON EICAS AFTER FLAPS RETRACTED. RETRACTING THE FLAPS FROM 9 TO 0 AND IMMEDIATELY RECEIVED FAIL AND THE INDICATION DASHED OUT AND KEPT THE AIRCRAFT BELOW 250 KNOTS. CREW REPORTED NO HARD OR OVERWEIGHT LANDING "REPLACED FPDU. REPLACED FECU. PERFORMED Z
- [SDR JJBA20220618012](https://openairdocs.org/sdr/JJBA20220618012.md): None · none · Jun 18, 2022 · N27190 · Emb EMB145XR · Emergency Lighting
  > FOUND COCKPIT STEP EMERGENCY EXIT LIGHT INOPERATIVE. FOUND HARNESS FOR COCKPIT STEP EMERGENCY LIGHT DISCONNECTED. RECONNECTED HARNESS. OPS CHECK SAT.
- [SDR JJBA20220513024](https://openairdocs.org/sdr/JJBA20220513024.md): Battery Pack · inoperative · May 13, 2022 · N27190 · Emb EMB145XR · Emergency Lighting
  > BOTH FWD WTF EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS #1 AND #2. OPS CHECK SAT FOR #1. OPS CHECK FAILED FOR #2. PART BAD FROM STOCK. REMOVED AND REPLACED #2. OPS CHECK SAT.
- [SDR JJBA20210505018](https://openairdocs.org/sdr/JJBA20210505018.md): None · none · May 5, 2022 · N27190 · Emb EMB145XR · Fuselage Structure (General)
  > AT REAR FUSE II EXT, SUSPECTED CRACKS (7X) FOUND ON RH SIDE SKIN BTW FR 77-FR80 AND BTW STR 3R-9R. AFTER INVESTIGATION 7 SUSPECTED CRACKS CONFIRMED. FRAME 77 BTW STR 3R-4R TWO CRACKS TOO CLOSED REPAIRED WITH DOUBLER. (X5) BUSHING LOCALLY FABRICATED)MADE REPAI
- [SDR JJBA20220505017](https://openairdocs.org/sdr/JJBA20220505017.md): None · none · May 5, 2022 · N27190 · Emb EMB145XR · Fuselage Structure (General)
  > AT REAR FUSE EXT, DAMAGE FOUND ON BELLY SKIN BTW FR73-74 AND BTW STR 19L-19R. RH REAR FUSELAGE #1 SKIN BTW FR72-76 AND BTW STR 16R TO 20L REMOVED AND SPLICED. NEW SKIN SECTION LOCALLY FABRICATED. RH REAR FUSELAGE #1 SKIN BTW FR77 - FR 76 AND BTW STR 16R-20L RE
- [SDR JJBA20220503016](https://openairdocs.org/sdr/JJBA20220503016.md): None · none · May 3, 2022 · N27190 · Emb EMB145XR · Fuselage Structure (General)
  > AT CFII, CORROSION FOUND ON LOWER STR 21R BTW FR50-51 IN U/FLOOR AREA. LOWER STR 21R BTW FR50-51 IN UNDERFLOOR AREA FOUND BADLY CORRODED. LOWER STR 21R BTW FR 50-51 IN UNDERFLOOR AREA REPLACED.
- [SDR JJBA20220503015](https://openairdocs.org/sdr/JJBA20220503015.md): None · none · May 3, 2022 · N27190 · Emb EMB145XR · Fuselage Structure (General)
  > CIRCULAR DOUBLER AT FWD BULKHEAD TO BE REMOVED FOR REPAIR MAPPING. DOUBLER AT FWD BULKHEAD REMOVED FOR INVESTIGATION. CIRCULAR DOUBLER AT FWD BULKHEAD REPLACED WITH MADE REPAIR PART, LOCALLY FABRICATED.
- [SDR JJBA20220102002](https://openairdocs.org/sdr/JJBA20220102002.md): Control Unit · inoperative · Jan 2, 2022 · N27190 · Emb EMB145XR · Stabilizer Control System
  > PITCH TRIM BACKUP INOPERATIVE ON EICAS IN FLIGHT. R&R HSCU. ADJUSTMENT TEST CARRIED OUT. REPLACED HAS. OPS CHECK SAT.
- [SDR JJBA202201020002](https://openairdocs.org/sdr/JJBA202201020002.md): Control Unit · inoperative · Jan 2, 2022 · N27190 · Emb EMB145XR · Elevator Tab Control System
  > PITCH TRIM BACKUP INOPERATIVE ON EICAS IN FLIGHT. R&R HSCU. ADJUSTMENT TEST CARRIED OUT. REPLACED HAS. OPS CHECK SAT.
- [SDR JJBA20210410025](https://openairdocs.org/sdr/JJBA20210410025.md): Armrest · cracked · Apr 10, 2021 · N27190 · Emb EMB145XR · Passenger Compartment Equipment
  > FOUND CRACK IN PAX SEAT ARMREST AT 3A, 4A, 5A, 6A, 7A, 9A, 10A. RR PAX SEAT 3A, 4A, 5A, 6A, 7A, 9A, 10A.
- [SDR JJBA20210211011](https://openairdocs.org/sdr/JJBA20210211011.md): Anti-Ice Valve · cracked · Feb 11, 2021 · N27190 · Emb EMB145XR · Engine Anti-Icing System
  > ENG A/I FAIL, NO ICE ON, AND BLEED 1 LOW TEMP MESSAGES IN FLIGHT (E2 E/I FAIL WITH NO ICE A/I ON MESSAGES ON CLIMB FROM FL220 TO FL270. BLEED 1 LOW TEMP CAME ON AT 3000 FEET ON APPROACH WITH N1 AT 70% AND N2 80-85%. PERFORMED A/I ADJUSTMENT TEST. OPS CHECK SAT
- [SDR JJBA20220503014](https://openairdocs.org/sdr/JJBA20220503014.md): None · none · May 3, 2020 · N27190 · Emb EMB145XR · Fuselage Structure (General)
  > AT CF I EXT, DENT FOUND ON LH SIDE SKIN BTW FR 19 - FR 20 AND BTW STR 11L-12L. AT CFI EXT, BTW FR 19-20 BTW STR 11L-12L, SKIN REPAIRED
- [SDR JJBA202004283005](https://openairdocs.org/sdr/JJBA202004283005.md): Battery Pack · discharged · Apr 23, 2020 · N27190 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHTS AT MAIN DOOR, MAIN ENTRANCE CEILING PANEL, COCK PIT FLOOR, GALLEY ISLE CEILING PANEL AND FWD WING-TO-FUSE, AND EMERGENCY EXIT SIGNS AT COCKPIT BULKHEAD, COCKPIT STEP, AND GALLEY CENTER AISLE CEILING INOP (8 LIGHTS TOTAL). R&R #1 EMERGENCY LIGH
- [SDR JJBA202004109004](https://openairdocs.org/sdr/JJBA202004109004.md): Light · inoperative · Apr 9, 2020 · N27190 · Emb EMB145XR · Emergency Lighting
  > LH FWD OF WING EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R LH FWD OF WING EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA202004109003](https://openairdocs.org/sdr/JJBA202004109003.md): Light · inoperative · Apr 9, 2020 · N27190 · Emb EMB145XR · Emergency Lighting
  > SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20190704012](https://openairdocs.org/sdr/JJBA20190704012.md): Unknown · malfunctioned · Jul 4, 2019 · N27190 · Emb EMB145XR · Drag Control System
  > AIRCRAFT UNCOMMANDED LEFT ROLL TWICE DURING DESCENT, WITH & WITHOUT AP ON. INADVERTENT SPOILER OPEN QRH PERFORMED, NO ROLL ISSUES AFTER CB F13, F14 & F21 WERE PULLED. PERFORMED FIM 27-63-00-810-802-A. FOUND TO BE IN TRANSITORY CONDITION. NO FURTHER DEFECTS NOT
- [SDR JJBA20190703004](https://openairdocs.org/sdr/JJBA20190703004.md): Pump · inoperative · Jul 3, 2019 · N27190 · Emb EMB145XR · Hydraulic Pump (Electric/Engine), Main
  > HYD 2 LOW QTY ON EICAS. R&R HYD PUMP. OPS CHECK SAT. LEAK CHECK GOOD.
- [SDR JJBA201906192015](https://openairdocs.org/sdr/JJBA201906192015.md): Connector · damaged · Jun 12, 2019 · N27190 · Emb EMB145XR · Landing Gear System Wiring
  > FAILED OCF, LANDING GEAR DISAGREEMENT, ALL GEAR WOULD NOT RETRACT. TROUBLESHOT PROXIMITY SWITCHES AND HARNESS. FOUND NLG DOWN LOCK A CONNECTOR P4661 WITH PUSHED PIN. RE-SEATED PIN IN CANNON PLUG. PERFORMED PROXIMITY SWITCH FUNCTIONAL CHECK. OPS CHECK GOOD. PER
- [SDR JJBA2019061105009](https://openairdocs.org/sdr/JJBA2019061105009.md): Yoke · damaged · Jun 5, 2019 · N27190 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > RT PYLON FWD YOKE UPPER FLANGE FASTENER HOLE SHOWS DAMAGE INDICATIONS BY THE HFEC ROTATIVE DRIVE INSPECTION METHOD. COMPLETED INSTALLATION OF FASTENER AT RIGHT PYLON FWD YOKE UPPER FLANGE.
- [SDR JJBA2019061105008](https://openairdocs.org/sdr/JJBA2019061105008.md): Floor Support · corroded · Jun 5, 2019 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FLOOR GUSSET, FOUND THE CENTER OMEGA BEAM HAS MULTIPLE AREAS OF CORROSION FR 59-61. FABRICATED AND INSTALLED OMEGA BEAM REPAIR DOUBLERS ON CENTER OMEGA BEAM AT FR59 AND FR61.
- [SDR JJBA201906031002](https://openairdocs.org/sdr/JJBA201906031002.md): Structure · damaged · Jun 1, 2019 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LEFT SIDEWALL OF THE INTERNAL STRUCTURE HAS ELONGATED HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 05L - 06L WHILE PICKING UP THE RIVET HOLES FOR REPAIR. REPAIRED LEFT SIDEWALL INTERNAL STRUCTURE ELONGATED HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 05L-06L
- [SDR JJBA201906031001](https://openairdocs.org/sdr/JJBA201906031001.md): Sidewall Panel · damaged · Jun 1, 2019 · N27190 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LEFT SIDEWALL OF THE INTERNAL STRUCTURE HAS HOLE (LOWER SIDE) AS MARKED FRAME 61 STRINGER 11L-12L IN A REPAIR DOUBLER AND THE EDGE OF THE SHEAR CLIP. REMOVED, FABRICATED, AND REPLACED EXISTING REPAIR DOUBLER, PLUGGED HOLE AND BLENDED SLIGHT EDGE DAMAGE ON SHEA

Next page: https://openairdocs.org/aircraft/N27190/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 = 'N27190' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N27190/reports

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