# Service difficulty reports: N33182

A list on [N33182](https://openairdocs.org/aircraft/N33182.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 · 90 reports

- [SDR JJBA20260413008](https://openairdocs.org/sdr/JJBA20260413008.md): Amplifier · malfunctioned · Apr 10, 2026 · N33182 · Emb EMB145XR · Emergency Lighting
  > CABIN AND CABIN EMERGENCY LIGHT ON ICU WILL NOT EXTINGUISH. RE-RACKED PA AMP. OPS CHECK OKAY AT THIS TIME. NO FAULTS NOTED.
- [SDR JJBA20260204003](https://openairdocs.org/sdr/JJBA20260204003.md): Fuse · failed · Feb 2, 2026 · N33182 · Emb EMB145XR · Emergency Lighting
  > LH FORWARD OF WING EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW BULB. DID NOT FIX. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY. DID NOT FIX. PUT BACK TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED BAD FUSE ON FWD BATTERY CHARGE ASSEMBLY. REMOVED AND REPLACED LH FWD
- [SDR JJBA20240130063](https://openairdocs.org/sdr/JJBA20240130063.md): Door · lack of lube · Jan 29, 2024 · N33182 · Emb EMB145XR · Passenger/Crew Doors
  > MAIN CABIN DOOR IS BECOMING STUCK WHILE TRYING TO OPEN. LUBED AND OPS CHECK MAIN CABIN DOOR. OPS CHECK GOOD
- [SDR JJBA20231130038](https://openairdocs.org/sdr/JJBA20231130038.md): Unknown · unknown · Nov 27, 2023 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > RF1 LOWER FUSELAGE, CORROSION BTW FR 61-63 LH AND AT STR 19L. LH STRINGER 19L SECTION BTW 61-66 INSTALLED AND STRINGER SPLICE COMPLETED BTW FR 65-66
- [SDR JJBA20231130037](https://openairdocs.org/sdr/JJBA20231130037.md): Unknown · unknown · Nov 27, 2023 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > RF1 EXTERNAL LOWER FUSELAGE, CORROSION BTW FR 61-62A RH AND AT STR 19R. RH STRINGER 19R SECTION BTW FR 61-66 INSTALLED AND STRINGER SPLICE COMPLETED
- [SDR JJBA20231130036](https://openairdocs.org/sdr/JJBA20231130036.md): Unknown · unknown · Nov 27, 2023 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > RF1 EXTERNAL LOWER FUSELAGE, CORROSION SUSPECTED BTW FR 61-63 RH AND AT STR 18R. RH STRINGER 18R SECTION BTW FR 61-66 INSTALLED AND STRINGER SPLICE COMPLETED
- [SDR JJBA20231128034](https://openairdocs.org/sdr/JJBA20231128034.md): Unknown · unknown · Nov 24, 2023 · N33182 · Emb EMB145XR · Cargo/Baggage Doors
  > UNRECORDED REPAIR DOUBLER FOUND ON BAGGAGE DOOR SKIN AROUND HANDLE CUT-OUT. SKIN REPAIRED WITH A DOUBLER BTW STA X22132.6-X22716.2 AND BTW HB#3-4
- [SDR JJBA20231128033](https://openairdocs.org/sdr/JJBA20231128033.md): Unknown · unknown · Nov 24, 2023 · N33182 · Emb EMB145XR · Cargo/Baggage Doors
  > DENT FOUND ON BAGGAGE DOOR SKIN, 7 INCHES FROM FWD SKIN EDGE AND 9.5 INCHES FROM LOWER SKIN EDGE. SKIN REPAIRED WITH A DOUBLER BTW STA X22132.6-X22716.2 AND BTW HB#3-4
- [SDR JJBA20231128032](https://openairdocs.org/sdr/JJBA20231128032.md): Unknown · unknown · Nov 22, 2023 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > CRACKS SUSPECTED (3X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 & BTW STR 3R-9R. AFTER NDT INVESTIGATION, 1 CRACK FOUND, SKIN REPAIRED WITH 1 BUSHING
- [SDR JJBA20231128031](https://openairdocs.org/sdr/JJBA20231128031.md): Unknown · unknown · Nov 21, 2023 · N33182 · Emb EMB145XR · Navigation System
  > RA #2 FWD ANTENNA BASE FOUND CORRODED. SKIN REPAIRED WITH A DOUBLER. CORROSION LEVEL 1
- [SDR JJBA20231127024](https://openairdocs.org/sdr/JJBA20231127024.md): Unknown · unknown · Nov 20, 2023 · N33182 · Emb EMB145XR · Fuselage Structure (General)
  > CF1 EXTERNAL UPPER FUSELAGE SCRATCHES FOUND UNDERNEATH TOP TCAS ANTENNA. SKIN REPAIRED WITH A DOUBLER BTW FR 16-17 AND BTW STR 1L-1R UNDER TCAS ANTENNA
- [SDR JJBA20231121014](https://openairdocs.org/sdr/JJBA20231121014.md): Unknown · unknown · Nov 17, 2023 · N33182 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CF1, CRACK FOUND ON ANGLE (2X) UNDER MIDDLE GUSSET BTW FR 20-22, ON FLOOR STRUCTURE AREA. REPLACED ANGLE (2X)
- [SDR JJBA20231121013](https://openairdocs.org/sdr/JJBA20231121013.md): Unknown · unknown · Nov 17, 2023 · N33182 · Emb EMB145XR · Fuselage Main, Frame
  > FWD FUSE II, FRAME 10 STR 9L ANGLE FOUND CRACKED. FWD FUSE II, FR10 STR 9L ANGLE REPLACED BY NEW ANGLE
- [SDR JJBA20231127029](https://openairdocs.org/sdr/JJBA20231127029.md): Unknown · unknown · Nov 16, 2023 · N33182 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > IN LH ENG PYLON, LH PRECOOLER STRUCTURE FWD BRACKET IS CRACKED. REPLACED
- [SDR JJBA20231127028](https://openairdocs.org/sdr/JJBA20231127028.md): Unknown · unknown · Nov 16, 2023 · N33182 · Emb EMB145XR · Fuselage Structure (General)
  > RF2, DENT FOUND ON LH AFT DUAL STRAKES INBOARD SIDE, 1" FWD OF END RIB FR 81. DENT IS ACCEPTED
- [SDR JJBA20231127027](https://openairdocs.org/sdr/JJBA20231127027.md): Unknown · unknown · Nov 16, 2023 · N33182 · Emb EMB145XR · Fuselage Structure (General)
  > NLG W/WELL, CRACK FOUND ON NLG UP-LOCK AFT CROSSBEAM. REPLACED
- [SDR JJBA20231127026](https://openairdocs.org/sdr/JJBA20231127026.md): Unknown · unknown · Oct 24, 2023 · N33182 · Emb EMB145XR · Wing Structure
  > RH OUTBD FLAP SHOUD, OUTBD HINGE FOUND CRACKED. NEW PART INSTALLED
- [SDR JJBA20231127025](https://openairdocs.org/sdr/JJBA20231127025.md): Unknown · unknown · Oct 24, 2023 · N33182 · Emb EMB145XR · Fuselage Structure (General)
  > CF1, CRACKS (3X) FOUND ON LH OMEGA BEAM #1 FLOOR STRUCTURE BTW FR 18-24. REPLACED
- [SDR JJBA20231127023](https://openairdocs.org/sdr/JJBA20231127023.md): Unknown · unknown · Oct 24, 2023 · N33182 · Emb EMB145XR · Fuselage Structure (General)
  > CF1, CRACK FOUND ON FUEL RELAY AVIONIC BOX RH FWD SUPPORT BTW FR 15-16 AND BTW STR 7R-9R. CF1, ON FUEL RELAY AVIONIC BOX RH FWD SUPPORT BTW FR 15-16 AND BTW STR 7R-9R REPLACED
- [SDR JJBA20231127022](https://openairdocs.org/sdr/JJBA20231127022.md): Unknown · unknown · Oct 24, 2023 · N33182 · Emb EMB145XR · Wing Structure
  > LH OUTBD FLAP SHROUD, OUTB HINGE EYELET FOUND CRACKED. LH OUTBD FLAP SHROUD OUTBD HINGE REPLACED
- [SDR JJBA20231121015](https://openairdocs.org/sdr/JJBA20231121015.md): Unknown · unknown · Oct 24, 2023 · N33182 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > CF1, FRAME 16, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. ON CF1, FRAME 16, RH SHEAR CLIP REPLACED BTW STR 15R-16R
- [SDR JJBA20230710006](https://openairdocs.org/sdr/JJBA20230710006.md): Unknown · unknown · Jul 6, 2023 · N33182 · Emb EMB145XR · Standard Practices/Structures
  > MAIN CABIN DOOR HARD TO OPEN. LUBED MCD & OPS CHECKED GOOD
- [SDR JJBA20230103003](https://openairdocs.org/sdr/JJBA20230103003.md): Light · detached · Jan 3, 2023 · N33182 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHTING STRIP ON THE FLOOR BY SEAT 1A IS DETACHED. RESECURED 1A LIGHT STRIP.
- [SDR JJBA20220825027](https://openairdocs.org/sdr/JJBA20220825027.md): None · out of adjust · Aug 24, 2022 · N33182 · Emb EMB145XR · Landing Gear System
  > L/G AIR GROUND FAIL AFTER TAKE OFF. UNABLE TO RETRACT L/G ADJUSTED NLG TORQUE LINK PROX SWITCH. CONDUCTED GEAR RETRACTION AND EXTENSION. OPS CHECK SAT.
- [SDR JJBA20220514025](https://openairdocs.org/sdr/JJBA20220514025.md): None · inoperative · May 14, 2022 · N33182 · Emb EMB145XR · Trailing Edge Flap Control System
  > FLAP FAIL WHEN SELECTING FLAPS 9 ON APPROACH. REMOVED AND REPLACED FECU AND FLAP DRIVE UNIT.
- [SDR JJBA20211201002](https://openairdocs.org/sdr/JJBA20211201002.md): None · none · Dec 1, 2021 · N33182 · Emb EMB145XR · Lighting System
  > FWD MOST EMERGENCY LIGHT STRIP UNSECURE. RESECURED FWD EMERGENCY LIGHT STRIP
- [SDR JJBA20210913032](https://openairdocs.org/sdr/JJBA20210913032.md): Skin · cracked · Sep 13, 2021 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > RF 1, BTW FR 77-79 BTW STR 3R-9R, CRACK SUSPECTED AROUND FASTENERS. RF1, BTW FR77-79 BTW 3R, 9R PAINT REMOVED AROUND FASTENERS FOR INVESTIGATION CRACK CONFIRMED. AT FR 79 AND STR 4R 3 CRACKS FOUND AND REPAIRED WITH DOUBLER
- [SDR JJBA2021090830024](https://openairdocs.org/sdr/JJBA2021090830024.md): Frame · corroded · Aug 30, 2021 · N33182 · Emb EMB145XR · Fuselage Main, Frame
  > CENTER FUSE IV UNDER FLOOR, FRAME 59 CORRODED. CENTER FUSE IV UNDERFLOOR FR59 HAS EXFOLIATED CORROSION AND IS OUT OF LIMITS. PERFORMED CUT OUT FRAME SECTION BTW STR 20L-20R FRABRICATED U FRAME SECTION FROM 7075-0 0.032" AND FABRICATED QTY 2 FRAME SPLICE REPAIR
- [SDR JJBA2021090830023](https://openairdocs.org/sdr/JJBA2021090830023.md): Yoke · cracked · Aug 30, 2021 · N33182 · Emb EMB145XR · Engine Mount Section
  > 2X CRACK FOUND ON PYLON YOKES UPPER FLANGE AT 2X HOLE LOCATION. INSTALLED LH AND RH BUSHINGS AND PERFORMED COLD WORK BUSHING HOLES THEN REAMED FULL SIZE AND INSTALLED NEW JO-BOLTS AND WASHERS WET INSTALLED AND RESTORED FINISH ALL FASTENERS.
- [SDR JJBA20210116016](https://openairdocs.org/sdr/JJBA20210116016.md): Control Unit · inoperative · Jan 16, 2021 · N33182 · Emb EMB145XR · Trailing Edge Flap Control System
  > FLAP FAIL 0-9 DEGREES ON APPROACH. PERFORMED GVI OF INBOARD AND OUTBOARD FLAPS. FOUND DAMAGE TO ALL FLAP TRACKS. SUSPECT DAMAGE TO FLAP DRIVE SHAFTS. FOUND FECU CONNECTOR P1003 LOOSE AND LT FLAP VELOCITY SENSOR INTERMITTENT AND CONNECTOR HAS SOME CORROSION
- [SDR JJBA20210116015](https://openairdocs.org/sdr/JJBA20210116015.md): Flap System · malfunctioned · Jan 16, 2021 · N33182 · Emb EMB145XR · Trailing Edge Flap Control System
  > FLAP FAIL 0-9 DEGREES ON APPROACH. OPERATIONAL CHECK OF FLAPS. INSPECTED FVS. NO DEFECTS NOTED.
- [SDR JJBA20210111009](https://openairdocs.org/sdr/JJBA20210111009.md): Warning Message · false activation · Jan 11, 2021 · N33182 · Emb EMB145XR · Trailing Flap Position Indicating System
  > EICAS FLAP FAIL ON FINAL APPROACH. FLAP POS SHOWING 1. CHECKED ELEC CONNECTORS ON FECU, VEL SENSORS, AND FPRU. PERFORMED GVI ON FLAP MECH LINE. OPERATIONS CHECK SATISFACTORY, NO DEFECTS FOUND.
- [SDR JJBA201912164002](https://openairdocs.org/sdr/JJBA201912164002.md): Terminal · loose · Dec 14, 2019 · N33182 · Emb EMB145XR · Light System Wiring
  > SERVICE DOOR EXTERNAL EMERGENCY LIGHT FLICKERS. R&R BROKEN SERVICE DOOR BONDING JUMPER AND RESECURED GROUND TERMINAL OF THE SERVICE DOOR EMERGENCY LIGHT LAMP. OPS CHECK SAT, FLICKERING STOPPED.
- [SDR JJBA201910075004](https://openairdocs.org/sdr/JJBA201910075004.md): Light · inoperative · Oct 5, 2019 · N33182 · Emb EMB145XR · Emergency Lighting
  > MAIN DOOR HINGE EMERGENCY LIGHT INOPERATIVE. R&R MAIN DOOR HINGE EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20190919005](https://openairdocs.org/sdr/JJBA20190919005.md): Skin · dented · Sep 19, 2019 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FUSELAGE CF1 14" AFT OF MAIN CABIN DOOR HAS DENT/GOUGE IN AREA OF PREVIOUS DENT. PERMANENT REPAIR IS DUE WITHIN 50 CYCLES.
- [SDR JJBA20190521010](https://openairdocs.org/sdr/JJBA20190521010.md): Controller · inoperative · May 21, 2019 · N33182 · Emb EMB145XR · Cabin Pressure Controller
  > LOST PRESSURIZATION AT 30,000 FT IN AUTOMATIC MODE. AS DESCENDING TO 30,000 FEET AND AFTER LEVELING OFF, PRESSURIZATION BEGAN A SLOW CLIMB TO ABOUT 14,000 USING QRH DESCENDED TO 10,000 AND ALLOWED PILOT TO REGAIN PRESSURIZATION CONTROL USING MANUAL MODE. O2 MA
- [SDR JJBA2019021309009](https://openairdocs.org/sdr/JJBA2019021309009.md): Light · damaged · Feb 9, 2019 · N33182 · Emb EMB145XR · Emergency Lighting
  > AFT RIGHT HAND EMERGENCY FLOOR LIGHTING IS DAMAGED. ALSO, ALL PLASTIC COVERS NEED TO BE CLEANED OR REPLACED PER CUSTOMER. REMOVED AND REPLACED AFT RIGHT HAND EMERGENCY FLOOR LIGHTING. ALSO, CLEANED ALL PLASTIC COVERS PER CUSTOMER.
- [SDR JJBA2019021309008](https://openairdocs.org/sdr/JJBA2019021309008.md): Floor Support · corroded · Feb 9, 2019 · N33182 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > OMEGA BEAM AT Y=0 AND FR 20 CORRODED. REMOVED AND REPLACED ENTIRE OMEGA BEAM AT Y=0 AND FR 20
- [SDR JJBA2019021307007](https://openairdocs.org/sdr/JJBA2019021307007.md): Floor Support · corroded · Feb 7, 2019 · N33182 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > OMEGA BEAM REPAIR AT -Y=479.0 AND FR 20 CORRODED. INSTALLED NEW REPAIR PARTS EXTERNAL ANGLE, FILLER AND 2 EA SHIMS.
- [SDR JJBA2019021304006](https://openairdocs.org/sdr/JJBA2019021304006.md): Door Frame · corroded · Feb 4, 2019 · N33182 · Emb EMB145XR · Fuselage Main, Structure
  > CORROSION ON LOWER SERVICE DOOR FRAME CHANNEL AROUND 3 EA FASTENER HOLES (MARKED). REMOVED AND REPLACED SERVICE DOOR LOWER BEAM.
- [SDR JJBA2019021304005](https://openairdocs.org/sdr/JJBA2019021304005.md): Skin · dented · Feb 4, 2019 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED BETWEEN FR 73 AND FR 74, STR 18R - 21R MARKED WITH GREEN DOT. COMPLIED WITH ETD 2019-145-012414 FOR PERMANENT ACCEPTANCE/REPAIR OF DENT/DAMAGE ON FUSELAGE SKIN BETWEEN FR 73 AND 74 AND STR 18R AND 21R. THIS REPAIR DOES NOT ADVERSELY AFFECT A FA
- [SDR JJBA201902131052](https://openairdocs.org/sdr/JJBA201902131052.md): Skin · dented · Jan 31, 2019 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BELOW STGR 11L BETWEEN FR 19 AND 20. EVALUATED (2 EACH) SKIN DENTS BELOW STGR 11L BETWEEN FR 19 & 20. DENT (1) LOCATED AT FR 19 + 11" HAS AREA = 2.75"L X 1.65"W X.015"H, DENT (2) LOCATED AT FR 19 + 14.5" = 2.5"L X 1.25"W X.007"H, BOTH AR
- [SDR JJBA201902131051](https://openairdocs.org/sdr/JJBA201902131051.md): Skin · dented · Jan 31, 2019 · N33182 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A PROTRUDING DENT BETWEEN STGR 17R & 18R; BETWEEN FR 22 & 23. EVALUATED PROTRUDING DENT BETWEEN STGR 17R & 18R AND FR 22 & 23. AREA =.048"L X.43"W X.013"H, IS WITHIN LIMITS AND NO ACTION REQUIRED.
- [SDR JJBA2018061907001](https://openairdocs.org/sdr/JJBA2018061907001.md): Unknown · smoke · May 7, 2018 · N33182 · Emb EMB145XR · Air Distribution System
  > SMOKE AND FUMES IN THE CABIN, FUMES IN COCKPIT SHORTLY AFTER TAKEOFF. R & R THE NR 1 HEAT EXCHANGER. OPS CHECKED GOOD. LEAK CHECK GOOD. FOUND GRATE ASSEMBLY DAMAGED. R & R THE GRATE ASSEMBLY. OPS AND LEAK CHECKED GOOD. FOUND THE NR 1 ACM TO BE SEIZED. AC
- [SDR JJBA201804295008](https://openairdocs.org/sdr/JJBA201804295008.md): Coupling · damaged · Apr 25, 2018 · N33182 · Emb EMB145XR · Pneumatic Distribution System
  > DURING CLIMB, BETWEEN FL200 FL280, AN EICAS WARNING MESSAGE FOR ICE CON A/I INOPERATIVE. WHILE RUNNING THE CHECKLIST, THE MESSAGE DISAPPEARED. A FEW SECONDS LATER THE EICAS CAUTION MESSAGE E2N A/ICE FAIL, THEN NO ICE A/ICE ON APPEARED. WHILE RUNNING CHECK
- [SDR JJBA20171216011](https://openairdocs.org/sdr/JJBA20171216011.md): Battery Pack · discharged · Dec 16, 2017 · N33182 · Emb EMB145XR · Emergency Lighting
  > THREE CABIN EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERIES AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. OPS CHECK GOOD.
- [SDR JJBA20171208009](https://openairdocs.org/sdr/JJBA20171208009.md): Receptacle · damaged · Dec 8, 2017 · N33182 · Emb EMB145XR · Fuselage Main, Structure
  > DAMAGE TO EXTERNAL POWER RECEPTACLE AND SURROUNDING STRUCTURE. REMOVED EXTERNAL POWER RECEPTACLE IAW EMB 145 AMM 24-40-01. REMOVED EXTERNAL POWER RECEPTACLE HOUSING IAW EMB 145 SRM 51-40-02. PERFORMED PERMANENT REPAIR IAW CONNUTAIR TECHNICAL ORDER E145-5311-20
- [SDR JJBA20171206003](https://openairdocs.org/sdr/JJBA20171206003.md): Light · inoperative · Dec 6, 2017 · N33182 · Emb EMB145XR · Emergency Lighting
  > ENTRY DOOR EMERGENCY LIGHT INOP. R&R LIGHT BULB. OPS CHECK SAT.
- [SDR JJBA20170925033](https://openairdocs.org/sdr/JJBA20170925033.md): Bulb · inoperative · Sep 25, 2017 · N33182 · Emb EMB145XR · Emergency Lighting
  > AFT CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.
- [SDR JJBA20170320012](https://openairdocs.org/sdr/JJBA20170320012.md): Bulb · inoperative · Mar 20, 2017 · N33182 · Emb EMB145XR · Emergency Lighting
  > GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N33182/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 = 'N33182' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33182/reports

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