# Service difficulty reports: N152CA, cancelled Jan 11, 2001

A list on [N152CA, cancelled Jan 11, 2001](https://openairdocs.org/deregistered/N152CA-2001-01-11.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 · 59 reports

- [SDR COMA0010014](https://openairdocs.org/sdr/COMA0010014.md): Battery · discharged · Jan 25, 2000 · N152CA · Emb EMB120RT · Emergency Lighting
  > AFT SECTION OF CABIN EMERGENCY LIGHTS WERE INOPERABLE. REPLACED THE NR 3 EMERGENCY BATTERY.
- [SDR COMA0010013](https://openairdocs.org/sdr/COMA0010013.md): Warning System · activated · Jan 24, 2000 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP DISAGREE WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. OPERATON OF FLAPS NORMAL.
- [SDR COMA0010010](https://openairdocs.org/sdr/COMA0010010.md): Battery · discharged · Jan 16, 2000 · N152CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTS ARE INOPERABLE ROWS 1-5. REPLACED EMERGENCY BATTERY.
- [SDR COMA0010001](https://openairdocs.org/sdr/COMA0010001.md): Warning System · activated · Dec 30, 1999 · N152CA · Emb EMB120RT · Door Warning System
  > SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND SECURED SIGNLE POINT FUEL SERVICE DOOR.
- [SDR COMA9910162](https://openairdocs.org/sdr/COMA9910162.md): Np Indicator · failed · Oct 9, 1999 · N152CA · Emb EMB120RT · Propeller Indication System
  > DURING TAKEOFF ROLL, THE RIGHT PROPELLER INDICATED 97.6 PERCENT NP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT NP INDICATOR.
- [SDR COMA9910107](https://openairdocs.org/sdr/COMA9910107.md): Sign · broken · Jul 8, 1999 · N152CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPAIRED EXIT SIGN.
- [SDR COMA9910088](https://openairdocs.org/sdr/COMA9910088.md): Batteries · discharged · May 28, 1999 · N152CA · Emb EMB120RT · Emergency Lighting
  > HTS - FLT 5730 - EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. (M)
- [SDR COMA9910085](https://openairdocs.org/sdr/COMA9910085.md): Battery · discharged · May 25, 1999 · N152CA · Emb EMB120RT · Emergency Lighting
  > LAN - FLT 5076 - EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERIES. (M)
- [SDR COMA9910078](https://openairdocs.org/sdr/COMA9910078.md): Actuator · failed · May 10, 1999 · N152CA · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT AT 80 KTS ON TAKEOFF. REPLACED RIGHT INBOARD FLAP ACTUATOR.
- [SDR COMA9910068](https://openairdocs.org/sdr/COMA9910068.md): Warning · activated · Apr 30, 1999 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE, NO DEFECTS FOUND.
- [SDR COMA9810292](https://openairdocs.org/sdr/COMA9810292.md): Bulb · failed · Dec 29, 1998 · N152CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 2A IS INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA9810272](https://openairdocs.org/sdr/COMA9810272.md): Actuator · malfunction · Nov 30, 1998 · N152CA · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT DURING APPROACH. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR.
- [SDR COMA9810258](https://openairdocs.org/sdr/COMA9810258.md): Connector · defective · Nov 6, 1998 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT. REPLACED ACTUATOR WIRNG CONNECTOR JO 365.
- [SDR COMA9810254](https://openairdocs.org/sdr/COMA9810254.md): Battery · discharged · Nov 4, 1998 · N152CA · Emb EMB120RT · Emergency Lighting
  > ROW 1 AND ROW 4 EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.
- [SDR COMA9810194](https://openairdocs.org/sdr/COMA9810194.md): Sign · broken · Sep 14, 1998 · N152CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHT COVER AT 5C IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA9810167](https://openairdocs.org/sdr/COMA9810167.md): Warning · activated · Jul 31, 1998 · N152CA · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLAP SYSTEM WARNING DURING TAKEOFF. COULD NOT DUPLICATE, SYSTEM TEST NORMAL.
- [SDR COMA9810126](https://openairdocs.org/sdr/COMA9810126.md): Battery · discharged · May 21, 1998 · N152CA · Emb EMB120RT · Emergency Lighting
  > FORWARD CABIN EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY BATTERY.
- [SDR COMA9810115](https://openairdocs.org/sdr/COMA9810115.md): Sign · broken · May 10, 1998 · N152CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5A IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA9810111](https://openairdocs.org/sdr/COMA9810111.md): De-Ice Boot · worn · Apr 29, 1998 · N152CA · Emb EMB120RT · Air Intake Anti/De-Ice System
  > RIGHT ENGINE INLET DE-ICE SYSTEM FAILURE DURING CRUISE FLIGHT. REPLACED LEFT AND RIGHT ENGINE INLET DE-ICE BOOTS.
- [SDR COMA9810073](https://openairdocs.org/sdr/COMA9810073.md): Rollers · worn · Mar 23, 1998 · N152CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND INBOARD FLAP ROLLERS.
- [SDR COMA9810041](https://openairdocs.org/sdr/COMA9810041.md): Actuator · malfunction · Feb 6, 1998 · N152CA · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING. REPLACED THE RIGHT HAND NACELLE FLAP ACTUATOR.
- [SDR COMA9710489](https://openairdocs.org/sdr/COMA9710489.md): Press Regulator · malfunction · Dec 5, 1997 · N152CA · Emb EMB120RT · Airfoil Anti/De-ice System
  > LEFT AIR FOIL DE-ICE SYSTEM INOP. REPLACED THE DE-ICE PRESSURE REGULATOR.
- [SDR COMA9710327](https://openairdocs.org/sdr/COMA9710327.md): Battery · discharged · Jul 6, 1997 · N152CA · Emb EMB120RT · Emergency Lighting
  > FORWARD CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHT BATTERY.
- [SDR COMA9710323](https://openairdocs.org/sdr/COMA9710323.md): Channel · worn · Jul 2, 1997 · N152CA · Emb EMB120RT · Wing Miscellaneous Structure
  > LEFT WING FAIRING COMPOSITE HAS SLIGHT DELAMINATION AT EDGE. REPAIRED WING FAIRING IAW SRM.
- [SDR COMA9710297](https://openairdocs.org/sdr/COMA9710297.md): Battery · discharged · May 20, 1997 · N152CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTS FAIL AFTER 5 SECONDS OF USE. REPLACED THE EMERGENCY LIGHT BATTERIES (S/N 1236, 810, AND 956).
- [SDR COMA9710222](https://openairdocs.org/sdr/COMA9710222.md): Rollers · worn · Apr 19, 1997 · N152CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT AFTER TAKEOFF. REPLACED RT OUTBOARD FLAP ROLLERS.
- [SDR COMA9710128](https://openairdocs.org/sdr/COMA9710128.md): Pitchlock Screw · malfunctioned · Feb 11, 1997 · N152CA · Emb EMB120RT · Propeller Feathering/Reversing
  > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR ACTUATOR AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB WAS FOUND DISPLACED.025 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PART TOTAL CYCLES,
- [SDR COMA9710126](https://openairdocs.org/sdr/COMA9710126.md): Connector · loose · Feb 1, 1997 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > WHEN FLAPS EXTENDED, INBOARD FLAPS REMAINED UP AND OUTBOARD FLAPS WENT FULL DOWN. REPAIRED LOOSE WIRE CONNECTOR AT THE FLAP CONTROL UNIT.
- [SDR COMA9710098](https://openairdocs.org/sdr/COMA9710098.md): Flap Contl Unit · malfunction · Jan 31, 1997 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,093.
- [SDR COMA9710091](https://openairdocs.org/sdr/COMA9710091.md): Hinge · broken · Jan 28, 1997 · N152CA · Emb EMB120RT · Landing Gear Doors
  > LT M.L.G. DOORS DO NOT CLOSE PROPERLY. REPLACED BROKEN DOOR HINGE ON LT M.L.G. AFT DOOR.
- [SDR COMA9610422](https://openairdocs.org/sdr/COMA9610422.md): Butt Strap · misdrilled · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK THE FUSELAGE AFT FLOOR SUPPORT STRUCTURE BUTT STRAP AT CARGO DOOR OPENING WAS FOUND TO HAVE MISDRILLED HOLES. THE BUTT STRAP WAS REPAIRED PER AERODESIGN REPORT NR 2139-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610421](https://openairdocs.org/sdr/COMA9610421.md): Joint Sheet · gouged · Dec 23, 1996 · N152CA · Emb EMB120RT · Wing Miscellaneous Structure
  > DURING 2C CHECK, INSPECTION REVEALED THE WING AUX SPAR CENTER SECTION JOINT SHEET DAMAGED BY SCREWS THAT ATTACH THE LOWER FAIRING. THE DAMAGE CONSISTS OF A SMALL GOUGE ALONG THE BOTTOM EDGE, ONE ON THE LEFT SIDE AND ONE ON THE RIGHT SIDE OF THE SHEET. THE SH
- [SDR COMA9610420](https://openairdocs.org/sdr/COMA9610420.md): Butt Strap · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT RT BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610419](https://openairdocs.org/sdr/COMA9610419.md): Sill · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL REPLACED WITH NEW PART PER SRM CHAPT. 51 STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610418](https://openairdocs.org/sdr/COMA9610418.md): Sill · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL CORRODED. SILL WAS REPAIRED PER AERODESIGN REPORT NR 2140-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610417](https://openairdocs.org/sdr/COMA9610417.md): Sill · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES.
- [SDR COMA9610416](https://openairdocs.org/sdr/COMA9610416.md): Sill · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. REPLACED SILL WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610415](https://openairdocs.org/sdr/COMA9610415.md): Butt Strap · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. REPLACED BUTT STRAP WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610414](https://openairdocs.org/sdr/COMA9610414.md): Butt Strap · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610413](https://openairdocs.org/sdr/COMA9610413.md): Butt Strap · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP FOUND CORRODED. BUTT STRAP WAS REPLACED WITH NEW PART PER SRM CHAPT 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610412](https://openairdocs.org/sdr/COMA9610412.md): Sill · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C CHECK FUSELAGE FWD CABIN FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM 51-40, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.
- [SDR COMA9610411](https://openairdocs.org/sdr/COMA9610411.md): Stringer · corroded · Dec 23, 1996 · N152CA · Emb EMB120RT · Fuselage Main, Longeron/Stringer
  > DURING 2C CHECK INSPECTION FOUND CORROSION ON FUSELAGE STRINGER 19L BETWEEN FRAMES 19 AND 20. STRINGER 19L WAS REPAIRED PER AERODESIGN REPORT NR 1990-2, REV.IR DATED 9-15-96.
- [SDR COMA9610405](https://openairdocs.org/sdr/COMA9610405.md): Hydraulic Hose · failed · Dec 17, 1996 · N152CA · Emb EMB120RT · Hydraulic System, Main
  > HYDRAULIC FLUID LEAKING FROM LT LANDING GEAR AREA. REPLACED LEAKING LANDING GEAR ACTUATOR HYDRAULIC HOSE.
- [SDR COMA9610309](https://openairdocs.org/sdr/COMA9610309.md): Flap Contl Unit · malfunction · Oct 17, 1996 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING, INBD FLAPS ARE FAILED. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9610306](https://openairdocs.org/sdr/COMA9610306.md): Flap Selector · malfunction · Oct 15, 1996 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR UNIT.
- [SDR COMA9610301](https://openairdocs.org/sdr/COMA9610301.md): T Section · corroded · Oct 9, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > FOUND FUSELAGE FLOOR SUPPORT STRUCTURE T-SECTION CORRODED IN FWD CABIN AREA. REMOVED CORRODED T-SECTION AND INSTALLED NEW PART PER REPORT NR 2057-1, REV. IR, DATED 10-6-96. AIRCRAFT TOTAL CYCLES, 19,871.
- [SDR COMA9610300](https://openairdocs.org/sdr/COMA9610300.md): Butt Strap · corroded · Oct 9, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > FOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871.
- [SDR COMA9610272](https://openairdocs.org/sdr/COMA9610272.md): Battery · discharged · Sep 3, 1996 · N152CA · Emb EMB120RT · Emergency Lighting
  > AFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088.
- [SDR COMA9610260](https://openairdocs.org/sdr/COMA9610260.md): Circuit Breaker · damaged · Aug 25, 1996 · N152CA · Emb EMB120RT · DC Power Distribution System
  > EMERGENCY BUS LOST POWER, CONTROL BUS INOP, RT ENGINE INSTRUMENTS INOP, COPILOTS EFIS AND COMM RADIO INOP, A LANDING GEAR INDICATION INOP. FOUND BUS BAR CONNECTION TO CIRCUIT BREAKER 0470 LOOSE WITH HEAT DAMAGE TO BREAKER. REPLACED C/B 0470 AND ATTACHING HAR
- [SDR COMA9610224](https://openairdocs.org/sdr/COMA9610224.md): Flap Warning · activated · Jul 11, 1996 · N152CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT WARNING AFTER LANDING. INSPECTED FLAP SYSTEM AND FOUND TO OPERATE NORMALLY. COULD NOT DUPLICATE DISCREPANCY.

Next page: https://openairdocs.org/deregistered/N152CA-2001-01-11/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 = 'N152CA' AND deregistration_id = 'N152CA-2001-01-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N152CA-2001-01-11/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.