# Service difficulty reports: N600BP

A list on [N600BP](https://openairdocs.org/aircraft/N600BP.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 · 126 reports

- [SDR HNAA2021050300164](https://openairdocs.org/sdr/HNAA2021050300164.md): Tat Probe · malfunctioned · Apr 30, 2021 · N600BP · Emb EMB145LR · Outside Air Temperature Indicator/Sensor
  > IN CRUISE TAT 2 INOPERATIVE IN EICAS. NO NOTED INDICATION ISSUES. R & R TAT 2 SENSOR IAW AMM 34 15 03. OPS CHECKED GOOD. R & R RELAY K0494 PER AMM 20 13 02. OPS CHECK GOOD. OK FOR SERVICE
- [SDR HNAA2020090900254](https://openairdocs.org/sdr/HNAA2020090900254.md): Wheel · failed · Sep 9, 2020 · N600BP · Emb EMB145LR · Wheel/Ski/Float
  > ABNORMAL NOISE AND ODOR FROM NOSE WHEEL AREA DURING TAKEOFF ROLL. MAINTENANCE R& R LT AND RT NOSE WHEEL ASSY, I/A/W 32-49-05. OK FOR SERVICE, PCS.
- [SDR HNAA2020080300241](https://openairdocs.org/sdr/HNAA2020080300241.md): Duct · blown · Jul 31, 2020 · N600BP · Emb EMB145LR · Cabin Cooling System
  > ON TAKE OFF 2 LOUD POPS WERE HEARD IN CABIN BETWEEN RIGHT E-EXIT AND AFT BULKHEAD, FOLLOWED BY A BLEED 1 LEAK ON EICAS. AT 10,000 FT CABIN WAS LOSING PRESSURIZATION. MAINTENANCE: UPON INSPECTION OF PACK 2 DUCTS, FOUND BLOWN OFF LINE. REPLACED RUBBER SEAL AND C
- [SDR HNAA2020022600079](https://openairdocs.org/sdr/HNAA2020022600079.md): Trim System · inoperative · Feb 22, 2020 · N600BP · Emb EMB145LR · Stabilizer Position Indicating
  > PITCH TRIM MAIN INOP. BACK-UP OPS NORMAL.....FIX: TRANSCRIBED TO WORK PACKAGE SEQ 1 DATED 22FEB20. R&RD HSA(HORIZ STAB ACTUATOR) IAW AMM 27-40-02. PERFORMED HSA ADJ/TEST IAW 27-40-02-700-801-A. OKAY FOR SERVICE.
- [SDR HNAA2020021700066](https://openairdocs.org/sdr/HNAA2020021700066.md): Trim System · malfunctioned · Feb 15, 2020 · N600BP · Emb EMB145LR · Stabilizer Position Indicating
  > PDIS 600 27-41 2110041 15FEB20 PHL CLOSE PITCH TRIM MAIN INOP ON EICAS DURING CLIMB WITH AUTO PILOT ENGAGED FACT 15FEB20 14:27 PHL RESET PITCH TRIM 1/ PITCH TRIM 2 CB PER FIM 27-43-00-810-801-A BLOCK 1. PERFORMED HORIZON
- [SDR HNAA2020011700019](https://openairdocs.org/sdr/HNAA2020011700019.md): Pump · leaking · Jan 15, 2020 · N600BP · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main
  > HYD SYS 1 FLUID LOSS IN FLIGHT....FIX:FOUND #1ENG DRIVEN HYD PUMP LEAKING OUT DRAIN TUBE. R&RD #1ENG DRIVEN HYD PUMP IAW 29-10-03-000-801-A AND 29-10-03-400-801A,OPS CHECK LEAK CHECK GOOD.OK FOR SERVICE
- [SDR HNAA2018081300190](https://openairdocs.org/sdr/HNAA2018081300190.md): Display · malfunctioned · Aug 10, 2018 · N600BP · Emb EMB145LR · Flight Environment Data
  > FIRST OFFICER`S ALTITUDE INDICATOR ON THE PFD SHOWED A RED X AND SPEED BUGS ON SPEED TAPE. DISAPPEARED AT VR SELECTED ADC 1 ON THE FIRST OFFICER`S REV PNL, ALL INDICATIONS NORMAL. R & R THE PFD 2 IAW AMM 34-22-01. OPS CHECKED GOOD. PERFORMED ADC SELF TEST
- [SDR HNAA2018072000161](https://openairdocs.org/sdr/HNAA2018072000161.md): Window · open · Jul 19, 2018 · N600BP · Emb EMB145LR · Flight Compartment Windows
  > CAPT DV WINDOW OPENED IN FLIGHT SHORTLY AFTER TAKEOFF. WINDOW WOULD NOT REMAIN CLOSED WITHOUT ASSISTANCE. INSPECTED CAPTAINS STORM WINDOW TRACK AND SEALS. NO DEFECTS NOTED. PERFORMED OPS CHECK IAW AMM TASK 56-11-00-700-801-A. OPS CHECK GOOD REQUIRES EVAL FLIGH
- [SDR HNAA2018052500113](https://openairdocs.org/sdr/HNAA2018052500113.md): Unknown · odor · May 10, 2018 · N600BP · Emb EMB145LR · Air Distribution System
  > ACRID SMOKE ODOR IN THE FLIGHT DECK AND FORWARD CABIN. NO VISUAL SIGNS OF SMOKE. VISUALLY INSPECTED AVIONICS NOSE BAY AND AROUND WINDSHIELDS, FOUND NO EVIDENCE OF BURNING. DURING GROUND RUN FOR RADAR, NO EVIDENCE OF SMOKE. OK FOR SERVICE.
- [SDR HNAA2018041100080](https://openairdocs.org/sdr/HNAA2018041100080.md): Unknown · odor · Apr 10, 2018 · N600BP · Emb EMB145LR · Air Distribution System
  > PASSENGER REPORTED POSSIBLE ELECTRICAL ODOR IN CABIN. MX UNABLE TO DUPLICATE DISCREPANCY. NO ELECTRICAL ODOR PRESENT IN ACFT AT THIS TIME. NO OBVIOUS DEFECTS NOTED, OK FOR SERVICE.
- [SDR HNAA2017101600350](https://openairdocs.org/sdr/HNAA2017101600350.md): Engine · fire · Oct 15, 2017 · N600BP · Emb EMB145LR · Engine (Turbine/Turboprop)
  > GROUND CREW REPORTED A NR 1 ENGINE FIRE AT EXHAUST NOZZLE DURING TAXI. CREW REPORTED THE ENGINE WAS JUST PREVIOUSLY SHUTDOWN AND NO ABNORMAL INDICATIONS OR MESSAGE VIEWED. INSPECTED FOR FIRE EVIDENCE AND DAMAGE. NONE FOUND. GROUND RAN THE ENGINE. SHUTDO
- [SDR HNAA2017100200343](https://openairdocs.org/sdr/HNAA2017100200343.md): Unknown · unknown · Sep 29, 2017 · N600BP · Emb EMB145LR · Flight Control System
  > AT 100 KNOTS DURING TAKE OFF, AIRCRAFT ABRUPTLY YAWED TO THE LEFT. COMPLIED WITH GVI ON NLG AND MLG. NO DEFECTS FOUND. ALL TIRE PRESSURES WERE GOOD. OK FOR SERVICE.
- [SDR HNAA2017090700301](https://openairdocs.org/sdr/HNAA2017090700301.md): Light · inoperative · Sep 1, 2017 · N600BP · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 17 INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-50-08-000/400-802-A, OPS CHECKED GOOD.
- [SDR HNAA2017082100279](https://openairdocs.org/sdr/HNAA2017082100279.md): Engine · fire · Aug 18, 2017 · N600BP · Emb EMB145LR · Engine (Turbine/Turboprop)
  > GATE AGENT NOTICED FLAMES AND SMOKE EMINATING FROM THE NR 1 ENGINE WHILE ENGINE WAS SHUTDOWN. INSPECTED AND NO DAMAGE NOTED. GVI ENGINE INLET AND EXIT AND NACELLE AREA. NO DAMAGE NOTED IAW MM 05-50-00. OK FOR SERVICE.
- [SDR HNAA2016120900381](https://openairdocs.org/sdr/HNAA2016120900381.md): Warning System · false activation · Dec 9, 2016 · N600BP · Emb EMB145 · Pneumatic Indicating System
  > HS VLV CAUTION ILLUMINATED AFTER ENGINE START. GROUND RAN BOTH ENGINE. PERFORMED 1 AND 2 ENGINE HSV FUNCTION TEST IN ACCORDANCE WITH MM 36-11-02. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2016121200387](https://openairdocs.org/sdr/HNAA2016121200387.md): Valve · failed · Dec 8, 2016 · N600BP · Emb EMB145LR · Pneumatic Distribution System
  > AFTER ENGINE START, HS VALVE 1 FAILED. R & R THE NR 1 HSV AND PRESSURE SWITCH IAW AMM 36-11-02. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR HNAA2016112100354](https://openairdocs.org/sdr/HNAA2016112100354.md): Warning Light · false activation · Nov 21, 2016 · N600BP · Emb EMB145LR · Central Warning
  > DURING TAKEOFF, EICAS CAUTION MESSAGE HS VALVE ILLUMINATED, NR 1 ENGINE N2 WAS ABOVE 80%. MESSAGE EXTINGUISHED AFTER REJECTED TAKEOFF AND THRUST LEVERS AT IDLE. GROUND RAN AIRCRAFT. PERFORMED HIGH STAGE VALVE FUNCTION TEST IAW MM 36-11-02-700-801-A/500. OP
- [SDR HNAA2016101400318](https://openairdocs.org/sdr/HNAA2016101400318.md): Warning Light · false activation · Oct 14, 2016 · N600BP · Emb EMB145LR · Airfoil Anti/De-ice System
  > DURING ICE PROTECTION TEST IN FLIGHT, STAB ANTI-ICE FAILED APPEARS ON EICAS. TROUBLESHOT IAW FIM 30-12-00-810-805-A. PERFORMED OPS CHECKED ON ANTI-ICE SYSTEM IAW MM 30-00-00 OPS CHECKED GOOD. FOUND TO BE TRANSITORY CONDITION.
- [SDR SIMA20160725005](https://openairdocs.org/sdr/SIMA20160725005.md): Valve · corroded · Jul 25, 2016 · N600BP · Emb EMB145LR · Waste Disposal System
  > TOILET WASTE VALVE SUPPORT BUCKET IS CORRODED. REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT BUCKET IAW SRM 51-40-02
- [SDR SIMA20160720006](https://openairdocs.org/sdr/SIMA20160720006.md): Wire · broken · Jul 20, 2016 · N600BP · Emb EMB145LR · Light System Wiring
  > NR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20160720004](https://openairdocs.org/sdr/SIMA20160720004.md): Floor Support · cracked · Jul 20, 2016 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT OMEGA BEAM IS CRACKED AT NUTPLATE HOLE ABOVE FRAME 69. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2199
- [SDR SIMA20160720007](https://openairdocs.org/sdr/SIMA20160720007.md): Wire · broken · Jul 20, 2016 · N600BP · Emb EMB145LR · Light System Wiring
  > LEFT NR 1 EMERGENCY LIGHT CONNECTION BROKEN. REPAIRED THE WIRE IAW SWPM 20-50-00
- [SDR SIMA20160720005](https://openairdocs.org/sdr/SIMA20160720005.md): Skin · damaged · Jul 20, 2016 · N600BP · Emb EMB145LR · Rudder, Plate/Skin
  > RUDDER LOWER RT SIDE TRAILING EDGE SKIN HAS A BLEND-OUT AREA. ACCOMPLISHED PERMANENT REPAIR OF THE RUDDER IAW ERS-EM-55MR-441
- [SDR SIMA20160712002](https://openairdocs.org/sdr/SIMA20160712002.md): Frame · corroded · Jul 12, 2016 · N600BP · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 65 IS CORRODED BELOW CARGO DOOR GUIDE PLATE. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20160417002](https://openairdocs.org/sdr/SIMA20160417002.md): Inverter · inoperative · Apr 17, 2016 · N600BP · Emb EMB145LR · Emergency Lighting
  > THREE AFT EMER FLOOR LIGHT STRIPS INOPERATIVE. R & R NR 6 EMER LIGHT DC & AC INVERTER. OPERATIONS CHECKED GOOD FOR ALL EMER FLOOR LIGHT STRIPS IAW AMM 33-50-11.
- [SDR SIMA20160414005](https://openairdocs.org/sdr/SIMA20160414005.md): Light · inoperative · Apr 14, 2016 · N600BP · Emb EMB145LR · Emergency Lighting
  > EMERGENCY FLOOR PROXIMITY LIGHT STRIP, FOURTH FROM FRONT INOPERATIVE. DEFERRED IAW MEL 33-30. R & R EMER FLOOR PROXIMITY LIGHT STRIP, 4TH FROM FRONT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.
- [SDR SIMA20160401003](https://openairdocs.org/sdr/SIMA20160401003.md): Transducer · failed · Apr 1, 2016 · N600BP · Emb EMB145LR · Brake Anti-Skid Section
  > ABORTED TAKEOFF AT 80KTS. BRAKE DEGRADED MSG & AT THE SAME TIME ACFT SWERVED TO THE LEFT. R & R NR 4 WHEEL SPEED TRANSDUCER IAW AMM 32-41-03. PERFORMED FUNCTIONAL CHECK OF THE MAIN BRAKE SYS IAW AMM TASK 32-41-00-700-801. CHECK IS GOOD.
- [SDR SIMA20160215002](https://openairdocs.org/sdr/SIMA20160215002.md): Door · lack of lube · Feb 15, 2016 · N600BP · Emb EMB145LR · Passenger/Crew Doors
  > FLIGHT ATTENDANTS REPORTS THE MAIN CABIN DOOR NOT OPEN OR CLOSE EASILY. CLEANED & LUBRICATED MAIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20160120007](https://openairdocs.org/sdr/SIMA20160120007.md): Structure · cracked · Jan 20, 2016 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CRACK AT RIVET BELOW ACCESS PANEL 113AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.
- [SDR SIMA20160120006](https://openairdocs.org/sdr/SIMA20160120006.md): Structure · cracked · Jan 20, 2016 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CRACK AT RIVET BELOW ACCESS PANEL 114AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.
- [SDR SIMA20160120005](https://openairdocs.org/sdr/SIMA20160120005.md): Uplock · failed · Jan 20, 2016 · N600BP · Emb EMB145LR · Landing Gear Retraction/Extension System
  > UNUSUAL THUMPING NOISE COMING FROM UNDERNEATH COCKPIT AREA. HAPPENED ON TWO SEPARATE TIMES WITH VIBRATION FELT BY BOTH PILOTS. REMOVED AND REPLACED NLG UPLOCK BOX IAW AMM 32-33-07. REMOVED AND REPLACED HARNESS TO NLG UPLOCK BOX FOR INTERNAL SHORT IAW SWPM 2
- [SDR SIMA20160107002](https://openairdocs.org/sdr/SIMA20160107002.md): Inverter · inoperative · Jan 7, 2016 · N600BP · Emb EMB145LR · Emergency Lighting
  > FOUND FLOOR STRIPS NR 2 AT NR 3 NOT WORKING. R & R NR 3 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151225003](https://openairdocs.org/sdr/SIMA20151225003.md): Regulator Valve · failed · Dec 25, 2015 · N600BP · Emb EMB145LR · Airfoil Anti/De-ice System
  > ANTI-ICE FAIL FOLLOWED BY ANTI-ICE COND. ANTI-ICE INOPERATIVE, BUT ALL VLVS INDICATED OPEN. MSG CLEARED & SYS WORKED MANUALLY WITHOUT FURTHER ISSUES. TRANSFERRED TO NRWC 600-ORD-02595, REF NRWC 600-ORD-02595. R & R RT PRESS REGULATOR VLV IAW AMM 21-31-05.
- [SDR SIMA20151103002](https://openairdocs.org/sdr/SIMA20151103002.md): Unknown · odor · Nov 3, 2015 · N600BP · Emb EMB145LR · Air Distribution System
  > STRONG ELEC BURNING ODOR THROUGHOUT ACFT, WHILE TAXING UP TO GATE. PERFORMED GVI OF ALL AVIONICS COMPARTMENTS, GVI OF MAIN CABIN AREA, GVI OF MAIN CABIN LIGHTS, GVI OF GALLEY AREA, GVI OF COCKPIT AREA & OPERATED BOTH PACKS IAW AMM 21-51-00. RAN ENG AT IDLE W
- [SDR SIMA20151001002](https://openairdocs.org/sdr/SIMA20151001002.md): Flashlight · inoperative · Oct 1, 2015 · N600BP · Emb EMB145LR · Emergency Equipment
  > CAPTAINS FLASH LIGHT QUIT WORKING. R & R CAPTAINS FLASH LIGHT ASSEMBLY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150915001](https://openairdocs.org/sdr/SIMA20150915001.md): Light · inoperative · Sep 15, 2015 · N600BP · Emb EMB145LR · Emergency Lighting
  > RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. R & R RT FWD OVERWING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.
- [SDR SIMA20150822001](https://openairdocs.org/sdr/SIMA20150822001.md): Radio Altimeter · failed · Aug 23, 2015 · N600BP · Emb EMB145LR · Ground Proximity System
  > ON CLIMB OUT RA SHOWED 25 FT GREEN WITH MIN BOX SHOWING & GND INDICATION UNDER ALTITUDE. NUMEROUS AURAL WARNINGS & MASTER CAUTIONS INCLUDING BANK ANGLE, PULL UP, LG, SINK RATE GND PROX, HOWEVER NO MSG ON EICAS. TRANSFERRED TO NRWC 600-DFW-02420. REFERENCE N
- [SDR SIMA20150819004](https://openairdocs.org/sdr/SIMA20150819004.md): Light · inoperative · Aug 19, 2015 · N600BP · Emb EMB145LR · Emergency Lighting
  > RIGHT FWD EMER WING LIGHT INOPERATIVE. R & R FWD WING EMER LIGHT IAW AMM 33-50-07.
- [SDR SIMA20150330002](https://openairdocs.org/sdr/SIMA20150330002.md): Mechanism · lack of lube · Mar 30, 2015 · N600BP · Emb EMB145LR · Passenger/Crew Doors
  > MAIN CABIN DOOR EXCEPTIONALLY DIFFICULT TO OPEN & CLOSE. LUBRICATED ACTUATING & LOCKING MECHANISM ON MAIN CABIN DOOR IAW AMM 52-18-00. OPENING & CLOSING GOOD IAW AMM 52-18-00-820-801A.
- [SDR SIMA20150319004](https://openairdocs.org/sdr/SIMA20150319004.md): Door · scratched · Mar 19, 2015 · N600BP · Emb EMB145LR · Passenger/Crew Doors
  > PASSENGER DOOR SCRATCHED & GOUGED ON LOWER TE. TRANSFERRED TO AML PAGE 3740390 ITEM 1. SATISFACTORILY ACCOMPLISHED ERS-EM-52MR-308.
- [SDR SIMA20141221003](https://openairdocs.org/sdr/SIMA20141221003.md): Engine · power loss · Dec 21, 2014 · N600BP · Emb EMB145LR · Engine (Turbine/Turboprop)
  > NUMBER 2 ENG UNABLE TO PRODUCE COMMANDED THRUST IN DETENT DURING CRUISE & NR 2 N1 ABOUT 1% BELOW COMMANDED THRUST. NR 2 ITT WAS ON BORDER OF AMBER A FEW TIMES. NR 2 ITT 50 + WARMER COMPARED TO NR 1 ENG ITT. NR 2 N2 APPROX 4% HIGHER THAN NR 1. RETURNED & AF
- [SDR SIMA20141117004](https://openairdocs.org/sdr/SIMA20141117004.md): Light · inoperative · Nov 17, 2014 · N600BP · Emb EMB145LR · Emergency Lighting
  > SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C01608.
- [SDR SIMA20141013002](https://openairdocs.org/sdr/SIMA20141013002.md): Rib · chafed · Oct 13, 2014 · N600BP · Emb EMB145LR · Wing, Rib/Bulkhead
  > LEFT WING AILERON PCA HYDRAULIC LINES CHAFING INTERNAL RIBS OF WING. COMPLIED WITH REPAIR OF LT WING RIB 21 IAW ERS-EM-57MR-260.
- [SDR SIMA20141009002](https://openairdocs.org/sdr/SIMA20141009002.md): Rib · gouged · Oct 9, 2014 · N600BP · Emb EMB145LR · Wing, Rib/Bulkhead
  > LEFT WING RIB 21 GOUGED. COMPLIED WITH LT WING RIB 21 REPAIR IAW ERS-EM-57MR-260.
- [SDR SIMA20141008012](https://openairdocs.org/sdr/SIMA20141008012.md): Rib · cracked · Oct 8, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IS CRACKED LOWER OTBD CORNER. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IAW SRM 51-40-02.
- [SDR SIMA20141008010](https://openairdocs.org/sdr/SIMA20141008010.md): Gusset · cracked · Oct 8, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > GALLEY FLOOR GUSSET HAS A CRACK AT FRAME 18. INSTALLED NEW GALLEY FLOOR GUSSET IAW SRM 51-40-02.
- [SDR SIMA20141005008](https://openairdocs.org/sdr/SIMA20141005008.md): Support Bracket · cracked · Oct 5, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > FOUND SUPPORT BRACKET FOR THE BLEED AIR DUCT, JUST AFT OF APU CHECK VLV IN THE AFT AVIONICS TO BE CRACKED. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IAW SRM 51-40-02.
- [SDR SIMA20141001008](https://openairdocs.org/sdr/SIMA20141001008.md): Support · cracked · Oct 1, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT OVERWING PANEL SUPPORT FLANGE IS CRACKED AT FRAME 48. REPAIRED LT OVERWING PANEL SUPPORT FLANGE AT FRAME 48 IAW SRM 53-23-12.
- [SDR SIMA20141001007](https://openairdocs.org/sdr/SIMA20141001007.md): Bracket · cracked · Oct 1, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT OVERWING PANEL SUPPORT FLANGE HAS A CRACKED BRACKET AT FRAME 48. R & R RT OVERWING SUPPORT FLANGE BRACKET IAW SRM CH 51-40-02.
- [SDR SIMA20141001006](https://openairdocs.org/sdr/SIMA20141001006.md): Support Angle · cracked · Oct 1, 2014 · N600BP · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE CRACKED, AFT OF THE RT MLG WELL FOR THE AFT BELLY FAIRING. R & R BRACKET IAW SRM CH 51-40-02.

Next page: https://openairdocs.org/aircraft/N600BP/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 = 'N600BP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N600BP/reports

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