Embraer EMB-145LR
Service difficulty reports · 36,788
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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 aircraft_model_key = 'EMB145LR' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 aircraft_model_key = 'EMB145LR' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HNAA2026081200658Clamp · leakingBLEED 1 LEAK IN FLIGHT, ENGINE BLEED SYSTEMS. TROUBLESHOT BLEED 1 SYSTEM, FOUND CLAMP BETWEEN HSV AND CHECK VALVE TO BE LEAKING. REINSTALLED CLAMP AND TORQUED IAW AMM 36-11-02. OPS CHECKED GOOD. ACFT OKAY FOR SERVICE. RETURNED ACFT TO NORMAL CONFIGURATIONSDR HNAA2026081400701Shear Tie · crackedSHEAR CLIP AT FRAME 61 BETWEEN STGR 6R AND 7R IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STGR 6R AND 7R IAW EMB145 SRM 51-40-02SDR HNA2026F00002Duct · leakingBLEED 1 LEAK IN FLT. R & R ENGINE 1 Y-DUCT IN PYLON. NO FIX. FOUND OVER-WING COUPLING IN BLEED DUCT MISSING INTERNAL O-RING (BLEED SLEEVE) COUPLIN REMAINS DETACHED.SDR HNAA202608120658Warning Message · false indicationDURING CRUISE RT TANK INDICATED FROM 2000LB TO 800LB WITH FUEL IMBALANCE MESSAGE. INDICATION RETURNED TO NORMAL IN DESCENT. INSPECTED FUEL QTY, EICAS MATCHES SPR AND MAGNA STICKS. PERFORMED OPS CHECKED IAW AMM 28-41-00. OPS CHECKED GOOD.SDR HNAA2026081200657Inverter · abnormalFWD FLOOR EMERGENCY LIGHT INOP AT FLOORBOARD 231GF. R & R FWD EMERGENCY LIGHT INVERTER IAW AMM33-50-11-04SDR HNAA2026092200883Skin · corrodedRT INLET HAS PITTING ON LIP SKIN. R/H INLET REMOVED AND REPLACED ON WO# H10452 S/N 00912 QUANTUM# 4600.SDR HNAA2026090100852Support · corrodedFOUND CORROSION UNDER LT OTBD SUPPORT AT FR 61-62. REMOVED AND REPLACED WITH A NEW LT OTBD PARTITION DOUBLER AT FR 61 IAW SRM 51-40-02PR, STEP 2E.SDR HNAA2026102101024Floor Support · crackedRIGHT OMEGA BEAM OTBD ANGLE CRACKED BTWN FR 46-48. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026082400763Door Frame · damagedCARGO DOOR LOWER FRAME HAS ELONGATED HOLES. R & R CARGO DOOR LOWER FRAME IAW SRM 51-40-02, 51-20-01SDR HNAA2026092200887Floor Support · crackedFOUND RH OMEGA BEAM TO HAVE A CRACK BETWEEN FR 60 AND FR 61. PERFORMED CUTOUT WITH FILLER AND DOUBLER REPAIR ON RH OMEGA BEAM BETWEEN FR 60 AND FR 61 IAW ETD2026-145-013745 AND PIEDMONT MAJOR EO# EO1-53-26-0392SDR HNAA2026092200886Floor Support · crackedFOUND RH OMEGA BEAM TO HAVE A CRACK AT FR 59. PERFORMED CUTOUT WITH A FILLER AND DOUBLER REPAIR ON THE RT OMEGA BEAM AT FR 59 IAW ETD2026-145-013745 AND MAJOR EO# EO1-53-26-0392SDR HNAA2026090100817Floor Support · crackedUPON REMOVAL OF ONE RT OMEGA BEAM GUSSET AT FR 61, FOUND RT OMEGA BEAM TO BE CRACKED BTWN FR 60 & FR 61. PERFORMED CUTOUT WITH FILLER & DOUBLER REPAIR ON RT OMEGA BEAM BTWN FR 60 & FR 61 IAW ETD2026-145-013745. SEE EO 1-53-26-0392.SDR HNAA2026090100816Floor Support · corrodedUPON REMOVAL OF ONE RT OMEGA BEAM GUSSET AT FR 61, FOUND RT OMEGA BEAM TO BE CRACKED AT FR 59. PERFORMED CUTOUT WITH A FILLER & DOUBLER REPAIR ON THE RT OMEGA BEAM AT FR 59 IAW ETD2026-145-013745 REV-. SEE EO1-53-26-0392.SDR HNAA2026090100815Floor Support · crackedUPON REMOVAL OF ONE LT OMEGA BEAM GUSSET AT FR 61, FOUND LT OMEGA BEAM TO HAVE A CRACK AT FR 59. PERFORMED CUTOUT WITH FILLER AND DOUBLER REPAIR ON LT OMEGA BEAM AT FR 59 IAW ETD2026-145-013738 REV-. SEE MAJOR EO- 1-53-26-0391.SDR HNAA2026090100851Support · corrodedRIGHT INBD FLAP, OTBD FLAP SHROUD SUPPORT, PITTED ON MATING SURFACE. REMOVED THE CORROSION ON RT INBD FLAP, OTBD FLAP SHROUD SUPPORT BY BLENDING. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-10-05-PR, STEP 3. REPLACED THE SHROUD SUPPORT WITH NEW.SDR HNAA2026080700654Skin · crackedRIGHT WING HAS CRACK ON LWR SURFACE BTW SPAR 11-12 AT SPAR II. STOP DRILLED CRACK IAW T1-145-26-130. COMPLIED WITH RT WING SKIN REPAIR IAW EO1-57-26-0409.SDR HNAA2026082400762Rib · crackedCARGO DOOR LOWER CENTER RIB CRACKED, AND LOWER RIB NEXT TO VENT DOOR HAS ELONGATED HOLE. REPAIRED CARGO DOOR LOWER CENTER RIB AT RIVET HOLE CRACK IAW ETD-2026-145-013555 AND EO1-52-26-0366.SDR HNAA2026080500649Fuel Tank · leakingSTRONG FUEL ODOR IN CABIN AND FLIGHT DECK. FOUND FUEL LEAKING AT FWD FUEL TANK BULKHEAD IN CABIN APPROX STRINGER 17R. R & R SEALANT TO AFFECTED AREA INSIDE FUEL TANK IN REF TO SRM 51-20-01. LEAK CHECK GOOD, NO FURTHER DEFECTS OR SMELLS NOTED AT THIS TIME ACSDR HNAA2026080500650Valve · stuckEXHAUST FUME ODOR NOTICED WITH PACKS ON, FROM NR 2 ENGINE. PERFORMED GVI AT ENG 2, NO SIGNS OF OIL IN BYPASS OR OTHER ENG AREAS, BOTH PACKS 1 & 2 AREAS APPEAR NORMAL WITH NO MELTED SLEEVES. ON INSPECTION, FOUND PC AIR FLAP VALVE STUCK OPEN, LUBED HINGE AND ASDR HNAA2026080400646Bleed Air Sys · leakingCREW NOTIFIED CLT MX OF EXHAUST FUMES IN COCKPIT. CLT MX CREW REPORTED SMELL IN COCKPIT, CABIN NORMAL, FUTHER TROUBLESHOOTING FOUND APU BLEED CAUSE OF FUMES AND WAS PUT ON MEL. A/C DEPARTED WITH NO FURTHER ISSUES IN FLIGHT.SDR HNAA202608100646O-Ring · leakingEXHAUST FUME SMELL IN COCKPIT. APU BLEED SYSTEM. R&R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHECKED GOOD. LEAKS CHECK GOOD.NO OTHER OR FUMES IN COCKPIT OR CABIN.OK FOR SERVICE AT THIS TIME.SDR HNAA2026080400645Elect Module · faultedON TAKE OFF ROLL AT V1 FLIGHT CONTROL DID NOT RESPOND TO YOKE MOVEMENT. C/W HORIZONTAL STABILIZER ELECTRICAL/ELECTRONIC OPS CHECK IAW AMM 27-40-00-700-802-A. C/W AURAL WARNING OPS CHECK IAW AMM TASK 31-51-00-700-801-A. C/W ELEVATOR CONTROL CABLE TENSION CHECKSDR HNAA2026080400644O-Ring · leakingEXHAUST FUME ODOR IN COCKPIT. MEL C21521, 36-2 APU BLEED SYSTEM. R & R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHKD GOOD. LEAK CHKD GOOD. NO OTHER OR FUMES IN COCKPIT OR CABIN.OK FOR SERVICE AT THIS TIME.SDR HNAA2026082400761Bulkhead · damagedPILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS ELONGATED. COMPLETED INSTALLING NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE ON PILOTS BULKHEAD UPPER OUTBD GUIDE PIN HOLE IAW SRM 53-21-02RE, ITEM 4, FIGURE 3204, & SRM 51-40-02.SDR HNAA2026081400712Rib · damagedF143997 RUDDER I TOP RIB DAMAGED DURING REMOVAL OF HORIZONTAL STABILIZER. PERFORMED RE-CONTOUR AND SPLICE REPAIR TO THE RUDDER I TOP RIB IAW EMB ETD2026-145-01327 REV. A, AND EO1-55-26-0370SDR HNAA2026080300642Sign · inoperativeEMERGENCY EXIT LIGHT DIRECTLY ABOVE FA JUMPSEAT DOES NOT ILLUMINATE WHEN SET TO ON. R & R EMERGENCY EXIT MARKING SIGN ASSY DIRECTLY ABOVE FA JUMPSEAT IAW EMB 145 33-50-14. OPS CHECK GOOD.SDR HNAA2026080300641Radar · failedWING A/I FAIL MSG APPEARED ON EICAS IN ICING CONDITIONS, WING ANTI-ICING SYSTEM. OPS CHECK GOOD IAW AMM 30-00-00. A/C OK FOR SERVICE AT THIS TIME.SDR HNAA2026081400711Door Frame · damagedCARGO DOOR LOWER FRAME HAS MULTIPLE ELONGATED HOLES. REMOVED AND REPLACED CARGO DOOR LOWER FRAME IAW EMB 145 SRM 51-40-02, 51-20-01SDR HNAA2026092200885Rib · crackedRT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE RT WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER IAW SRM 57-20-07-RE, AND EO 1-57-26-0404SDR HNAA202609220085Rib · crackedRT WING, 1EA RIB 21 HAS A CRACK ON UPPER MID FLANGE. REPAIRED CRACK ON RIB 21 OF THE R/H WING UPPER MID FLANGE WITH A CUTOUT FILLER AND DOUBLER PER EMB 145 SRM 57-20-07-RE, AND PIEDMONT MAJOR EO-1-57-26-0404.SDR HNAA2026090100814Rib · crackedRIGHT WING, ONE RIB 21 HAD A CRACK ON UPPER MID FLANGE. REPAIRED THE RIB MID FLANGE WITH A CUTOUT FILLER & DOUBLER IAW SRM 57-20-07-RE, & EO-1-57-26-0404.SDR KY7A20260730001Rib · crackedDURING A SCHEDULED C-CHECK, FOLLOWING REMOVAL OF BOTH ENGINES, A VISUAL INSPECTION IDENTIFIED FOUR APPROXIMATELY 1.5-INCH CRACKS, TWO ON EACH SIDE OF THE AIRCRAFT, IN THE RIB FIREPROOF PYLON SKIN, P/N 145-21430-402 SAME ON BOTH SIDES. PROPOSED REPAIR HAS BEEN SDR HNAA2026082600795Strip · corrodedTAIL BOOM STRIP CORRODED. R & R STRIPS IAW AMM20-10-01 AND SB 145-55-0030SDR HNAA2026090100850Floor Support · corrodedLEFT FLOOR SUPPORT AT FR 49 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT AT FR 49 IAW SRM 51-40-02 PR , ALODINE PO 342139 & SRM CPM 51-21-04.SDR HNAA2026090100849Floor Support · corrodedRIGHT FLOOR SUPPORT AT FR 49 WAS CORRODED. REMOVED AND REPLACED THE RT FLOOR SUPPORT FROM FR 48 TO FR 52 IAW SRM 51-40-02, STEP 2 AND 4.SDR HNAA2026090100848Floor Support · corrodedLEFT FLOOR SUPPORT FROM FR 41 TO FR 45 HAD CORROSION. REMOVED THE FLOOR SUPPORT AND INSTALLED A NEW LT FLOOR SUPPORT FROM FR 41 TO FR 45 IAW SRM 51-40-02-PR, & SRM 51-20-01-PR.SDR HNAA2026090100847Gusset · corrodedLEFT OMEGA BEAM UPPER GUSSET FROM FR 39 TO FR 45 HAD CORROSION. REMOVED AND INSTALLED A NEW LT OMEGA BEAM UPPER GUSSET FROM FR 39 TO FR 45, SEALANT PO 342559 IAW SRM 51-40-02, STEP 2.SDR HNAA2026090100846Gusset · corrodedMID OMEGA BEAM UPPER GUSSET FROM FR 40 TO FR 43 HAD CORROSION. REMOVED AND REPLACED THE MID OMEGA BEAM UPPER GUSSET FROM FR 40 TO FR 46 IAW SRM 51-40-02 PR, STEP 2C, AND 3B.SDR HNAA2026090100845Floor Support · corrodedRIGHT FLOOR SUPPORT, FR 41 TO FR 44 HAS CORROSION. REMOVED THE DAMAGED FLOOR SUPPORT & INSTALLED NEW, FR 41 TO FR 44 IAW SRM 51-40-02-PR, & SRM 51-20-01-PR.SDR HNAA2026090100844Floor Support · corrodedLEFT FLOOR SUPPORT FROM FR 35 TO FR 39 HAD CORROSION. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 35 TO FR 39 IAW SRM 51-20-03.SDR HNAA2026090100843Floor Support · corrodedRIGHT FLOOR SUPPORT FROM FR 35 TO FR 39 HAD CORROSION. REMOVED & REPLACED THE RT FLOOR SUPPORT FROM FR 36 - 42 IAW SRM 51-40-02-PR, STEPS 2 & 4.SDR HNAA2026090100842Gusset · corrodedMID OMEGA BEAM UPPER GUSSET FROM FR 35 TO FR 38 HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM MID UPPER GUSSET AT FR 35 TO 38 IAW SRM 51-40-02-PR, STEP 2C.SDR HNAA2026090100841Floor Support · corrodedLEFT FLOOR SUPPORT FROM FR 29 TO FR 35 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, STEP 2.B AND 3.B.SDR HNAA2026090100840Gusset · corrodedLEFT OMEGA BEAM UPPER GUSSET FROM FR 29 TO FR 35 HAD CORROSION. REMOVED AND REPLACED THE LT OMEGA BEAM GUSSET FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR.SDR HNAA2026090100839Gusset · corrodedMID OMEGA BEAM UPPER GUSSET FROM FR 29 TO FR 35 HAD CORROSION. REMOVED AND REPLACED THE MID OMEGA BEAM GUSSET FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, & SRM 51-20-01-PR.SDR HNAA2026090100838Floor Support · corrodedRIGHT FLOOR SUPPORT FROM FR 31 TO FR 35 HAD CORROSION. REMOVED AND REPLACED RT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02PR, STEP 2 B & C.SDR HNAA2026082500780Firewall · crackedAPU FIREWALL CRACKED. REPAIRED IAW SRM 53-32-12SDR HNAA2026081000656Shear Tie · crackedSHEAR TIE CRACKED AT FR 24 BTW STR 16-17R. R & R SHEAR TIE IAW SRM 51-40-02.SDR HNAA2026090100833Floorbeam · corrodedMID FLOORBEAM AT FR 25 HAS CORROSION. REMOVED AND REPLACED WITH A NEW MID FLOORBEAM AT FR 25 IAW SRM 51-40-02-PR.SDR HNAA202609010233Floorbeam · corrodedMID FLOORBEAM AT FR 25 HAD CORROSION. REMOVED AND REPLACED WITH A NEW FLOORBEAM AT FR 25 IAW SRM 51-40-02-PR.
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