# Service difficulty reports: N931AE A list on [N931AE](https://openairdocs.org/aircraft/N931AE.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 · 145 reports - [SDR HNAA2026072400604](https://openairdocs.org/sdr/HNAA2026072400604.md): Floor Support · corroded · Jul 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > RT OTBD FLOOR SILL AT FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL AT FR 22 IAW EMB 145 SRM 51-40-02-PR - [SDR HNAA2026072400631](https://openairdocs.org/sdr/HNAA2026072400631.md): Rib · cracked · Jul 14, 2026 · N931AE · Emb EMB145LR · Wing, Rib/Bulkhead > RT WING, RIB 21 OB OF AILERON PCU HAS A CRACK ON UPPER FLANGE. REPAIRED RT WING RIB 21 OB OF AILERON PCU UPPER FLANGE CRACK WITH A FILLER AND DOUBLER IAW SRM 57-20-07 STEP 4 FIG. 203 - [SDR HNAA2026072400630](https://openairdocs.org/sdr/HNAA2026072400630.md): Rib · cracked · Jul 14, 2026 · N931AE · Emb EMB145LR · Wing, Rib/Bulkhead > LEFT WING, RIB 21 OB OF AILERON PCU HAS A CRACK ON UPPER FLANGE. REPAIRED LT WING RIB 21 OB AILERON PCU CRACK USING FILLER AND DOUBLER ON UPPER FLANGE IAW SRM 57-20-07 STEP 4 FIG. 203. - [SDR HNAA2026072400629](https://openairdocs.org/sdr/HNAA2026072400629.md): Floor Support · cracked · Jun 24, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > FR 59 TO FR 61 LH OMEGA BEAM HAS CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE L/H OMEGA BEAM BETWEEN FRAME 59 - 60 SPLICE PER EMB 145 ETD2026-145-011104 REV.: A, AND SEE PIEDMONT MAJOR EO# EO1-53-26-0292 - [SDR HNAA2026072400628](https://openairdocs.org/sdr/HNAA2026072400628.md): Rib · cracked · Jun 22, 2026 · N931AE · Emb EMB145LR · Elevator, Spar/Rib > RIB ON RH ELEVATOR AT STA YH= 1340 HAS A CRACK. REMOVED AND REPLACED WITH NEW 1EA RIB ON RH ELEVATOR AT STA YH=1340 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400627](https://openairdocs.org/sdr/HNAA2026072400627.md): Rib · damaged · Jun 21, 2026 · N931AE · Emb EMB145LR · Trailing Edge Flaps > 00361 LH INBD FLAP HAS AN ELONGATED SCREW HOLE AS MARKED. COMPLIED WITH PERMANENT REPAIR OF THE L/H IB FLAP FAIRING ATTACH RIB PER EMB 145 ETD2026-145-010947 REV.: A, AND PIEDMONT EO1-57-26-0313 - [SDR HNAA2026072400621](https://openairdocs.org/sdr/HNAA2026072400621.md): Floor Support · corroded · Jun 20, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT OTBD FLOOR SILL FROM FR 30 TO FR 35 HAS CORROSION. REMOVED AND REPLACED RT OTBD FLOOR SILL FROM FR 30 - FR 35 PER EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400620](https://openairdocs.org/sdr/HNAA2026072400620.md): Floor Support · corroded · Jun 20, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OMEGA BEAM GUSSET AT FR 35 HAS CORROSION. REMOVED AND REPLACED LT OMEGA BEAM GUSSET FROM FR 30 TO FR 35 PER SRM 51-40-02 STEP 2C - [SDR HNAA2026072400619](https://openairdocs.org/sdr/HNAA2026072400619.md): Floor Support · corroded · Jun 20, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 30 TO FR 35 HAS CORROSION. REMOVED AND INSTALLED NEW FROM STOCK LT OTBD FLOOR SILL FROM FR 30 TO FR 35 PER SRM 51-40-02 - [SDR HNAA2026072400618](https://openairdocs.org/sdr/HNAA2026072400618.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OMEGA BEAM GUSSET FROM FR 36 TO FR 41 HAS CORROSION. REMOVED AND REPLACED 1EA LT OMEGA BEAM GUSSET LOCATED BETWEEN FR 36 - FR 41 PER EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400617](https://openairdocs.org/sdr/HNAA2026072400617.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 36 TO FR 41 HAS CORROSION. COMPLIED WITH PERMANENT REINFORCING REPAIR OF THE LT OTBD FLOOR SILL FROM FR36 - FR41 PER EMB 145 ETD2026-145-011099 REV.: / AND PIEDMONT EO1-53-26-0304. - [SDR HNAA2026072400616](https://openairdocs.org/sdr/HNAA2026072400616.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT OTBD FLOOR SILL FROM FR 36 TO FR 41 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL FROM FR 36 TO FR 41 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400615](https://openairdocs.org/sdr/HNAA2026072400615.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 43 TO FR 46 HAS CORROSION. REMOVED AND REPLACED LT OTBD FLOOR SILL FROM FR 43 TO FR 46 IAW SRM 51-40-02-PR. - [SDR HNAA2026072400614](https://openairdocs.org/sdr/HNAA2026072400614.md): Floor Support · not reported · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 47 TO FR 51 HAS CORROSION. REMOVED AND REPLACED LT OTBD FLOOR SILL FROM FR 47 TO FR 51 IAW SRM 51-40-02-PR. - [SDR HNAA2026072400613](https://openairdocs.org/sdr/HNAA2026072400613.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW SRM 51-40-02-PR. - [SDR HNAA2026072400612](https://openairdocs.org/sdr/HNAA2026072400612.md): Floor Support · corroded · Jun 19, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400626](https://openairdocs.org/sdr/HNAA2026072400626.md): Floor Support · cracked · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > ONE LT OMEGA BEAM GUSSET AT FR 28 HAS A CRACK. REMOVED AND REPLACED LH OMEGA BEAM GUSSET AT FR 28 PER EMB 145 SRM 51-40-08-PR. - [SDR HNAA2026072400625](https://openairdocs.org/sdr/HNAA2026072400625.md): Access Panel · cracked · Jun 18, 2026 · N931AE · Emb EMB145LR · APU Cowling/Containment > APU COWLING ACCESS PANEL CRACKED ON THE INTERIOR SIDE NEAR THE HINGE. REMOVED AND REPLACED APU COWLING ACCESS PANEL PER EMB 145 SRM 51-20-03 STEP 3 - [SDR HNAA2026072400624](https://openairdocs.org/sdr/HNAA2026072400624.md): Support Bracket · cracked · Jun 18, 2026 · N931AE · Emb EMB145LR · Cargo/Baggage Doors > FWD CARGO DOOR MECHANISM SUPPORT BRACKET CRACKED ON BOTTOM LEG. REMOVED AND REPLACED WITH NEW FWD CARGO DOOR MECHANISM SUPPORT BRACKET IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400623](https://openairdocs.org/sdr/HNAA2026072400623.md): Floor Support · cracked · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > ONE LT OMEGA BEAM AT FR 23 HAS A CRACKED. COMPLIED WITH PERMANENT REINFORCING REPAIR OF THE LT OMEGA BEAM AT FRAME 23 SPLICE IAW ETD2026-145-010691 REV. AND PIEDMONT EO1-53-26-0291. - [SDR HNAA2026072400622](https://openairdocs.org/sdr/HNAA2026072400622.md): Panel · cracked · Jun 18, 2026 · N931AE · Emb EMB145LR · Aerodynamic Fairings > PANEL 191ZB RT LEADING EDGE NR 1 STRAP ASSY ( HORSE COLLAR) IS CRACKED AT THE UPPER RADIUS BY FIRST FASTENER HOLE. COMPLIED WITH REPAIR TO THE RT WING-TO -FUSELAGE FAIRING PANEL 191ZB JOIN STRAP PER EMB 145 ETD2026-145-012463 REV.: / AND PIEDMONT EO1-05-26-03 - [SDR HNAA2026072400611](https://openairdocs.org/sdr/HNAA2026072400611.md): Gusset · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Structure > ONE LT FLOOR GUSSET AT FR 59 HAS CORROSION. REMOVED AND REPLACED LT FLOOR GUSSET FROM FR 59 TO FR 61 PER SRM 51-40-02, STEP 2 C, AND 3 B - [SDR HNAA2026072400610](https://openairdocs.org/sdr/HNAA2026072400610.md): Floor Support · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT OTBD FLOOR SILL FROM FR 25 TO FR 28 HAS CORROSION. REMOVED AND REPLACED RT OTBD FLOOR SILL FROM FR 23 - FR 29 PER EMB 145 SRM 51-40-02-PR - [SDR HNAA2026072400609](https://openairdocs.org/sdr/HNAA2026072400609.md): Floor Support · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SILL FROM FR 24 TO FR 29 HAS CORROSION. REMOVED AND REPLACED THE LT OTBD FLOOR SILL FROM FR24 - FR29 PER EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400608](https://openairdocs.org/sdr/HNAA2026072400608.md): Floor Support · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LEFT OTB FLOOR SILL FROM FR 20 TO FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 20 TO FR 22 IAW EMB 145 SRM 51-40-02 STEP 2 B, C AND 4B - [SDR HNAA2026072400607](https://openairdocs.org/sdr/HNAA2026072400607.md): Floorbeam · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Floor Beam > LH FLOOR CROSSBEAM AT FR 18 HAS CORROSION. REMOVED AND REPLACED WITH NEW LH FLOOR CROSSBEAM AT FR 18 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400606](https://openairdocs.org/sdr/HNAA2026072400606.md): Door Frame · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Structure > SERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 HAS CORROSION. REMOVED AND REPLACED WITH NEW SERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 IAW EMB 145 SRM 51-40-02-PR - [SDR HNAA2026072400605](https://openairdocs.org/sdr/HNAA2026072400605.md): Gusset · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Structure > RIGHT FLOOR GUSSET AT FR 22 HAS CORROSION. REMOVED RH FLOOR GUSSET AT FR 22.AND INSTALLED NEW GUSSET AT FR 22 PER EMB 145 SRM 51-40-02-PR - [SDR HNAA2026072400603](https://openairdocs.org/sdr/HNAA2026072400603.md): Floor Support · corroded · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > 00148 1EA RH OB FLOOR SILL AT FR 20 HAS CORROSION. REMOVED AND REPLACED WITH NEW RH OB FLOOR SILL AT FR 20 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2026072400602](https://openairdocs.org/sdr/HNAA2026072400602.md): Paint · flaking · Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Structure > PANEL 191HL HAS CORROSION UNDER PAINT AND PAINT IS FLAKING OFF. REMOVED CORROSION FOUND ON PANEL 191HL, LOWEST REMAINING THICKNESS FOUND TO BE AT.06995 PARTS FOUND TO BE WITHIN LIMITS PER EMB 145 SRM 51-10-05. - [SDR HNAA2026072400601](https://openairdocs.org/sdr/HNAA2026072400601.md): Cup · corroded · Jun 17, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Structure > CORROSION AROUND THE WASTE DRAIN VALVE. REMOVED AND REPLACED WITH NEW WASTE DISCHARGE CUP ASSY PER EMB 145 SRM 51-40-02-PR STEP 4B. - [SDR HNAA2026061600500](https://openairdocs.org/sdr/HNAA2026061600500.md): Unknown · odor · Jun 14, 2026 · N931AE · Emb EMB145LR · Air Distribution System > IN FLT FUMES AND ODOR IN COCKPIT- BURNING ELEC SMELL. OPS CHECKED APU BOTH ENGINES, BOTH PACKS, BOTH WIPERS, WINDSHIELD HEAT. OPS CHECK GOOD. INSPECTED BOTH DISTRIBUTION BOXES AND RELAY PANELS UNDER COCKPIT AND NOSE AVI BAY NO DISCREPANCY FOUND. OK FOR SERV - [SDR HNAA2026032300229](https://openairdocs.org/sdr/HNAA2026032300229.md): Pipe · broken · Mar 22, 2026 · N931AE · Emb EMB145LR · Air Distribution System > WITH E1 ON, ON TAXI OUT BURNING SMELL IN FLT DECK AND CABIN WITH EITHER PACK ON. INSPECTED PACK 1 AND PACK 2. FOUND BROKEN SECTION OF PIPE. SUSPECT BROKEN SECTION OF PIPE SUCKED INTO PACK 2 SYSTEM R & R EMERGENCY VENTILATION PIPE ON PACK NR 2 THAT CONNECTS - [SDR HNAA2025120300847](https://openairdocs.org/sdr/HNAA2025120300847.md): Warning Message · false activation · Dec 2, 2025 · N931AE · Emb EMB145LR · Central Warning > BLEED 1 LEAK DISPLAYED IN FLIGHT. INSPECTED FOR BLEED 1 LEAK/ NO DEFECTS NOTED. OPS CHECKED IAW AMM 36-00-00. OPS CHECKED GOOD. COULD NOT DUPLICATE. AC OK FOR SERVICE - [SDR HNAA2025092300638](https://openairdocs.org/sdr/HNAA2025092300638.md): Bleed Valve · failed · Sep 22, 2025 · N931AE · Emb EMB145LR · Compressor Bleed Valve > BLEED 1 VALVE FAILED MESSAGE ON TO ROLL. R & R THE BLEED VALVE IAW AMM 36-11-05. OPS CHECKED GOOD IRT AMM 36-00-00-700-803-A. GROUND RAN AIRCRAFT. NO LEAKS NOTED AT THIS TIME. OKAY FOR SERVICE. - [SDR HNAA2025031000145](https://openairdocs.org/sdr/HNAA2025031000145.md): Bleed Valve · activation error · Mar 8, 2025 · N931AE · Emb EMB145LR · Compressor Bleed Valve > ON TAKEOFF ENGINE BLEED VALVE FAIL ON EICAS, GOING 20 KNOTS AND REFKECTED TAKEOFF. FACT 08MAR25 18:48 CLT REMOVED AND REPLACED ENGINE BLEED AIR VALVE IRW AMM 36-11-05. PERFORMED OPS CHECK IAW AMM 36-11-05-700-802-A, OPS CHECK IS GOOD NO LEAKS NOTED. AIR - [SDR HNAA2024060700488](https://openairdocs.org/sdr/HNAA2024060700488.md): Computer · faulted · Jun 6, 2024 · N931AE · Emb EMB145LR · Stall Warning System > SPS 2 INOP DISPLAYED IN FLT FACT 06JUN24 20:04 PHL REMOVED AND REPLACED STALL PROTECT COMPUTER IAW AMM 27-36-02. PREFORMED OPS CHECK IAW AMM 27-36-00. OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR HNAA2024053000478](https://openairdocs.org/sdr/HNAA2024053000478.md): Unknown · odor · May 29, 2024 · N931AE · Emb EMB145LR · Air Distribution System > BURNING SMELL DURING TAXI. CLEARED WITH PACK 1 SELECTED OFF FACT 29MAY24 19:10 CLT INSPECTED BOTH PACKS FOR DEFECTS. NONE NOTED AT THIS TIME. PERFORMED OPS CHECK OF THE COOLING PACK SYSTEM IRT AMM 21-51-00. NO BURNING SMELL NOTED AT THIS TIME. A/C OK FOR SE - [SDR HNAA2024042900328](https://openairdocs.org/sdr/HNAA2024042900328.md): Boot · damaged · Apr 16, 2024 · N931AE · Emb EMB145LR · Cabin Cooling System > IN CLIMB OUT SLOW TO RAPID DEPRESSURIZATION AT FL 290.BEGAN TO STABALIZE AT FL 230 IN AUTO MODE. FACT 16APR24 20:05 PHL INSPECTED PACK 1 AREA AND FOUND DAMAGED BOOT BETWEEN AIRFRAME AND CONDENSER/MIXER. R+R BOOT IAW AMM 25-51-04. PERFORMED MANUAL/AUTO MODE - [SDR HNAA2024040100245](https://openairdocs.org/sdr/HNAA2024040100245.md): Floor Support · corroded · Mar 15, 2024 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > 00210 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN FRM48 AND FRM50. REMOVED AND REPLACED LH Y-479 FLOOR BEAM CAP BETWEEN FRM46 AND FRM53 IAW EMB-145 SRM 51-40-02-PR - [SDR HNAA2024040100244](https://openairdocs.org/sdr/HNAA2024040100244.md): Floorbeam · corroded · Mar 15, 2024 · N931AE · Emb EMB145LR · Fuselage Main, Floor Beam > 00207 LH Y-479 FLOOR BEAM CAP IS CORRODED BETWEEN X13200 AND X15125. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP (GUSSET) PN: 145-30634-005 IAW EMB-145 SRM 51-40-02-PR. - [SDR HNAA2024040100243](https://openairdocs.org/sdr/HNAA2024040100243.md): Floor Support · corroded · Mar 15, 2024 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > 00206 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN X11990 AND X13200.: INSTALLED NEW SERVICEABLE CENTER Y 0 FLOOR BEAM CAP BETWEEN X11990 AND 13200 IAW EMB145 SRM 51-40-02. - [SDR HNAA2024040100242](https://openairdocs.org/sdr/HNAA2024040100242.md): Seat Track · corroded · Mar 15, 2024 · N931AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > 00203 CENTER Y 0 FLOOR SEAT TRACK IS CORRODED BETWEEN FRM37 AND FRM38. INSTALLED CENTER Y 0 FLOOR SEAT TRACK BETWEEN FRM36 TO FRM46 IAW EMB145 AMM 53-01-06-400-801-A. - [SDR HNAA2024040100238](https://openairdocs.org/sdr/HNAA2024040100238.md): Floorbeam · corroded · Mar 15, 2024 · N931AE · Emb EMB145LR · Fuselage Main, Floor Beam > 00178 RH FLOOR BEAM CAP AT FRM22 AND Y+479 IS CORRODED. REMOVED AND REPLACED WITH NEW RH FLOOR BEAM CAP (P/N: 145-22461-011) IAW EMB145LR SRM 51-40-02 - [SDR HNAA2024240100240](https://openairdocs.org/sdr/HNAA2024240100240.md): Strap · corroded · Mar 14, 2024 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > LH FLOOR SUPPORT SRTRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED. REMOVED AND REPLACED STRAP IAW EMB145 SRM 51-40-02. - [SDR HNAA2024040100241](https://openairdocs.org/sdr/HNAA2024040100241.md): Floor Support · corroded · Mar 14, 2024 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > 00192 CENTER Y 0 FLOOR BEAM LH FLANGE IS CORRODED BETWEEN FRM28 AND FRM29. REPAIRED CENTER Y 0 FLOOR BEAM LH FLANGE IS CORROSION BETWEEN FRM28 AND FRM29 IAW EMB-145 SRM 53-22-10-RE AND PIEDMONT EO1-53-24-0210 - [SDR HNAA2024040100240](https://openairdocs.org/sdr/HNAA2024040100240.md): Strap · corroded · Mar 14, 2024 · N931AE · Emb EMB145LR · Fuselage Miscellaneous Structure > 00182 LH FLOOR SUPPORT STRAP AT X7578 BETWEEN Y-479 AND Y 0 IS CORRODED. - [SDR HNAA2024040100239](https://openairdocs.org/sdr/HNAA2024040100239.md): Floorbeam · corroded · Mar 14, 2024 · N931AE · Emb EMB145LR · Fuselage Main, Floor Beam > 00179 CENTER Y 0 FLOOR BEAM CAP IS CORRODED BETWEEN FRM20 AND X7038. INSTALLED NEW CENTER Y 0 FLOOR BEAM CAP PN# 145-22460-013 BETWEEN FRM20 AND X7038 IAW EMB 145 SRM 51-40-02-PR. - [SDR HNAA2023103000369](https://openairdocs.org/sdr/HNAA2023103000369.md): Unknown · unknown · Oct 28, 2023 · N931AE · Emb EMB145LR · Tire > LEFT I/B MAIN TIRE DAMAGED (TREAD CAME OFF). R&R #200 MLG TIRE IAW EMB AMM 32-49-02-000-801-A/32-49-02-400-801-A INSPECTED AND FOUND ADDITIONAL DAMAGE SEE SEQ 2,3, THIS LP. SEQ 1 OF L.P. 301128 - [SDR SIMA20230319001](https://openairdocs.org/sdr/SIMA20230319001.md): Flashlight · inoperative · Mar 19, 2023 · N931AE · Emb EMB145LR · Emergency Equipment > AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NOT CHARGING-C/A-RAR AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPC GOOD PER EMB AMM 33-51-01 Next page: https://openairdocs.org/aircraft/N931AE/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 = 'N931AE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N931AE/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.