# Service difficulty reports: N640AE

A list on [N640AE](https://openairdocs.org/aircraft/N640AE.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 6 · 282 reports

- [SDR HNAA2026100200941](https://openairdocs.org/sdr/HNAA2026100200941.md): Pin · damaged · Oct 1, 2026 · N640AE · Emb EMB145LR · Light System Wiring
  > WIRE DE-PINNED @ EMERGENCY FLOOR LIGHTS CONNECTOR BETWEEN ROWS 9 AND 10. REPINNED WIRE & INSTALLED NEW MALE CONNECTOR IAW WM 33-50-50. PERFORMED OPS CHECK IRW AMM 33-50-00-05 P/N ON AND OFF CONNECTOR, 1330280 1330372
- [SDR HNAA2026092300899](https://openairdocs.org/sdr/HNAA2026092300899.md): Spar · cracked · Sep 4, 2026 · N640AE · Emb EMB145LR · Nacelle/Pylon, Frame/Spar/Rib
  > RELEVANT INDICATION NOTED DURING HFEC OF LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE BUSHING IAW SB 145-54-0008 AND EO1-54-26-0423.
- [SDR HNAA2026092300898](https://openairdocs.org/sdr/HNAA2026092300898.md): Spar · cracked · Sep 4, 2026 · N640AE · Emb EMB145LR · Nacelle/Pylon, Frame/Spar/Rib
  > RELEVANT INDICATION NOTED DURING HFEC OF RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE BUSHING IAW SB 145-54-0008 AND EO1-54-26-0423.
- [SDR HNAA2026092300897](https://openairdocs.org/sdr/HNAA2026092300897.md): Mount · cracked · Aug 30, 2026 · N640AE · Emb EMB145LR · Rudder Structure
  > RUDDER II PANEL 327FR LOWER MOUNTING FLANGE CRACKED ON RH SIDE. REMOVED CRACKED RUDDER II PANEL 327FR LOWER MOUNTING FLANGE (RIB), PREPPED AND INSTALLED SERVICEABLE 327FR LOWER MOUNT FLANGE (RIB) IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026092300896](https://openairdocs.org/sdr/HNAA2026092300896.md): Shear Tie · cracked · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > CABIN SHEAR TIE CRACKED AT FR-61 BETWEEN STGRS 6L/7L. REMOVED AND REPLACED CRACKED CABIN SHEAR TIE IAW SRM 51-40-02.
- [SDR HNAA2026092300895](https://openairdocs.org/sdr/HNAA2026092300895.md): Door Sill · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR SILL CORRODED IN MULTIPLE AREAS. R & R CARGO DOOR SILL IAW SRM 51-40-02.
- [SDR HNAA2026092300893](https://openairdocs.org/sdr/HNAA2026092300893.md): Floor Support · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT NR 4 HAD CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300892](https://openairdocs.org/sdr/HNAA2026092300892.md): Floor Support · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT HAD CORROSION IN MULTIPLE AREAS. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300891](https://openairdocs.org/sdr/HNAA2026092300891.md): Floor Support · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. R & R RT CABIN FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300890](https://openairdocs.org/sdr/HNAA2026092300890.md): Floor Support · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED LH CABIN FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR HNAA2026092300889](https://openairdocs.org/sdr/HNAA2026092300889.md): Seat Track · corroded · Aug 25, 2026 · N640AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT UPPER SEAT TRACK NR 3 CORRODED IN NUMEROUS AREAS. R & R LT UPPER SEAT TRACK IAW AMM 53-01-06
- [SDR HNAA2026092300901](https://openairdocs.org/sdr/HNAA2026092300901.md): Skin · cracked · Aug 22, 2026 · N640AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAD A POSSIBLE CRACK AT A RIVET AT FRAME 78, JUST BELOW STRINGER 4L. REPAIRED CRACKED FUSELAGE SKIN IAW EO1-53-26-0433 AND SRM 53-32-01
- [SDR HNAA2026092300900](https://openairdocs.org/sdr/HNAA2026092300900.md): Skin · dented · Aug 22, 2026 · N640AE · Emb EMB145LR · Elevator, Plate/Skin
  > LEFT ELEVATOR LOWER EXTERNAL SKIN HAS A DENT, AFT AND OTBD OF 335BB. PERFORMED DRILL OUT AND RECONTOURED DENTED AREA, INSTALLED BLIND RIVET IAW ETD2026-145-014792 REV A AND EO1-55-26-0421.
- [SDR HNAA2026092300894](https://openairdocs.org/sdr/HNAA2026092300894.md): Hinge Fitting · excess play · Aug 22, 2026 · N640AE · Emb EMB145LR · Rudder Structure
  > RUDDER UPPER HINGE FITTING, AT VERTICAL STAB, HAS PLAY. REMOVED AND REPLACED RUDDER UPPER HINGE FITTING IAW SRM 51-40-02 AND AMM 20-10-01.
- [SDR HNAA2026051800383](https://openairdocs.org/sdr/HNAA2026051800383.md): Light · inoperative · May 15, 2026 · N640AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT STRIP FOR SEAT 8A TO 9A INOP. R & R LIGHT STRIP IRT AMM 33-50-12 P/N ON 6636-8 P/N OFF 6636-8
- [SDR HNAA2026042400356](https://openairdocs.org/sdr/HNAA2026042400356.md): Switch · out of adjust · Apr 23, 2026 · N640AE · Emb EMB145LR · Landing Gear Position and Warning
  > AFTER TAKE OFF AIR/GND FAIL MSG. SELECTED GEAR UP WITH NO GEAR RETRACTION. UPON INSPECTION FOUND NLG WOW SWITCH NO MAKING GAP WITH TARGET. ADJUSTED GAP ON NLG WOW SWITCH AND TARGET IAW AMM 32-63-05. OPS CHECK GOOD. PERFORMED GEAR SWINGS IAW AMM 32-30-00. O
- [SDR HNAA2026020400110](https://openairdocs.org/sdr/HNAA2026020400110.md): Gearbox · failed · Feb 3, 2026 · N640AE · Emb EMB145LR · Trailing Edge Flap Actuator
  > ON APPROACH FLAP LOW SPEED FOLLOWED BY FLAP FAIL. STUCK AT 45*. MESSAGES APPEARED FROM 22* TO 45* R/R L/H O/B FLAP ANGLE GEARBOX IRT AMM 27-51-02-000/400-801-A. OPS CHECK GOOD. CHECKED RIGGING OF FLAPS IN REF TO AMM 27-53-04-700-801-A. RIGGING CHECKD GOOD. M
- [SDR HNAA202601230072](https://openairdocs.org/sdr/HNAA202601230072.md): Control Unit · abnormal · Jan 22, 2026 · N640AE · Emb EMB145LR · Trailing Edge Flap Control System
  > FLAP FAIL DISPLAYED ON EICAS ON APPROACH. RMU SHOWS RT FLAP AT 41 DEGREES & LEFT FLAP BLANKED OUT. EICAS & ACTUAL FLAP SHOWS 45 DEGREES BOTH SIDES. FACT 24JAN26 05:15 ERI REMOVED AND REPALCED FECU IRT AMM #27-53-02, OPS CHECK PERFORMED IRT AMM TASK #27-
- [SDR HNAA2025111700740](https://openairdocs.org/sdr/HNAA2025111700740.md): Pressure Switch · faulted · Nov 16, 2025 · N640AE · Emb EMB145LR · Rudder Control System
  > RUDDER SYSTEM 2 INOP DISPLAYED DURING TAKE-OFF AT ABOUT 50 KNOTS. R&R RUDDER PRESSURE SWITCH IN REF WITH 27-23-04-000-A/400-801-A. R&R RELAY K0387 IN REF WITH AMM TASK 20-13-02-000/400-801-A. R&R RUDDER SHUTOFF SYS 2 PB SWITCH IN REF WITH AMM 20-13-04-000/4
- [SDR HNAA2025102700724](https://openairdocs.org/sdr/HNAA2025102700724.md): Controller · faulted · Oct 26, 2025 · N640AE · Emb EMB145LR · Cabin Pressure Controller
  > AUTO PRESS FAIL MEL C29930 21-12-3 PRESS CONTROL AUTO AND MANUAL
- [SDR HNAA2025090400586](https://openairdocs.org/sdr/HNAA2025090400586.md): Control Unit · failed · Sep 4, 2025 · N640AE · Emb EMB145LR · Landing Gear Brake System
  > WHILE ON RUNWAY AN EICAS MESSAGE OF BRAKE DEGRADED APPEARED. REMOVED AND REPLACED BCU IRT EMB 145 AMM 32-41-02 OP. S CHECK GOOD.
- [SDR HNAA2025072300472](https://openairdocs.org/sdr/HNAA2025072300472.md): Start Valve · faulted · Jul 22, 2025 · N640AE · Emb EMB145LR · Engine Start Valves/Controls
  > DURING CLIMB AT ABOUT 3K BLEED 2 LEAK MESAGE ON EICAS, C/W QRH, MESSAGE CLEARED FACT 22JUL25 10:51 CLT RRD GROUND AIR START CONNNECTION ASSY IAW AMM 36-10-02. LEAK CHECK GOOD OK FOR SERVICE
- [SDR HNAA2025050100295](https://openairdocs.org/sdr/HNAA2025050100295.md): Check Valve · misinstalled · Apr 30, 2025 · N640AE · Emb EMB145LR · Hydraulic System, Main
  > AFTER T/O LG LEVER DISAGREE. HANDLE SELECTED UP GEAR REMAINED DOWN FACT 01MAY25 15:59 SBY UPON INSPECTION OF #100 HYDRULIC ACCUMILATOR, FOUND T-FITTING CHECK VALVE BACKWARDS. REMOVED AND REPLACED O-RINGS AND INSTALLED CHECK VALVE IN THE CORRECT ORIENTATI
- [SDR HNAA2024032700233](https://openairdocs.org/sdr/HNAA2024032700233.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026820 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 77 STGR 8L-9L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 77 BTW STR 8L-9L, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0201 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213.
- [SDR HNAA2024032700232](https://openairdocs.org/sdr/HNAA2024032700232.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026819 NO REPAIR INFO FOUND FOR STGR 19L REPAIR BTW FR 52-53. RE-ACCOMPLISHED REPAIR FOR DTI FCD ON STR 19L BTW FR 52-53 IAW PIEDMONT EO1-53-24-0204 AND EMB 145 SRM 53-24-02RE, ITEM 2, FIG. 201.
- [SDR HNAA2024032700231](https://openairdocs.org/sdr/HNAA2024032700231.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026818 NO REPAIR INFO FOUND FOR STGR 19R REPAIR BTW FR 52-53. REACCOMPLISHED SINGLE DOUBLER REPAIR ON STGR 19R BETWEEN FR 52-53 IAW EMB 145 SRM 53-24-02, ITEM 2 FIG 201, AND EO1-53-24-0189
- [SDR HNAA2024032700230](https://openairdocs.org/sdr/HNAA2024032700230.md): Frame · cracked · Mar 8, 2024 · N640AE · Emb EMB145LR · Fuselage Main, Frame
  > E026728 FR 66 CRACKED STGR 17L-18L BELOW CARGO DOOR SILL. RAR LOWER FR 66 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700220](https://openairdocs.org/sdr/HNAA2024032700220.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026833 NO REPAIR INFO FOUND FOR EXTERNAL LAV BUCKET DOUBLER. RE-ACCOMPLISHED EXTERNAL LAV BUCKET DOUBLER IAW EMB 145 SRM 53-31-02/RE AND ITEM 2 FIG 201, ETD2024-145-007309, AND EO1-53-24-0193.
- [SDR HNAA2024032700219](https://openairdocs.org/sdr/HNAA2024032700219.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026827: NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 77 STGR 8R-9R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 77 BTW STR 8R-9R, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0200 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 21
- [SDR HNAA2024032700218](https://openairdocs.org/sdr/HNAA2024032700218.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026826 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 5R-6R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 5R-6R, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0200 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213
- [SDR HNAA2024032700217](https://openairdocs.org/sdr/HNAA2024032700217.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026825 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 3R-4R. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 3R-4R, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0200 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213
- [SDR HNAA2024032700216](https://openairdocs.org/sdr/HNAA2024032700216.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026824 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 3L-4L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 3L-4L, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0201 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213
- [SDR HNAA2024032700215](https://openairdocs.org/sdr/HNAA2024032700215.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026823 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 4L-5L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 4L-5L, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0201 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213
- [SDR HNAA2024032700214](https://openairdocs.org/sdr/HNAA2024032700214.md): None · none · Mar 8, 2024 · N640AE · Emb EMB145LR · Standard Practices/Structures
  > E026821 NO REPAIR INFO FOUND FOR SKIN BUSHING REPAIR FR 79 STGR 6L-7L. REMOVED EXISTING SKIN BUSHING REPAIR AT FR 79 BTW STR 6L-7L, RE-ACCOMPLISHED SKIN BUSHING REPAIR AT SAME LOCATION IAW PIEDMONT EO1-53-24-0201 AND EMB 145 SRM 53-32-01 RE, ITEM 9, FIG. 213
- [SDR HNAA2024032700201](https://openairdocs.org/sdr/HNAA2024032700201.md): Support · corroded · Mar 6, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E026360 GALLEY CENTER BEAM RAMP SUPPORT AT FR20 CORRODED. REMOVED CORRODED GALLEY CENTER BEAM RAMP SUPPORT, INSTALLED SERVICEABLE RAMP SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700200](https://openairdocs.org/sdr/HNAA2024032700200.md): Cap · corroded · Mar 6, 2024 · N640AE · Emb EMB145LR · Main Landing Gear
  > E026358 CORROSION ON RH MLG FWD BEARING CAP. REMOVED AND REPLACED RH MLG FWD BEARING CAP IAW EMB 145 AMM 32-10-01.
- [SDR HNAA2024032700229](https://openairdocs.org/sdr/HNAA2024032700229.md): Shear Tie · cracked · Mar 4, 2024 · N640AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > E026057 FR 10 SHEAR CLIP CRACKED JUST BELOW THE LH DV WINDOW CUT-OUT. REMOVED AND REPLACED LH FR10 SHEAR CLIP JUST BELOW DV WINDOW CUTOUT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700228](https://openairdocs.org/sdr/HNAA2024032700228.md): Bulkhead · cracked · Mar 4, 2024 · N640AE · Emb EMB145LR · Fuselage Main, Bulkhead
  > E025977 NLG WHEEL WELL RH BULKHEAD CRACKED INSIDE NOSE HYDRAULIC COMPARTMENT, AT AFT UPPER END OF BULKHEAD. REPAIRED NLG WHEEL WELL RH BULKHEAD CRACK INSIDE NOSE HYDRAULIC COMPARTMENT, AT AFT UPPER END OF BULKHEAD IAW PIEDMONT EO1-53-24-0199 AND ETD2024-145-0
- [SDR HNAA2024032700199](https://openairdocs.org/sdr/HNAA2024032700199.md): Unknown · corroded · Mar 4, 2024 · N640AE · Emb EMB145LR · Fuselage Structure (General)
  > E025899 FWD DIGITAL IS CORRODED AT LH BEAM. ACCOMPLISHED REPAIR OF FWD DIGITAL AT LH BEAM IAW ETD# ETD2024-145-006688
- [SDR HNAA2024032700227](https://openairdocs.org/sdr/HNAA2024032700227.md): Shear Tie · cracked · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > E025727 RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 25 IS CRACKED. RAR RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 25 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700226](https://openairdocs.org/sdr/HNAA2024032700226.md): Shear Tie · cracked · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > E025726 RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 26 IS CRACKED. RAR RH SIDE SHEAR CLIP AT STRINGER 15R FRAME 26 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700213](https://openairdocs.org/sdr/HNAA2024032700213.md): Support · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025820 GALLEY LH OMEGA BEAM HAS CORROSION ON SIDE WALL AT FRAME 20. REPAIRED GALLEY LH OMEGA BEAM CORROSION ON SIDE WALL AT FR 20 IAW PIEDMONT EO1-53-24-0209 AND ETD2024-145-007851.
- [SDR HNAA2024032700212](https://openairdocs.org/sdr/HNAA2024032700212.md): Support · cracked · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025819 GALLEY LH OMEGA BEAM IS CRACKED ON SIDE WALL AFT OF FRAME 23. REPAIRED CRACKED GALLEY LH OMEGA BEAM ON SIDE WALL AFT OF FRAME 23 IAW PIEDMONT EO1-53-24-0186 AND ETD2024-145-006724
- [SDR HNAA2024032700211](https://openairdocs.org/sdr/HNAA2024032700211.md): Support · cracked · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025818 GALLEY LH OMEGA BEAM IS CRACKED ON SIDE WALL AFT OF FRAME 21. ACCOMPLISHED REPAIR ON CRACKED L/H GALLEY OMEGA BEAM SIDE WALL AFT OF FR21 IAW PIEDMONT EO1-53-24-0192 AND ETD2024-145-006707.
- [SDR HNAA2024032700210](https://openairdocs.org/sdr/HNAA2024032700210.md): Door Sill · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025813 CENTER GALLEY SERVICE DOOR SILL IS CORRODED AROUND NUTPLATE HOLES. REPAIRED CENTER GALLEY SERVICE DOOR CUTOUT LOWER SILL AT FWD AND AFT NUTPLATE HOLES IAW PIEDMONT EO1-53-24-0208 AND EMB145 SRM 53-21-02RE, ITEM 2, FIG 201.
- [SDR HNAA2024032700209](https://openairdocs.org/sdr/HNAA2024032700209.md): Shear Tie · cracked · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > E025729 LH SIDE SHEAR CLIP AT STRINGER 15L FRAME 24 IS CRACKED. REMOVED CRACKED SHEAR CLIP AT STRINGER 15L FRAME 24 AND INSTALLED SERVICEABLE LH SIDE SHEAR CLIP IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700208](https://openairdocs.org/sdr/HNAA2024032700208.md): Floor Support · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025734 RH #2 FLOOR SUPPORT HAS CORROSION. REMOVED CORRODED RH #2 FLOOR SUPPORT AND REPLACED WITH SERVICEABLE RH #2 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700207](https://openairdocs.org/sdr/HNAA2024032700207.md): Floor Support · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025732 LH #4 FLOOR SUPPORT HAS CORROSION. REMOVED CORRODED LH #4 FLOOR SUPPORT AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700206](https://openairdocs.org/sdr/HNAA2024032700206.md): Floor Support · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > E025730 LH #2 FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION ON LH #2 FLOOR SUPPORT IAW EMB 145 SRM 51-10-03 REMOVED AND REPLACED WITH SERVICEABLE LH #2 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2024032700198](https://openairdocs.org/sdr/HNAA2024032700198.md): Crossbeam · corroded · Mar 3, 2024 · N640AE · Emb EMB145LR · Fuselage Main, Structure
  > E025826 GALLEY LH SIDE CROSSBEAM AT FRAME 18 IS CORRODED. REMOVED CORRODED GALLEY LH SIDE CROSSBEAM AT FR 18 AND REPLACED GALLEY LH SIDE CROSSBEAM AT FR18 IAW EMB 145 SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N640AE/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 = 'N640AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N640AE/reports

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