# Service difficulty reports: N655AE

A list on [N655AE](https://openairdocs.org/aircraft/N655AE.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 4 · 198 reports

- [SDR HNAA2026092100860](https://openairdocs.org/sdr/HNAA2026092100860.md): Unknown · odor · Sep 20, 2026 · N655AE · Emb EMB145LR · Air Distribution System
  > DURING APP NOTICED OIL/RUBBER BURNING SMELL IN FLT DECK AT ABOUT 2000 FT. PERFORMED E1 & E2 HIGH POWER RUN IAW MAINTENANCE RUNUP CHECKLIST. NO DEFECTS NOTED DURING RUNUP. A/C OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2026080400646](https://openairdocs.org/sdr/HNAA2026080400646.md): Bleed Air Sys · leaking · Aug 4, 2026 · N655AE · Emb EMB145LR · APU Bleed Air System
  > CREW 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 HNAA2026072700637](https://openairdocs.org/sdr/HNAA2026072700637.md): A/C Pack · odor · Jul 26, 2026 · N655AE · Emb EMB145LR · Cabin Cooling System
  > OIL SMELL IN FLIGHTDECK FROM PACK 1. FACT 27JUL26 01:02 CLT INSPECTED PAX 1. FOUND TO BE GOOD. FOUND PAX 2 TO HAVE MELTED DUCT. REMOVED AND REPLACED DUCT AS REQUIRED. PERFORMED OP CHECK IAW 21-51-00. OP CHECK GOOD. NO DEFECTS NOTED A/C OKAY FOR SERVICE
- [SDR HNAA2026052000422](https://openairdocs.org/sdr/HNAA2026052000422.md): Skin · damaged · May 4, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > COCKPIT UNDERFLOOR HATCH 123BL HAS TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL. REPAIRED COCKPIT UNDERFLOOR HATCH 123BL TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL IAW PIEDMONT EO1-52-26-0223 AND ETD2026-145-007987.
- [SDR HNAA2026052000421](https://openairdocs.org/sdr/HNAA2026052000421.md): Floor Support · cracked · Apr 22, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LAVATORY RT HAT BEAM AT FR 59-60, CRACK ON FWD END OF NUT-PLATE. PERFORMED DOUBLER REPAIR FOR LAVATORY R/H HAT BEAM AT FR 59-60 IAW ETD2026-145-007317 AND SRM 53-24-10RE
- [SDR HNAA2026052000420](https://openairdocs.org/sdr/HNAA2026052000420.md): Frame · cracked · Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Frame
  > CRACKED FRAME 72, BETWEEN STRINGER 17L AND 16L. R & R FRAME 72 IAW ETD-2026-145-007557 AND EO1-53-26-0206.
- [SDR HNAA2026052000419](https://openairdocs.org/sdr/HNAA2026052000419.md): Stringer Splice · chafed · Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 19R (INTERIOR STRINGER) STRINGER SPLICE BETWEEN FR 52/53 CHAFED. REMOVED AND REPLACED STGR 19R SPLICE BTW FR 52-53 IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2026052000406](https://openairdocs.org/sdr/HNAA2026052000406.md): Structure · corroded · Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > GALLEY FLOOR, FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L AROUND NUT PLATE HOLE HAS CORROSION. PERFORMED DOUBLER ON GALLEY FLOOR FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L IAW EMB 145 SRM 53-21-10RE ITEM 2 FIG. 201 SHEET 5 DETAIL C AND EO1-05-26-0232.
- [SDR HNAA2026052000418](https://openairdocs.org/sdr/HNAA2026052000418.md): Floor Support · cracked · Apr 20, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > FOUND CRACKS ON LH OMEGA BEAM #2 AT FR 29. PERFORMED CUT-OUT OF DAMAGE, AND DOUBLER REPAIR TO LT OMEGA BEAM #2 AT FR 29 IAW EMB ETD2026-145-007261 AND EO1-53-26-0215.
- [SDR HNAA2026052000417](https://openairdocs.org/sdr/HNAA2026052000417.md): Door Frame · damaged · Apr 18, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Structure
  > MAIN DOOR LOWER FRAME AFT NUTPLATE HOLE DOUBLER HAS NO DTA INFORMATION. REPAIR WAS ACCOMPLISHED IAW ETN-EM-52-041. RE-ACCOMPLISHED DOUBLER FOR REPAIR OF MAIN DOOR LOWER FRAME AT AFT NUT-PLATE HOLE IAW SRM 52-10-04RE, ITEM 3, FIG 201, SHEET 3 AND EO1-52-26-019
- [SDR HNAA2026052000416](https://openairdocs.org/sdr/HNAA2026052000416.md): Doubler · not reported · Apr 17, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 35/36 AT STR 1L HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED DOUBLER REPAIR ON FUSELAGE EXTERNAL SKIN BETWEEN FR 35/36 AT STR 1L IAW ETD2026-145-007253-A AND EO1-53-26-0222.
- [SDR HNAA2026052000415](https://openairdocs.org/sdr/HNAA2026052000415.md): Repair · chafed · Apr 17, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 19R PREVIOUS REPAIR BETWEEN FR 52/53 CHAFED. PERFORMED NEW REPAIR OF STRINGER 19R (2 ANGLE REPAIR) BETWEEN FR 52/53 IAW SRM 53-24-02RE, ITEM 2, FIG 202 AND EO1-53-26-0231.
- [SDR HNAA2026052000414](https://openairdocs.org/sdr/HNAA2026052000414.md): Doubler · not opened · Apr 16, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Structure
  > FUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 70/71 STR 16R/18R HAS NO REPAIR INFORMATION. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FOR FUSELAGE EXTERNAL SKIN REPAIR BETWEEN FR 70/71 STR 16R/18R IAW EMB 145 ETD2026-145-007284 AND EO1-53-26-0217.ER BE
- [SDR HNAA2026052000413](https://openairdocs.org/sdr/HNAA2026052000413.md): Stringer · cracked · Apr 16, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STGR 2L AT FR-75 HAS A CRACK. PERFORMED SPLICE REPAIR ON STGR 2L AT FR-75 IAW ETD2026-145-007461 AND SRM 51-40-02 AND EO1-53-26-0207.
- [SDR HNAA2026052000405](https://openairdocs.org/sdr/HNAA2026052000405.md): Seat Track · corroded · Apr 16, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT UPPER SEAT TRACK 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 4 IAW AMM 53-01-06.
- [SDR HNAA2026052000404](https://openairdocs.org/sdr/HNAA2026052000404.md): Seat Track · corroded · Apr 16, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT UPPER SEAT TRACK NR 3 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK NR 3 IAW AMM 53-01-06.
- [SDR HNAA2026052000403](https://openairdocs.org/sdr/HNAA2026052000403.md): Gusset · corroded · Apr 15, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOORBEAM GUSSET AROUND NUT-PLATE HOLE BETWEEN FRAME'S 60 AND 61 HAS CORROSION. REMOVED AND INSTALLED NEW LAV LT FLOOR BEAM GUSSET IAW SRM 51-40-02 & SRM 51-40-09.
- [SDR HNAA2026052000412](https://openairdocs.org/sdr/HNAA2026052000412.md): Bulkhead · damaged · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Bulkhead
  > PILOT'S BULKHEAD OTBD UPPER GUIDE PIN HOLE IS ELONGATED. INSTALLED NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE FOR PILOT UPPER OUTBD GUIDE PIN HOLE REPAIR IAW SRM 53-21-02RE ITEM 4, FIGURE 204 AND EO1-53-26-0225
- [SDR HNAA2026052000402](https://openairdocs.org/sdr/HNAA2026052000402.md): Seat Track · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBD SEAT TRACK 2 HAS MULTIPLE CORRODED SPOTS. R & R RT INBD SEAT TRACK 2 IAW AMM 53-01-06.
- [SDR HNAA2026052000401](https://openairdocs.org/sdr/HNAA2026052000401.md): Seat Track · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK 1 HAS MULTIPLE CORRODED SPOTS. R & R RT OTBD SEAT TRACK 1 IAW AMM 53-01-06.
- [SDR HNAA2026052000400](https://openairdocs.org/sdr/HNAA2026052000400.md): Seat Track · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBD SEAT TRACK 1 HAS MULTIPLE CORROSION SPOTS. REMOVED AND REPLACED RT INBD SEAT TRACK 1 IAW AMM 53-01-06.
- [SDR HNAA2026052000399](https://openairdocs.org/sdr/HNAA2026052000399.md): Floorbeam · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > LEFT FLOORBEAM SUPPORT LOCATED ON FR35 HAS CORROSION. R & R LT FLOORBEAM SUPPORT LOCATED ON FR35 IAW SRM 51-40-02.
- [SDR HNAA2026052000398](https://openairdocs.org/sdr/HNAA2026052000398.md): Floorbeam · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > LH FLOORBEAM SUPPORT LOCATED ON FR25 HAS CORROSION. R & R LH FLOORBEAM SUPPORT AT FR 25 IAW SRM 51-40-02.
- [SDR HNAA2026052000397](https://openairdocs.org/sdr/HNAA2026052000397.md): Floorbeam · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Floor Beam
  > LH FLOOR CROSS SUPPORT LOCATED ON FR28 HAS CORROSION. REMOVED AND REPLACED LH FLOOR CROSS SUPPORT LOCATED ON FR28 IAW EMB 145 SRM 51-40-02
- [SDR HNAA2026052000396](https://openairdocs.org/sdr/HNAA2026052000396.md): Floor Support · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT OTBD FLOOR SILL 1 HAS MULTIPLE CORROSION SPOTS. R & R RT OTBD FLOOR SILL 1 IAW SRM 51-40-02, 51-40-09.
- [SDR HNAA2026052000395](https://openairdocs.org/sdr/HNAA2026052000395.md): Floor Support · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT OTBD FLOOR SILL 3 HAS MULTIPLE CORROSION SPOTS. R & R LT OTBD FLOOR SILL 3 IAW SRM 51-40-02.
- [SDR HNAA2026052000394](https://openairdocs.org/sdr/HNAA2026052000394.md): Door Sill · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Structure
  > GALLEY FLOOR SERVICE DOOR LOWER AFT SILL HAS CORROSION IN MULTIPLE AREAS. PERFORMED DOUBLER REPAIR ON GALLEY FLOOR SERVICE DOOR LOWER AFT SILL IAW EMB-145 SRM 53-21-10 RE, ITEM 4, FIGURE 203, SHEET 3 AND EO-1-53-26-0216
- [SDR HNAA2026052000393](https://openairdocs.org/sdr/HNAA2026052000393.md): Door Sill · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Structure
  > GALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS CORROSION IN MULTIPLE AREAS. GALLEY FLOOR SERVICE DOOR FUSELAGE CUT-OUT LOWER CENTER SILL HAS CORROSION IN MULTIPLE AREAS. MECHANICALLY MEASURED RH OUTBOARD (4) NUT PLATES ON GALLEY FLOOR SERVI
- [SDR HNAA2026052000392](https://openairdocs.org/sdr/HNAA2026052000392.md): Seat Track · corroded · Apr 13, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > F118708 L/H UPPER SEAT TRACK #1 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.
- [SDR HNAA2026052000391](https://openairdocs.org/sdr/HNAA2026052000391.md): Floor Support · corroded · Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL 3 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT FLOOR SILL 3 IAW SRM 51-40-02.
- [SDR HNAA2026052000390](https://openairdocs.org/sdr/HNAA2026052000390.md): Floor Support · corroded · Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL 4 HAVE CORROSION IN MULTIPLE AREAS. R & R LT FLOOR SILL 4 IAW SRM 51-40-02.
- [SDR HNAA2026052000389](https://openairdocs.org/sdr/HNAA2026052000389.md): Floor Support · corroded · Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL 6 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT FLOOR SILL 6 IAW SRM 51-40-02.
- [SDR HNAA2026052000388](https://openairdocs.org/sdr/HNAA2026052000388.md): Seat Track · corroded · Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT UPPER SEAT TRACK 5 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 5 IAW AMM 53-01-06.
- [SDR HNAA2026052000387](https://openairdocs.org/sdr/HNAA2026052000387.md): Seat Track · corroded · Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > RT UPPER SEAT TRACK 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK 4 IAW AMM 53-01-06.
- [SDR HNAA2026052000408](https://openairdocs.org/sdr/HNAA2026052000408.md): Seat Track · corroded · Apr 11, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT UPPER SEAT TRACK 6 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 6 IAW AMM 53-01-06.
- [SDR HNAA2026052000386](https://openairdocs.org/sdr/HNAA2026052000386.md): Floor Support · corroded · Apr 11, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL 7 AROUND NUT-PLATES HOLES HAVE CORROSION. REMOVED AND REPLACED LT FLOOR SILL 7 IAW SRM 51-40-02.
- [SDR HNAA2026052000411](https://openairdocs.org/sdr/HNAA2026052000411.md): Shear Tie · cracked · Apr 10, 2026 · N655AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > F118310 CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L HAS CRACK. REMOVED AND INSTALLED NEW CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L IAW EMB-145 SRM 51-40-02.
- [SDR HNAA2026052000410](https://openairdocs.org/sdr/HNAA2026052000410.md): Shear Tie · corroded · Apr 10, 2026 · N655AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP ABOVE LWR CENTER SILL IS CORRODED. RE-ACCOMPLISHED CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP SPLICE PATCH REPAIR ABOVE LWR CENTER SILL IAW ETD2016-145-072133 AND SRM 53-31-04RE, ITEM4. AND EO1-53-26-0224.
- [SDR HNAA2026052000409](https://openairdocs.org/sdr/HNAA2026052000409.md): Hinge Fitting · worn · Apr 10, 2026 · N655AE · Emb EMB145LR · Rudder Structure
  > RUDDER I UPPER HINGE ATTACHMENT FITTING TRIANGLE FITTING ATTACHMENT TANGS WORN. REMOVED AND REPLACED WORN RUDDER I UPPER HINGE ATTACHMENT FITTING/ TRIANGLE FITTING ASSY IAW SRM 51-40-02 AND AMM 20-10-01. EASI 4484. PAINTED FASTENERS AS REQUIRED IAW CPM 51-21-
- [SDR HNAA2026052000407](https://openairdocs.org/sdr/HNAA2026052000407.md): Door Sill · corroded · Apr 10, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IAW SRM 51-40-02.
- [SDR HNAA2026052000429](https://openairdocs.org/sdr/HNAA2026052000429.md): Yoke · cracked · Apr 9, 2026 · N655AE · Emb EMB145LR · Engine Mount Section
  > RIGHT ENGINE YOKE LOWER FWD FITTING HAS A POSSIBLE CRACK. REMOVED AND REPLACED CRACKED RT ENGINE YOKE LOWER FWD FITTING IAW PDT FCD1-54-21-0017 REV D.
- [SDR HNAA2026052000428](https://openairdocs.org/sdr/HNAA2026052000428.md): Skin · scratched · Apr 8, 2026 · N655AE · Emb EMB145LR · Rudder, Plate/Skin
  > RUDDER 2 RH EXTERNAL SKIN HAS A DEEP SCRATCH. PERFORMED DOUBLER REPAIR ON RUDDER 2 RH EXTERNAL SKIN IAW ETD2026-145-006765 AND EO1-55-26-0208.
- [SDR HNAA2026052000427](https://openairdocs.org/sdr/HNAA2026052000427.md): Skin · damaged · Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > POSSIBLE LIGHTNING STRIKE ON FUSELAGE EXTERNAL SKIN AT FR 37-38, STRG 6R-7R. PERFORMED DRILL OUT OF LIGHTNING STRIKE AREA AND REPAIRED WITH SOLID BUTTON HEAD RIVET AND WASHER PER EMB 145 SRM 53-00-01,ITEM 2, FIG 201, SHEET 1 AND 2.
- [SDR HNAA2026052000426](https://openairdocs.org/sdr/HNAA2026052000426.md): Skin · damaged · Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > POSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR33-34, STRG 5R-6R. PREPPED PRIMED AND PAINTED FUSELAGE SKIN FR 33-34, STRG 5R-6R IAW EMB 145 CPM 51-21-05 AND 51-21-06 51-21-03 AND PIEDMONT DRAWING AE-ERJ145-IR PIEDMONT BULLETIN CPM 51-02
- [SDR HNAA2026052000425](https://openairdocs.org/sdr/HNAA2026052000425.md): Skin · damaged · Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > POSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR-25-26, STRG 6R-7R. PERFORMED RIVET AND WASHER IN AFFECTED HOLE ON EXTERNAL FUSELAGE SKIN BTW FR 25-26 AND BTW STR 6R-7R IAW ETD 2026-145-0, SRM 53-00-01, ITEM 2, FIG 201, SHEET 1 AND 2 AND EO1-53-26-0239
- [SDR HNAA2025052000424](https://openairdocs.org/sdr/HNAA2025052000424.md): Drag Angle · cracked · Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage, Stabilizer Attach Fittings
  > RIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.
- [SDR HNAA2026052000423](https://openairdocs.org/sdr/HNAA2026052000423.md): Skin · dented · Apr 6, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L HAS A DENT. INSTALLED REPAIR DOUBLER & FILLER ON FUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L IAW SRM 53-12-01 RE, ITEM 2, FIGURE 201. AND EO1-53-26-0226.
- [SDR HNAA2025092300637](https://openairdocs.org/sdr/HNAA2025092300637.md): Hydraulic Line · leaking · Sep 22, 2025 · N655AE · Emb EMB145LR · Hydraulic System, Main
  > ENGINE HYD 1 PUMP FAIL & HYD 1 LOW QTY. PERFORMED GVI INSPECTION ENG #1 DUE TO SUSPECTED ENG #1 HYD LEAD. FOUND ABUNDACE OF HYD FLUID IN COWLING. SUSPECTED HYD RETURN LINE. FURTHER TROUBLESHOOTING REQUIRED. R & R NR 1 EDHP IRW AMM 29-10-03. OPS & LEACH CHEC
- [SDR HNAA2025050700306](https://openairdocs.org/sdr/HNAA2025050700306.md): Fuel Nozzle · faulted · May 6, 2025 · N655AE · Emb EMB145LR · Fuel Injector Nozzle
  > HUNG START ON NO.2 FOLLOWED BY FUEL SMELL IN A/C. PERFORMED GVI OF ENG 2 NO OBVIOUS DEFECTS NOTED OTHER THAN POOLED FUEL. DRY MOTORED ENG TO CLEAR OUT FUEL. DURING DRY MOTOR CONSTANT FUEL SPRAY WAS NOTED AT THE 6 OCLOCK POSITION WITH A 0 FUEL FLOW INDICATION
- [SDR HNAA2025041400202](https://openairdocs.org/sdr/HNAA2025041400202.md): Fuse · leaking · Apr 13, 2025 · N655AE · Emb EMB145LR · Hydraulic Indicating System
  > HYD 2 QTY IS EMPTY. HYD 2 WAS FULL AT PUSH BACK EMPTY BY GATE RETURN. FOUND #400 HYDRAULIC FUSE LEAKING. R&R #400 HYDRAULIC FUSE IAW AMM 32-41-07. LEAK CHECK AND OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N655AE/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 = 'N655AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N655AE/reports

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