# Service difficulty reports: N634AE

A list on [N634AE](https://openairdocs.org/aircraft/N634AE.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 · 138 reports

- [SDR HNAA2023102300366](https://openairdocs.org/sdr/HNAA2023102300366.md): Unknown · unknown · Oct 22, 2023 · N634AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT STRIP IS DIM FROM ROW 8 TO 12. R&R'D EMERGENCY LIGHT #3 BATTERY IAW WORKCARD 33-70-19
- [SDR HNAA2023081700310](https://openairdocs.org/sdr/HNAA2023081700310.md): Unknown · unknown · Aug 17, 2023 · N634AE · Emb EMB145LR · Drag Control System
  > SPOILER FAIL SPOILER OLPEN INDICATION ON EICAS AFTER TAKE-OFF. VISUALLY CONFIRMED SPOILERS WERE NOT OPEN. MESSAGE STAYED ENTIRE FLIGHT. CHECKED CMC AND FOUNS INBD PROX SWITCH FAIL. TESTED PROX SWITCHES & HARNESS WITH TEST BOX, NO DEFECTS NOTED. DEOXITED C/P'
- [SDR HNAA2023072500253](https://openairdocs.org/sdr/HNAA2023072500253.md): Unknown · unknown · Jul 25, 2023 · N634AE · Emb EMB145LR · Drag Control System
  > SPOILER FAIL MSG ON EICAS AFTER TAKEOFF, SPOILERS WERE OPENED AND STAYED OPEN. T/S PER FIM TASK 27-63-00-800-806-A, BLOCKS 1 TO 5,15, 21 GROUND SPOILER VALVE FOUND TO BE DEFECTIVE PER FIM R&R GROUND SPOILER VALVE IRT AMM 27-62-03. OPS CHECK / LEAK CHECK GOOD
- [SDR HNAA2023071800249](https://openairdocs.org/sdr/HNAA2023071800249.md): Unknown · unknown · Jul 18, 2023 · N634AE · Emb EMB145LR · Flight Control System
  > DURING TAKEOFF SPOILER FAIL DISPLAYED ON EICAS. WITH SPOILER I/B FAIL DISPLAYED ON CMC. FOUND "SPOILER IB FAIL" ON CMC. INSPECTED I/B SPOILERS PROX SENSORS WITH NO DEFECTS NOTED. REMOVED AND REPLACED RELAYS K0059 AND K0362 IN REF TO AMM 20-13-000/400-801-A
- [SDR HNAA2021022500056](https://openairdocs.org/sdr/HNAA2021022500056.md): Skin · dented · Feb 20, 2021 · N634AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS 2 DENTS BETWEEN FRAMES 12-13, STRINGERS 20--21L. COMPLETED INSTALLING REPAIR DOUBLER AND FILLER ON EXTERNAL FUSELAGE SKIN NR 4 BETWEEN FRAMES 12-13, STRINGER 20-21L IAW ETD2021-145-001545 AND EO1-53-21-027. DENT NR 3 ACCEPTED AS IS
- [SDR HNAA2021022500059](https://openairdocs.org/sdr/HNAA2021022500059.md): Flange · bent · Feb 5, 2021 · N634AE · Emb EMB145LR · Leading Edge Devices
  > RIGHT NR 1 WING LEADING EDGE UPPER ATTACHMENT FLANGE BENT-NRWC E838627. REPAIRED RT NR 1 WING LEADING EDGE BY INSTALLING (MS20426AD8), DRILLED AND COUNTERSUNK FOR SCREW IAW ETD2021-145-000134 REV.: A AND EO1-57-21-0026 SEE TURNOVER FOR DETAILS.
- [SDR HNAA2021022500057](https://openairdocs.org/sdr/HNAA2021022500057.md): Skin · cracked · Feb 5, 2021 · N634AE · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR EXTERNAL HANDLE CUTOUT HAS A POSSIBLE CRACK AT THE AFT END. CUT OUT CRACKED AREA OF CARGO DOOR SKIN AT AFT END OF HANDLE, FABRICATED EXTERNAL DOUBLER AND FILLER, INSTALLED FILLER AND DOUBLER ON CARGO DOOR REPAIR IAW ETD2021-145-002383 AND PIEDMONT
- [SDR HNAA2021022500058](https://openairdocs.org/sdr/HNAA2021022500058.md): Profile · corroded · Feb 1, 2021 · N634AE · Emb EMB145LR · Fuselage Main, Structure
  > FR 65 L-SHAPE PROFILE IS CORRODED ON THE LOWER END JUST ABOVE THE DOOR. PERFORMED REPAIR OF FR 65 L-SHAPE PROFILE ON THE LOWER END JUST ABOVE THE DOOR SILL IAW EMB 145 SRM 53-31-04 ITEM 4,FIG 212 AND PIEDMONT EO1-53-21-0029.
- [SDR HNAA2020091800256](https://openairdocs.org/sdr/HNAA2020091800256.md): Carbon Seal · leaking · Sep 18, 2020 · N634AE · Emb EMB145LR · Engine (Turbine/Turboprop)
  > THIS WAS THE FIRST OF 2 CABIN ODOR EVENTS ASSOCIATED WITH THIS AIRCRAFT/ENGINE. INITIAL TROUBLESHOOTING (INCLUDING BORESCOPE OF THE COMPRESSOR) DID NOT FIND ANY FAULTS RELATED TO THE ENGINE AND THE AIRCRAFT WAS RETURNED TO SERVICE. DURING FURTHER TROUBLESHOO
- [SDR HNAA2020081700247](https://openairdocs.org/sdr/HNAA2020081700247.md): Unknown · odor · Aug 15, 2020 · N634AE · Emb EMB145LR · Air Distribution System
  > FLIGHT DECK HAZY WITH PLASTIC SMELL ON CLIMB OUT BUT NO SMOKE. MAINTENANCE: DISPLACED POWER DISTRIBUTION AND RELAY PANELS IN FLIGHT DECK FOR INSPECTION, DETAILED VISUAL RE-INSTALLED ALL PANELS. DISPLACED GLARESHIELD FOR VISUAL INSP. RESECURED GLARESHIELD. RAN
- [SDR HNAA2020081700245](https://openairdocs.org/sdr/HNAA2020081700245.md): Unknown · odor · Aug 14, 2020 · N634AE · Emb EMB145LR · Air Distribution System
  > DURING TAKEOFF AND THROUGHOUT FLIGHT FUMES NOTED IN COCKPIT AND CABIN WITH BOTH PACKS IN AUTO AND APU OFF. CREW NOTICED THAT LH SIDEWALL AND CEILING PANEL AT ROW 15 TURNED ORANGE. SEE LOG PAGE 216382-3 FOR NEW DISCREPANCY. #1 ENG OIL SMELL. (LG PG 216382 SEQ.
- [SDR HNAA2020081100243](https://openairdocs.org/sdr/HNAA2020081100243.md): Unknown · smoke · Aug 10, 2020 · N634AE · Emb EMB145LR · Air Distribution System
  > ABORTED TAKEOFF DUE TO SMOKE IN FLIGHT DECK AND CABIN. CREW REPORTED OILY AND ELECTRICAL ODOR TO THE SMOKE. ABORTED AT 80 KNOTS. OPEN
- [SDR HNAA2020081000242](https://openairdocs.org/sdr/HNAA2020081000242.md): Unknown · odor · Aug 8, 2020 · N634AE · Emb EMB145LR · Air Distribution System
  > FLIGHT DECK HAD CHEMICAL ODOR DURING CLIMB OUT AND GOT WORSE ON DECENT WITH NO VISABLE SMOKE. BLEEDS AND PACKS WERE ON. CABIN AREA HAD NO ODOR. RAN PACKS FOR 30 MINUTES WITH APU AND 30 MINUTES WITH BOTH ENGS IAW AMM 21-00-00 NO ODORS OR DEFECTS NOTED AT THIS
- [SDR HNAA2020030900090](https://openairdocs.org/sdr/HNAA2020030900090.md): Valve · failed · Mar 8, 2020 · N634AE · Emb EMB145LR · Pneumatic Distribution System
  > ON TAKEOFF ATTEMP, AT 65KNOTS, GOT HIGH STAGE VLV 2 FAIL EICAS MESSAGE. REMOVED PANEL 422BT TO FOM. R/R'D #2 HIGH STAGE VALVE REF AMM 36-11-02. OPS CGHECK GOOD. LEAK CHECK AND FUNCTION CHECK GOOD. REINSTALLED PANEL 422BT. OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2020020500046](https://openairdocs.org/sdr/HNAA2020020500046.md): Warning Message · illuminated · Feb 4, 2020 · N634AE · Emb EMB145LR · Fire Detection
  > ON CLIMB OUT E1 FIRE DETECTION FAIL MESSAGE ON EICAS. DISCREPANCY IS STILL IN WORK AT THIS TIME.
- [SDR HNAA2020011700020](https://openairdocs.org/sdr/HNAA2020011700020.md): Warning Message · false activation · Jan 15, 2020 · N634AE · Emb EMB145LR · Central Warning
  > ON T/O ROLL EICAS CAUTION MESSAGE FOR HIGH STAGE VALVE 1 0R 2 FAILED. CAPTAIN SAID HE DID NOT KNOW FOR SURE WHICH IT WAS. AND MESSAGE WENT AWAY, WITH NO CMC MESSAGE.NO EICAS MESSAGE TO CONFIRM....FIX: CREW GROUND RAN A/C.C/W AMM 36-11-02-700-801-A.OPS CHECK GO
- [SDR HNAA2020011530017](https://openairdocs.org/sdr/HNAA2020011530017.md): Warning Message · false activation · Jan 14, 2020 · N634AE · Emb EMB145LR · Fire Detection
  > ON TAKE-OFF, E1 FIRE DET FAIL, EICAS CAUT MESS, PERFORMED QRH, MESS EXTINGUISHED. PERFORMED FIRE DETECTION SYSTEM OPERATIONAL CHECK PER AMM 26-10-00-700-802-A. OPS GOOD,NO DEFECTS NOTED. A/C OK FOR SERVICE.
- [SDR HNAA2019060300158](https://openairdocs.org/sdr/HNAA2019060300158.md): Warning Light · false activation · May 30, 2019 · N634AE · Emb EMB145LR · Airfoil Anti/De-ice System
  > WING A/I FAIL IN CONJUCTION WITH WING ICE CONDITION, NO A/I EICAS WARNING FOLLOWED BY STAB A/I FAIL AND BLEED LOW TEMP EICAS MESSAGES. EICAS MESSAGES PERSISTED IN ICING CONDITION. MDT PERFORMED CROSS BLEED START FROM NR 1 ENGINE TO NR 2 ENGINE IAW AMM 71-00-
- [SDR HNAA2019043000124](https://openairdocs.org/sdr/HNAA2019043000124.md): Button · loose · Apr 28, 2019 · N634AE · Emb EMB145LR · Pneumatic Distribution System
  > PDIS 634 36-10 2040022 28APR19 PHL CLOSE BLD 1 VLV CLSD ON TAKEOFF. 28569 00 VAG HISTORY: YES FACT 28APR19 18:03 PHL INSP #1 BLEED PUSH BUTTON, FOUND TO BE LOOSE. REINSTALLED IAW EMB 14
- [SDR HNAA2019043000123](https://openairdocs.org/sdr/HNAA2019043000123.md): Sensor · failed · Apr 27, 2019 · N634AE · Emb EMB145LR · Pneumatic Indicating System
  > PDIS 634 36-21 2040011 27APR19 PHL CLOSE BLD 1 VLV CLSD ADVISORY MESS ON T/O. C/W QRH. 28370 00 LLS RETURN TO FIELD 00 HISTORY: SWAPPED TO 672. FACT 27AP
- [SDR HNAA2019042600121](https://openairdocs.org/sdr/HNAA2019042600121.md): Warning Message · false activation · Apr 24, 2019 · N634AE · Emb EMB145LR · Compressor Bleed Valve
  > PDIS 634 36-12 1846482 24APR19 PWM CLOSE BLEED 1 VALVE CLOSED MESSAGE ON TAKEOFF. C/W QRH. FACT 24APR19 11:36 PWM CHECKED CMC FOR MESSAGES. NO RELEVANT MESSAGES NOTED. C/W AMM TASK 36-11-05-700-802-A. NO
- [SDR HNAA2019030100053](https://openairdocs.org/sdr/HNAA2019030100053.md): Warning System · false activation · Feb 28, 2019 · N634AE · Emb EMB145LR · Pneumatic Indicating System
  > HSV 2 VLV FAIL MSG ON TAKEOFF FLASHED AND SELF-CLEARED. GROUND RAN NO.2 WITH BLEEDS ON NO DEFECTS OR MESSAGES NOTED CND OKAY FOR SERVICE AT THIS TIME.
- [SDR HNAA2019020600035](https://openairdocs.org/sdr/HNAA2019020600035.md): Warning System · false activation · Feb 5, 2019 · N634AE · Emb EMB145LR · Pneumatic Indicating System
  > ABORTED T/O DUE TO HS 2 VLV MSG FLASHED AND SELF CLEARED. C/W QRH AND NO MSG NOTED.
- [SDR HNAA2019010700009](https://openairdocs.org/sdr/HNAA2019010700009.md): Light · inoperative · Jan 4, 2019 · N634AE · Emb EMB145LR · Emergency Lighting
  > NDIS 634 33-51 0019600 04JAN19 RIC CLOSE MAIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE. FACT 04JAN19 10:12 RIC. R/R THE EMERGENCY LIGHT ASSEMBLY IAW AMM TASK 33-30-01-000/400-801-A. OPS CHECK GOOD. OK FOR SERVICE. P/N ON: LIGHT ASSY 136245-305 S/N: - P/N OFF:
- [SDR HNAA2018122100326](https://openairdocs.org/sdr/HNAA2018122100326.md): Bulb · inoperative · Dec 20, 2018 · N634AE · Emb EMB145LR · Emergency Lighting
  > MAIN DOOR EMERGENCY LIGHT INOP. R&R LIGHT BULB
- [SDR HNAA2018111600284](https://openairdocs.org/sdr/HNAA2018111600284.md): Wire · broken · Nov 15, 2018 · N634AE · Emb EMB145LR · Light System Wiring
  > DISCREPANCY: WIRE OF THE EMERGENCY LIGHT AT SERVICE DOOR IS BROKEN. ACTION TAKEN: R&R WIRE CONNECTOR ON MALE SIDE OF CONNECTOR FOR EMERGENCY LIGHT AT SERVICE DOOR IAW SWPM 20-50-00.
- [SDR HNAA2018092600229](https://openairdocs.org/sdr/HNAA2018092600229.md): None · none · Sep 21, 2018 · N634AE · Emb EMB145LR · Standard Practices/Structures
  > PDIS 634 05-51 1691272 21SEP18 ILM CLOSE BIRD STRIKE R/H SIDE OF NOSE AREA, NO EVIDENCE OF IN GESTION NOTICED 21584 00 EK FACT 21SEP18 00:22 ILM ACCOMPLISH DETAILED VISUAL IN
- [SDR HNAA2018081300195](https://openairdocs.org/sdr/HNAA2018081300195.md): Light · inoperative · Aug 11, 2018 · N634AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY FLOOD LIGHT ON SERVICE DOOR WAS INOPERATIVE. R & R THE EMERGENCY FLOOD LIGHT ASSEMBLY. OPS CHECKED GOOD.
- [SDR HNAA2018081300194](https://openairdocs.org/sdr/HNAA2018081300194.md): Ground Wire · dirty · Aug 11, 2018 · N634AE · Emb EMB145LR · Light System Wiring
  > EMERGENCY FLOOD LIGHT ON MAIN DOOR WORKS INTERMITTENLY. CLEANED THE GROUND WIRE AND ADJUSTED THE GROUND WIRE ON THE EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2018081300193](https://openairdocs.org/sdr/HNAA2018081300193.md): Light · damaged · Aug 11, 2018 · N634AE · Emb EMB145LR · Emergency Lighting
  > RIGHT EMERGENCY LIGHT WAS INOPERATIVE. INSPECTED AND FOUND THE BULB MOVED INSIDE THE ASSEMBLY. R & R LIGHT ASSY IAW AMM 33-50-10-000-801-A SECTION M AND 33-50-10-400-801-A, SECTION L. OPS CHECKED GOOD.
- [SDR HNAA2018070600140](https://openairdocs.org/sdr/HNAA2018070600140.md): Crossbeam · corroded · Jun 12, 2018 · N634AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > GALLEY CROSSBEAM AT FRAME 20 CORRODED. INSTALLED 3 NUTPLATES ON GALLEY CROSSBEAM AT FRAME 20 IAW SRM 51-40-09.
- [SDR HNAA2018070600139](https://openairdocs.org/sdr/HNAA2018070600139.md): Fitting · corroded · Jun 12, 2018 · N634AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TWO LT APU FIRE WALL SHEER CLIPS INSIDE 312AR HAVE SURFACE CORROSION. REMOVED AND REPLACED TWO APU FIRE WALL SHEER CLIPS INSIDE 312AR IAW SRM 51-40-02.
- [SDR HNAA2018070600138](https://openairdocs.org/sdr/HNAA2018070600138.md): Structure · corroded · Jun 10, 2018 · N634AE · Emb EMB145LR · Service Doors
  > SERVICE DOOR LOWER FWD NUT PLATE HOLE CORROSION. PERFORMED HFEC INSPECTIONS AND UT THICKNESS IAW EASI NDTM NO CRACK NOTED. BLENDED SERVICE DOOR LOWER FWD NUT PLATE HOLE TO REMOVE CORROSION IAW SRM 51-10-03, BLENDED AREA ACCEPTED AS IS IAW EO1-52-18-0239 AND ET
- [SDR HNAA2018070600137](https://openairdocs.org/sdr/HNAA2018070600137.md): Door Frame · corroded · Jun 10, 2018 · N634AE · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR FWD UPPER TWO NUTPLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC INSPECTION AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLES, FILLERS AND SHIM ON 2 LOWER NUTPLATE HOLES ON CARGO DOOR FWD FRAME IAW SRM 52-30-04. REPAIRED
- [SDR HNAA2018070600136](https://openairdocs.org/sdr/HNAA2018070600136.md): Structure · corroded · Jun 10, 2018 · N634AE · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR FWD LOWER NUT PLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. CARGO DOOR FWD LOWER NUT PLATE PROFILE IAW SRM 51-40-02.
- [SDR HNAA2018070600133](https://openairdocs.org/sdr/HNAA2018070600133.md): Structure · corroded · Jun 10, 2018 · N634AE · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR NUT PLATE HOLE HAS SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM NO DEFECTS NOTED. R&R CARGO DOOR UPPER SURFACE ANGLE PROFILE IAW SRM 51-40-02.
- [SDR HNAA2018041800082](https://openairdocs.org/sdr/HNAA2018041800082.md): Light · inoperative · Apr 16, 2018 · N634AE · Emb EMB145LR · Emergency Lighting
  > RT SERVICE DOOR EMERGENCY LIGHT INTERMITTENT. R & R THE LIGHT ASSY.
- [SDR HNAA2018033000077](https://openairdocs.org/sdr/HNAA2018033000077.md): Light · unknown · Mar 28, 2018 · N634AE · Emb EMB145LR · Emergency Lighting
  > REAR OVERHEAD AND AISLE EMERGENCY LIGHT WILL NOT ILLUMINATE. INSPECTED THE OVERHEAD & AISLE EMERGENCY LIGHTS, NO DEFECTS NOTED. OPS CHECKED GOOD IAW AMM 33-50-00-700-801-A.
- [SDR HNAA2017013000029](https://openairdocs.org/sdr/HNAA2017013000029.md): Anti-Ice System · malfunctioned · Jan 30, 2017 · N634AE · Emb EMB145 · Airfoil Anti/De-ice System
  > ON DESCENT, IN ICING CONDITIONS, WING ANTI-ICE FAIL EICAS CAUTION MESSAGE APPEARED ON QRH, STAB ANTI-ICE FAIL CAUTION AND ICE CONDITION ANTI-ICE INOP WARNING APPEARED. PERFORMED ANTI-ICE SYSTEM OPS CHECKED IAW MM 30-00-00-700-802 AND ANTI ICE VALVE OPS CHECK
- [SDR HNAA2017010400005](https://openairdocs.org/sdr/HNAA2017010400005.md): Warning Light · illuminated · Jan 4, 2017 · N634AE · Emb EMB145 · Airfoil Anti/De-ice System
  > ICE DETECTION PNEUMATIC ON GROUND CHECK, ICAS MESSAGE ENG, A/I DISAGREE. ILLUMINATES DURING TEST AND THEN EXTINGUISHES AFTER TEST IS COMPLETE. REMOVED AND REPLACED FIM.
- [SDR HNAA2017010400004](https://openairdocs.org/sdr/HNAA2017010400004.md): Warning Light · false activation · Jan 4, 2017 · N634AE · Emb EMB145 · Airfoil Anti/De-ice System
  > ABORTED TAKEOFF DUE TO ICE CONDITION ADVISORY AND ANTI ICE INOPERATIVE WARNING MESSAGE. GROUND RAN, OPS CHECKED NORMAL. IAW FIM 30-80-810-801-A AND MM 30-00-700-801-A.
- [SDR HNAA2016111600350](https://openairdocs.org/sdr/HNAA2016111600350.md): Lamp · inoperative · Nov 16, 2016 · N634AE · Emb EMB145 · Emergency Lighting
  > EMERGENCY LIGHT OVER THE WING ON THE RIGHT SIDE IS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW MM 33-50-10. OPS CHECKED GOOD.
- [SDR HNAA2016091400281](https://openairdocs.org/sdr/HNAA2016091400281.md): Indication Sys · reads high · Sep 12, 2016 · N634AE · Emb EMB145LR · Fuel Quantity Indicator
  > DURING CLIMB AT 7000 FEET, AN EICAS MESSAGE ILLUMINATED FOR FUEL INBALANCE. DURING RETURN TO FIELD, THE RT TANK SHOWED LOWER QUANTITY BY VARIOUS AMOUNTS STARTING AT 800 LBS AND DECREASING TO 300 LBS. NO LEAKS NOTED AFTER LANDING. MX COMPLIED WITH MAGNA STI
- [SDR HNAA201662000189](https://openairdocs.org/sdr/HNAA201662000189.md): Actuator · malfunctioned · Jun 19, 2016 · N634AE · Emb EMB145 · Elevator Control System
  > TRIM MAIN INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS DURING CLIMB OUT 41500. R & R THE HSCU, NO FIX. CAN RESET P TRIM INDICATION WITH TRIM FULL DOWN. FAIL, WHEN TRIM GOES UP BEFORE FIRST CARROT. INSTALLED IAW AMM TASK 27-40-01-400-801-A.
- [SDR HNAA2016062000189](https://openairdocs.org/sdr/HNAA2016062000189.md): Not Reported · malfunctioned · Jun 19, 2016 · N634AE · Emb EMB145LR · Stabilizer Control System
  > PTRM MAIN INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS DURING CLIMBOUT. T/S PTRIM MAIN INOPERATIVE R & R HSCU. NO FIX. CAN RESET PTRIM INDICATION WITH TRIM FULL DOWN. FAIL, WHEN TRIM GOES UP BEFORE FIRST CARROT. INSTALLED IAW AMM TASK 27-40-01-400-80
- [SDR HNAA2016062000188](https://openairdocs.org/sdr/HNAA2016062000188.md): Switch · failed · Jun 18, 2016 · N634AE · Emb EMB145 · Stabilizer Control System
  > PTRIM MAIN INOPERATIVE, WARNING MESSAGE APPEARED ON EICAS IN FLIGHT WITH AUTOPILOT ON. QRH PROCEDURE WAS FOLLOWED AND BACKUP SYS OPERATED NORMALLY. T/S PTRIM MAIN INOPERATIVE IAW 24-43-00-810-801-A AND FOUND MAIN SYS CUTOUT SWITCH FAILED STEP 8 SUBTASK 817-0
- [SDR HNAA2016060600163](https://openairdocs.org/sdr/HNAA2016060600163.md): Acm · failed · Jun 5, 2016 · N634AE · Emb EMB145 · Cabin Cooling System
  > IN ICING CONDITIONS AT CRUISE CREW NOTICED A BURNING ODOR IN THE COCKPIT AND FWD GALLEY AREA AND AFTER LANDING PACK 2 OVERHEAT AND PACK 2 OVLD EICAS MESSAGES APPEARED. DURING T/S MX FOUND METAL SHAVINGS AT OUTLET SCREEN NR 2 PACK. PERFORMED FIM TASK FOR SMOK
- [SDR HNAA2016052400148](https://openairdocs.org/sdr/HNAA2016052400148.md): Unknown · odor · May 21, 2016 · N634AE · Emb EMB145LR · Air Conditioning System
  > UPON LEVELING OUT FROM DESCENT WHEN THRUST LEVER ADVANCED, SMOKE ODOR COMING FROM VENTS. POSSIBLE ELECTRICAL SMOKE ODOR FOR 1-2 MINUTES. INSPECTED ACFT. GROUND POWER RAN ACFT IN TAKEOFF AND CRUISE CONDITIONS FOR SEVERAL MINUTES. OPS CK GOOD NO DEFECTS NOTED
- [SDR HNAA2016031600085](https://openairdocs.org/sdr/HNAA2016031600085.md): Line · leaking · Mar 18, 2016 · N634AE · Emb EMB145LR · Hydraulic System, Main
  > NR 1 HYDRAULIC LOST EICAS MESSAGE, HYDRAULIC LOW QTY. FOUND GEAR ACTUATOR DOWN LINE LEAKING. FERRIED ACFT.
- [SDR SIMA20160126005](https://openairdocs.org/sdr/SIMA20160126005.md): Skin · cracked · Jan 26, 2016 · N634AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > RIGHT UPPER FUSELAGE SKIN CRACKED 2 PLACES, CRACK 1 IS JUST AFT OF FRAME 75, JUST ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. CRACK 2 IS ON FRAME 75, AT THE FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 1/4". EASI 8071 USED, 100-500 KHZ PROBE, FRE

Next page: https://openairdocs.org/aircraft/N634AE/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 = 'N634AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N634AE/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.