# Service difficulty reports: N638AE

A list on [N638AE](https://openairdocs.org/aircraft/N638AE.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 · 156 reports

- [SDR HNAA2022091200258](https://openairdocs.org/sdr/HNAA2022091200258.md): None · none · Sep 9, 2022 · N638AE · Emb EMB145LR · Rudder Control System
  > PDIS 638 27-22 2677131 09SEP22 CLT CLOSE RUD SYS 2 INOP INFLIGHT FACT 09SEP22 10:53 CLT C/W FIM 27-22-00-810-802A STEPS 1,2,3 R/R W RUDDER SYSTEMS PRESSURE SWITCH IN REF TO AMM 27-23-04 OPS AND LEAK CHECK GOOD OK FOR SERVICE
- [SDR HNAA2022050700177](https://openairdocs.org/sdr/HNAA2022050700177.md): None · none · May 18, 2022 · N638AE · Emb EMB145LR · Air Conditioning System
  > PDIS 638 21-01 2514801 19MAY22 AVL CLOSE BURNING FUMES COMING FROM PACKS. FACT 20MAY22 17:18 ROA #2 PACK VLV R&R'D, SEE LP 251481-2 FOR SIGNOFF. R&R'D #1 ACM IAW AMM 21-51-03-04. OPS AND LEAK CHECK GOOD. NO SMOKE OR SMELL AT
- [SDR HNAA2021120200593](https://openairdocs.org/sdr/HNAA2021120200593.md): None · none · Nov 30, 2021 · N638AE · Emb EMB145LR · Pneumatic Indicating System
  > PDIS 638 36-21 2745471 30NOV21 ROA CLOSE BLEED 2 LEAK MSG IN FLIGHT FACT 30NOV21 12:33 ROA C/W FIM TASK 36-20-00-810-802 INSPECTED AND FOUND V BAND CLAMP ON IB SIDE OF Y PIPE IN PYLON LOOSE REMOVED AND REPLACED CLAMP PER AMM 3
- [SDR HNAA2021071500324](https://openairdocs.org/sdr/HNAA2021071500324.md): Control Cable · frayed · Jul 15, 2021 · N638AE · Emb EMB145LR · Elevator Control System
  > FLIGHT CREW: WHEN DOING THE FLIGHT CONTROL CHECK (FWD AND AFT) CREW FELT A STICKING POINT. MAINTENANCE: DISCOVERED THAT THE ELEVATOR SERVO BRACKET CABLE WAS CORRODED AND FRAYED. REMOVED AND REPLACED ELEVATOR SERVO BRACKET ASSEMBLY AND TENSIONED CABLE IAW 27-31
- [SDR HNAA2021070600312](https://openairdocs.org/sdr/HNAA2021070600312.md): Unknown · odor · Jul 4, 2021 · N638AE · Emb EMB145LR · Air Distribution System
  > COMING THROUGH 31K FEET. STRONG ODER NOTICED IN COCK PIT/CABIN. DISSIPATED GOING BACK THROUGH 31K FEET. OCCURRING INTERMITTENTLY ON DESCENT. COULD DUPLICATE ON GROUND WITH PACKS. INSPECTED RELAY AND DISTRIBUTION BOX PANELS, NO DEFECTS NOTED. R/R'D #2 RE-CIRCUL
- [SDR HNAA2021063000296](https://openairdocs.org/sdr/HNAA2021063000296.md): Pump · faulted · Jun 28, 2021 · N638AE · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main
  > IN CRUISE FLIGHT AT 10K, $2 HYD PSI SPIKED TO 3,800 PSI FOLLOWED BY LOSS OF #2 HYD QUNTY AND SYSTEM PSI DROPPED TO ZERRO. ELECTRIC DRIVEN PUMP TURNED OFF AFTER 5 TO 10 MINUTES. (EICAS MESSAGE OF HYD SYS 2 FAIL). REMOVED AND REPLACED #2 HYD ENG DRIVEN PUMP IAW
- [SDR HNAA2021041200135](https://openairdocs.org/sdr/HNAA2021041200135.md): Ecs · odor · Apr 10, 2021 · N638AE · Emb EMB145LR · Air Distribution System
  > PDIS 638 21-01 2554732 10APR21 CMI CLOSE BURNING SMELL AT 100 KNOTS IN COCKPIT QUICKLY DISSIPATED AFTER REJECTED TAKE OFF, FACT 11APR21 04:10 CMI PERFORMED FIM 21-20-00-810-801-A. NO DEFECTS NOTED NO BURNING SMELL FOUND. GROUND RAN ENG AND PACK TO FULL P
- [SDR HNAA2021010400001](https://openairdocs.org/sdr/HNAA2021010400001.md): A/C Pack · overheated · Jan 1, 2021 · N638AE · Emb EMB145LR · Cabin Cooling System
  > POOR AIR FLOW COCKPIT AND PACK 1 OVERHEAT WITH BURNING SMELL. OPERATED PACKS CORRECTLY, IAW AMM 21-00-00-810-001A AND FOLLOWED FIM TASK 21-51-00-810-803A AND CONFIRMED A TRANSITORY CONDITION CAUSED BY OPERATOR ERROR. OPERATIONS CHECK GOOD. AIRCRAFT OK FOR S
- [SDR HNAA2020121400361](https://openairdocs.org/sdr/HNAA2020121400361.md): Contactor · burned · Dec 13, 2020 · N638AE · Emb EMB145LR · APU System Wiring
  > PDIS 638 49-10 2346991 13DEC20 MDT CLOSE. WHEN PILOT TURNED ON HIS APU HE HAD SHED BUS 1 AND 2 OFF LINE FOLLOWED BY APU GEN OFF BUSS AND ELECTRICAL BURNING SMELL. FACT 13DEC20 23:10 MDT. APU LINE CONTACTOR SHOWS SIGNS OF BURN DAMAGE. R & R APU LINE CONTACT
- [SDR HNAA2020121200360](https://openairdocs.org/sdr/HNAA2020121200360.md): Starter Gen · malfunctioned · Dec 10, 2020 · N638AE · Emb EMB145 · Starter-Generator
  > APU GEN OFF BUS MESSAGE APPEARED ON EICAS WITH CLICKING NOISE AND ELECTRICAL BURNING SMELL IN COCKPIT. RESTARTED APU WITH GEN OFF NO SMELL NOTED OR CB S POPPED. R & R APU START GEN, IAW W/C 24-80-01. OPERATIONS CHECK GOOD.
- [SDR HNAA2020110500296](https://openairdocs.org/sdr/HNAA2020110500296.md): Sleeve · damaged · Nov 7, 2020 · N638AE · Emb EMB145LR · Air Distribution System
  > PDIS 638 21-01 2346581 07NOV20 PHL CLOSE. FOLLOWING A/I TEST IN FLT, F/A REPORTED RUSHING AIR NOISE FROM MIDDLE OF CABIN, BURNING SMELL NOTED SHORTLY AFTER. SHUT OFF PAC 1 AND NOISE AND SMELL DISAPATED. 36444 00 SMS FACT 07NOV20 09:53 PHL. R & R FLEX SLEEV
- [SDR HNAA2020090800253](https://openairdocs.org/sdr/HNAA2020090800253.md): Unknown · odor · Sep 7, 2020 · N638AE · Emb EMB145LR · Air Distribution System
  > PDIS 638 21-21 2416061 07SEP20 RIC CLOSE. STRONG CHEMICAL ODOR PRESENT IN COCKPIT. OBSERVED WITH PACKS RUNNING. FACT 07SEP20 06:21 RIC. R/R APU CONTACTOR K0291 IN REF TO AMM 24-60-01-000/400-801A. AS MAINTENANCE PRECAUTION R/R APU GCU IAW AMM 34-24-
- [SDR HNAA2020072100231](https://openairdocs.org/sdr/HNAA2020072100231.md): Contactor · burned · Jul 20, 2020 · N638AE · Emb EMB145LR · Fuel Boost Pump
  > ON ARRIVAL TO FLIGHT DECK, NOTICED PLASTIC, ELECTRICAL ODOR. MX FOUND CONTACTOR K0119 FOR 1A FUEL PUMP BURNED. ACFT HAS PRIOR HISTORY. R & R THE CONTACTOR IAW AMM 28-21-14. OPS CHECKED IAW AMM 28-45-00. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR HNAA2020071700194](https://openairdocs.org/sdr/HNAA2020071700194.md): Contactor · burned · Jul 16, 2020 · N638AE · Emb EMB145LR · DC Generating System
  > BURNING PLASTIC SMELL IN FLIGT DECK. FOUND BURNT CONTACTOR K0291 BEHIND LIFE VEST STORAGE PANEL. R/R CONTACTOR IAW AMM 24-34-04. OPS CHECK GOOD. OK FOR SERVICE. PERFORMED MAIN GENERATOR TEST IAW AMM 24-31-00.
- [SDR HNAA2020021400060](https://openairdocs.org/sdr/HNAA2020021400060.md): Wire · detached · Feb 13, 2020 · N638AE · Emb EMB145LR · Light System Wiring
  > EMERGENCY LIGHT ON MAIN DOOR INOP.... RE-ATTACHED WIRES TO THE ELECTRIC CONNECTORS FOR THE EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR HNAA2020012000023](https://openairdocs.org/sdr/HNAA2020012000023.md): Unknown · odor · Jan 18, 2020 · N638AE · Emb EMB145LR · Air Distribution System
  > AFTER TAKEOFF CREW NOTED PUNGENT ELECTRICAL/BURNING ODOR IN COCKPIT. SMELL CLEARD SHORTLY AFTER LANDING. MX T/S ISSUE IN REF TO FIM 21-20-00-810-801-A. NO DEFECTS NOTED. PERFORMED OPS CHECKS OF BOTH BLEED SYST EMS, BOTH PACK SYSTEMS AND ANTI ICING SYSTEMS
- [SDR HNAA2019102200313](https://openairdocs.org/sdr/HNAA2019102200313.md): Unknown · odor · Oct 20, 2019 · N638AE · Emb EMB145LR · Air Distribution System
  > PDIS 638 05-50 1995782 20OCT19 GSO CLOSE BURNING ODOR OBSERVED A 26,000 ICING CONDITIONS. SME LL DISSIPATED AT 5000 FT. FACT 20OCT19 13:37 GSO INSP LIGHTS AND PUSHBUTTONS IN COCKPIT NO DISCREPANC IES FOUND P
- [SDR HNAA2019091100267](https://openairdocs.org/sdr/HNAA2019091100267.md): Generator · malfunctioned · Sep 10, 2019 · N638AE · Emb EMB145LR · AC Generator-Alternator
  > GEN #3 SHOWING AMBER DASHES AND 0 AMPS DURING FLIGHT. FIX: R&R GEN 3 IAW AMM 24-31-01 LEAK AND OPS CHECK GOOD. NOTE: AIRCRAFT DIVERTED FROM YQB TO ALB TO BE FIXED.
- [SDR HNAA2019043000129](https://openairdocs.org/sdr/HNAA2019043000129.md): Wire · broken · Apr 28, 2019 · N638AE · Emb EMB145LR · Light System Wiring
  > NDIS 638 33-51 0011560 28APR19 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS INOP 30100 00 BAD FACT 28APR19 08:18 SBY R&R'D LAMP NO FIX. INSPECTED & FOUND BROKEN WIRE R&R P
- [SDR HNAA2019041700103](https://openairdocs.org/sdr/HNAA2019041700103.md): A/C Pack · odor · Apr 16, 2019 · N638AE · Emb EMB145LR · Cabin Cooling System
  > 638 21-01 2098402 16APR19 FLO CLOSE ON TAKEOFF FLIGHT DECK FILLED WITH SMELL.ON APPROACH SMELL/HAZE RETURNED AND DISAPATED BEFORE LANDING. 26803 00 SMK MEL 16APR19 14:25 FLO C10615 21-13
- [SDR HNAA2019012500028](https://openairdocs.org/sdr/HNAA2019012500028.md): Flap · out of rig · Jan 23, 2019 · N638AE · Emb EMB145LR · Trailing Edge Flap Control System
  > PDIS 638 27-50 2047071 23JAN19 PHL CLOSE FLAPS FAIL MSG IN FLT AFTER T/O WHEN SETTING FLAPS TO ZERO. FACT 24JAN19 22:25 PHL FOUND FLAPS TO BE OUT OF RIG. PERFORMED FLAP ZERO-DEGREE RIGGING IAW AMM 27-53-04. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2018103100270](https://openairdocs.org/sdr/HNAA2018103100270.md): Light · inoperative · Oct 30, 2018 · N638AE · Emb EMB145LR · Emergency Equipment
  > NDIS 638 33-51 0007300 30OCT18 RIC CLOSE AFT CABIN EMERGENCY FLASHLIGHT INOP 28629 00 NGR FACT 30OCT18 07:35 RIC R/R BULB IN AFT CABIN EMERGENCY FLASHLIGHT AS REQ OPS CHECK GOD OK FOR SERVICE.
- [SDR HNAA2018101900262](https://openairdocs.org/sdr/HNAA2018101900262.md): Fan · odor · Oct 17, 2018 · N638AE · Emb EMB145LR · Air Distribution Fan
  > PDIS 638 21-24 1595132 17OCT18 PHL CLOSE ELECTRICAL SMELL OBSERVED AFTER APU ATTEMPTED START. OUTSIDE OF AIRCRAFT NEAR GPU PLUG-IN. 76840 00 VAG HISTORY: FACT 17OCT18 22:20 PHL INSP AND FOUND EXHAUST FAN SMELLING BURNT R&R EXHAUST FAN. OPS CHECK FAILED. SEE SE
- [SDR HNAA2018092600231](https://openairdocs.org/sdr/HNAA2018092600231.md): Unknown · fumes · Sep 21, 2018 · N638AE · Emb EMB145LR · Air Distribution System
  > PDIS 638 21-01 1682341 21SEP18 PHL CLOSE WHILE STARTING EITHER #1 OR #2 ENG OFF APU, FUMES ARE PRESENT THROUGHOUT A/C. APU TEMP SPIKES TO MID 600 DEGREES 21585 00 EK HISTORY:. FACT
- [SDR HNAA2018052500114](https://openairdocs.org/sdr/HNAA2018052500114.md): Unknown · odor · May 12, 2018 · N638AE · Emb EMB145LR · Air Distribution System
  > DURING CRUISE, CREW BEGAN TO SMELL AN UNUSUAL ODOR ACCOMPANIED BY RADIO STATIC. ODOR AND STATIC DISAPPEARED AFTER LEAVING PRECIP. FA DID NOT NOTE THE ODOR IN THE CABIN. PERFORMED ENGINE RUN, CAN NOT DUPLICATE ODOR IN THE FLIGHT DECK. AIRCRAFT OKAY FOR SERVIC
- [SDR HNAA2018052500100](https://openairdocs.org/sdr/HNAA2018052500100.md): Indicator · false indication · May 2, 2018 · N638AE · Emb EMB145LR · Fuel Quantity Indicator
  > DURING TAXI OUT, THE NR 1 FUEL TANK LEVEL FLUCTUATED FROM 42 - 4600 LBS. AFTER DEPARTURE THE NR 2 TANK CONTENTS AND TOTAL FOB INDICATIONS ON MFD AND EICAS SHOWED DASHES AND FUEL 1 LOW LEVEL EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH PROCEDURES. R & R THE R
- [SDR HNAA2018032100062](https://openairdocs.org/sdr/HNAA2018032100062.md): Inlet · iced · Mar 20, 2018 · N638AE · Emb EMB145LR · Turbine Engine Air Inlet Section
  > NR 2 ENGINE REPORTED FOD IN INLET. REMOVED ICE FROM THE NR 2 ENGINE INLET
- [SDR HNAA2018021900036](https://openairdocs.org/sdr/HNAA2018021900036.md): Cabin Pressure · malfunctioned · Feb 15, 2018 · N638AE · Emb EMB145LR · Cabin Pressure Control System
  > CABIN ALTITUDE REACHED 13,500 FT AT FL190. AUTO PRESSURE MODE HAD NO EFFECT. MANUAL MODE BEGAN TO WORK AT 10,000 FT, MAINTAINING CABIN ALTITUDE OF 5,500 FT. CABIN ALTITUDE JUMPED UNCONTROLLABLY UP IN 200 FOOT INCREMENTS. CABIN DIFFERENTIAL PRESSURE. REMAINED
- [SDR HNAA2018021900035](https://openairdocs.org/sdr/HNAA2018021900035.md): Oxygen Mask · malfunctioned · Feb 14, 2018 · N638AE · Emb EMB145LR · Passenger Oxygen System
  > SEAT 6A OXYGEN MASK DID NOT DEPLOY. PERFORMED AN OPS CHECK OF THE PAX OXYGEN MASK IAW AMM 35-20-00, NO DEFECTS NOTED. OKAY FOR SERVICE.
- [SDR HNAA2018021900034](https://openairdocs.org/sdr/HNAA2018021900034.md): Controller · failed · Feb 14, 2018 · N638AE · Emb EMB145LR · Cabin Pressure Controller
  > SLOW LOSS OF PRESSURIZATION AT 34,000 FT. PRESSURIZATION STABILIZED AROUND 15,500 FT. SMALL POP IN CABIN AT THE TIME CABIN ALTITUDE WENT AMBER. R & R THE CABIN PRESSURE CONTROLLER AND PERFORMED AN OPS CHECK IAW AMM 21-31-01, 21-31-00-700-801-A, AND 21-31-00-
- [SDR HNAA2018021400030](https://openairdocs.org/sdr/HNAA2018021400030.md): Indicator · malfunctioned · Feb 11, 2018 · N638AE · Emb EMB145LR · Fuel Quantity Indicator
  > FUEL 1 LOW LEVEL MESSAGE AND NR 2 TANK INDICATED ZERO. RANDOM INDICATIONS. ALSO LOST TOTAL FUEL USED. CMC SHOWS FUEL 1 LO LEVEL MESSAGE. PERFORMED A CHECK ON THE REFUELING PANEL, NO FAULTS FOUND. CLEANED CONNECTORS ON FCU AND PERFORMED AN ELECTRICAL FUEL
- [SDR SIMA20180124001](https://openairdocs.org/sdr/SIMA20180124001.md): Frame · chafed · Jan 24, 2018 · N638AE · Emb EMB145LR · Fuselage Main, Frame
  > RIGHT FRAME 65 IN CARGO BAY HAS A CHAFE NEAR STINGER 12R. REPAIRED IAW ERS-EM-53MR-3082.
- [SDR SIMA20180121002](https://openairdocs.org/sdr/SIMA20180121002.md): Frame · cracked · Jan 21, 2018 · N638AE · Emb EMB145LR · Fuselage Main, Frame
  > FRAME 66 IS CRACKED BETWEEN STRINGERS 17 TO 18L. REPAIRED THE FRAME IAW SRM 53-00-04, AND SRM 51-40-02.
- [SDR SIMA20180121001](https://openairdocs.org/sdr/SIMA20180121001.md): Skin · punctured · Jan 21, 2018 · N638AE · Emb EMB145LR · Rudder, Plate/Skin
  > RIGHT SIDE OF RUDDER HAS A HOLE IN THE SKIN NEAR THE LOWER AFT CORNER. REPAIRED THE RUDDER LOWER SKIN IAW ERS EM-55MR-632.
- [SDR SIMA20180118005](https://openairdocs.org/sdr/SIMA20180118005.md): Fitting · gouged · Jan 18, 2018 · N638AE · Emb EMB145LR · Ailerons
  > RIGHT AILERON PCA FITTING IS GOUGED. REMOVED AND REPLACED THE RT AILERON PCA FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180116004](https://openairdocs.org/sdr/SIMA20180116004.md): Floor Support · corroded · Jan 16, 2018 · N638AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. REPAIRED THE LEFT OMEGA BEAM IAW EO EM-53MR-1518.
- [SDR SIMA20180115007](https://openairdocs.org/sdr/SIMA20180115007.md): Floor Support · corroded · Jan 15, 2018 · N638AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 58 - 59. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518.
- [SDR SIMA20180112003](https://openairdocs.org/sdr/SIMA20180112003.md): Torque Box · cracked · Jan 12, 2018 · N638AE · Emb EMB145LR · Passenger/Crew Doors
  > PAX DOOR INNER HANDLE TORQUE BOX HAS A.750 INCH CRACK. REPAIRED THE SUPPORT IAW EO EM-52MR-250.
- [SDR SIMA20180111009](https://openairdocs.org/sdr/SIMA20180111009.md): Door Sill · corroded · Jan 11, 2018 · N638AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL HAS AN AREA OF CORROSION. INSTALLED A NEW DOOR SILL IAW 51-40-02.
- [SDR SIMA20180111008](https://openairdocs.org/sdr/SIMA20180111008.md): Shear Tie · cracked · Jan 11, 2018 · N638AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR TIE AT FRAME 80, STRINGER 7L IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20180111012](https://openairdocs.org/sdr/SIMA20180111012.md): Shear Tie · cracked · Jan 11, 2018 · N638AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR TIE AT FRAME 80, STRINGER 7R IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20180111006](https://openairdocs.org/sdr/SIMA20180111006.md): Angle · cracked · Jan 11, 2018 · N638AE · Emb EMB145LR · Aerodynamic Fairings
  > LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.
- [SDR SIMA20180111010](https://openairdocs.org/sdr/SIMA20180111010.md): Angle · cracked · Jan 11, 2018 · N638AE · Emb EMB145LR · Aerodynamic Fairings
  > LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PANEL ANGLE IAW SRM 51-20-02 AND ETN-EM-53-142.
- [SDR SIMA20171019002](https://openairdocs.org/sdr/SIMA20171019002.md): Inverter · inoperative · Oct 19, 2017 · N638AE · Emb EMB145LR · Emergency Lighting
  > ROW 3 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11 AND WM 33-50-50. EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME
- [SDR SIMA20170926001](https://openairdocs.org/sdr/SIMA20170926001.md): Light · inoperative · Sep 26, 2017 · N638AE · Emb EMB145LR · Emergency Lighting
  > LT WING AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP AT LT WING AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR SIMA20170808002](https://openairdocs.org/sdr/SIMA20170808002.md): Light · inoperative · Aug 8, 2017 · N638AE · Emb EMB145LR · Emergency Lighting
  > ROW 12 CEILING EMERGENCY LT INOP. REMOVED AND REPLACED ROW 12 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPC GOOD END.
- [SDR SIMA20170502001](https://openairdocs.org/sdr/SIMA20170502001.md): Connector · unsecure · May 2, 2017 · N638AE · Emb EMB145LR · Emergency Lighting
  > AFT EMERGENCY FLOOR LIGHTING INOPERATIVE. SECURED INVERTER CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-11.
- [SDR SIMA20170302001](https://openairdocs.org/sdr/SIMA20170302001.md): Wire · broken · Mar 2, 2017 · N638AE · Emb EMB145LR · Light System Wiring
  > MAIN DOOR EXTERIOR EMERENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT SPLICE REMOVED AND REPLACED WIRE TERMINAL AND RECEPTICLE IAW SWPM 20-21-00. OPS CHECKED GOOD.
- [SDR SIMA20170222001](https://openairdocs.org/sdr/SIMA20170222001.md): Connector · unsecure · Feb 22, 2017 · N638AE · Emb EMB145LR · Light System Wiring
  > OVERHEAD EMERGENCY LIGHT INOP IN ROW 12 (EXIT SIGN). RESECURED EMERGENCY LIGHT CONNECTOR AND OPS CHECK GOOD IAW EMERGENCY LIGHT TEST AMM 33-50-00.
- [SDR SIMA20170212003](https://openairdocs.org/sdr/SIMA20170212003.md): Flashlight · inoperative · Feb 12, 2017 · N638AE · Emb EMB145LR · Emergency Equipment
  > FA FWD FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE FLASHLIGHT, OPS OK IAW AMM 33-51-01.

Next page: https://openairdocs.org/aircraft/N638AE/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 = 'N638AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N638AE/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.