# Service difficulty reports: N838AE

A list on [N838AE](https://openairdocs.org/aircraft/N838AE.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 2 · 87 reports

- [SDR SIMA202001232002](https://openairdocs.org/sdr/SIMA202001232002.md): Boot · disconnected · Jan 22, 2020 · N838AE · Emb EMB135KL · Airfoil Anti/De-ice System
  > WG A/ICE FAIL IN FLIGHT IN ICING CONDITIONS. QRH PROC. COMPLIED WITH, MSG REMAINS-C/A-FOUND WING 2 A/ICE LEAK ON CMC PERFORMED EMB 140 FIM TASK 30-11-00-810-807-A BLOCK DIAGRAM 001 UP TO SUBTASK 2, 817-001-A, FOUND AFT COUPLING BOOT OFF OF DUAL TEMP CNTRL VLV
- [SDR SIMA2020010229002](https://openairdocs.org/sdr/SIMA2020010229002.md): Flashlight · unsecure · Dec 29, 2019 · N838AE · Emb EMB135KL · Emergency Lighting
  > MEL 25-53 AUTH# 121051-C AFT FA FLASHLIGHT INOPREF LOG PAGE 4550081 ITEM 1.-C/A-RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OPC GOOD. MEL 25-53 RESTORED.
- [SDR SIMA2020010228001](https://openairdocs.org/sdr/SIMA2020010228001.md): Flashlight · inoperative · Dec 28, 2019 · N838AE · Emb EMB135KL · Emergency Equipment
  > AFT FA FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHTAUTH 121051-CREF 25-53 MOC 696266. RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OPC GOOD. MEL 25-53 RESTORED.
- [SDR SIMA201911298003](https://openairdocs.org/sdr/SIMA201911298003.md): Thermostat · failed · Nov 28, 2019 · N838AE · Emb EMB135KL · Pneumatic Indicating System
  > BLEED 1-2 VLV OVR TEMP IN FLIGHT WHILE IN ICING CONDITIONS DECLARED EMERGENCY AND AIR RETURN "TRANSFERRED TO NRWC 838-SGF-03378"-C/A-RAR LH AND RH FAN AIR CONTROL THERMOSTATS SEE NRWC 838-SGF-03378 FOR CORRECTIVE ACTION
- [SDR SIMA201911132001](https://openairdocs.org/sdr/SIMA201911132001.md): Handset · odor · Nov 12, 2019 · N838AE · Emb EMB135KL · Interphone/Passenger Announcement (PA) System
  > UPON LANDING FA REPORTED A BURNING SMELL IN GALLEY AREA-C/A-PERFORMED FIM TASK 21-20-00-810-801-A- FOUND FWD FA HAND MIC TO HAVE AN ELECTRICAL BURNT SMELL.CHECKED GENERAL CONDITION OF PLUG NO DEFECTS NOTED REMOVED AND REPLACED FWD FA HAND MIC IAW AMM 23-31-03
- [SDR SIMA201911121003](https://openairdocs.org/sdr/SIMA201911121003.md): Flashlight · unknown · Nov 11, 2019 · N838AE · Emb EMB135KL · Emergency Equipment
  > AFT FA FLASH LIGHT INOP-C/A-FLT CREW PLACARD AFT FA FLASH LIGHT IAW MEL 2553 AUTH # 110372-C MOC # 624980. OPS CHECKED AFT FA FLASHLIGHT. OPS CHECKED GOOD. IAW CMM 25-60-14 MEL RESTORED
- [SDR SIMA20190928005](https://openairdocs.org/sdr/SIMA20190928005.md): Wire · damaged · Sep 28, 2019 · N838AE · Emb EMB135KL · Light System Wiring
  > FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IS INOP-C/A-REPAIRED THE WIRING TO THE FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IAW EMB SWPM 20-20-00 OPS CHECK GOOD
- [SDR SIMA201908263001](https://openairdocs.org/sdr/SIMA201908263001.md): Cabin Pressure · malfunctioned · Aug 23, 2019 · N838AE · Emb EMB135KL · Cabin Pressure Control System
  > AIRCRAFT FAILED TO PRESSURIZE ABOVE 900 FT AT 13,000 FT. PERFORMED PRESSURIZATION CONTROL OPS TEST IN BOTH MANUAL & AUTOMATIC MODE IAW AMM 21-31-00. PERFORMED GROUND CONNECTION VALVE ADJUSTMENT TEST IAW AMM 21-22-04. OPS CHECK GOOD.NO OTHER DEFECTS NOTED.
- [SDR SIMA20190821001](https://openairdocs.org/sdr/SIMA20190821001.md): Skin · dented · Aug 21, 2019 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > DENT FOUND ON LOWER EDGE OF PASSENGER DOOR. PERFORMED PERMANENT REPAIR IAW ERS-EM-52MR-1016 PART A
- [SDR SIMA201908196004](https://openairdocs.org/sdr/SIMA201908196004.md): Structure · dented · Aug 16, 2019 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > PERFORM PERMANENT REPAIR OF PAX DOOR DENT IAW ERS-EM-52DF-1006 PTD. MAJOR REPAIR. REPAIRED PAX DOOR IAW ERS-EM-52DF-1006R2 PART D AND ERS-EM- 52MR-1016. SEE NRWC 838-ABI-03210 FOR DETAILS TDMI 838T5263 IS RESTORED
- [SDR SIMA201908164001](https://openairdocs.org/sdr/SIMA201908164001.md): Battery · overheated · Aug 14, 2019 · N838AE · Emb EMB135KL · Battery/Charger System
  > BATT 2 OVTEMP ON SHORT FINAL APPROACH TURNED PER EPC OFF BAT 2, THEN RECIEVED PROPER EICAS BATT 2 OFF BUS. PRIOR TO POWERING DOWN A GATE, SAW BATT 2 TEMP OF 104, IT WAS 80 AFTER TAXIED OFF RUNWAY. FIRE DEPT CALLED AND DISCONNECTED BOTH MAIN BATTERIES. REMOV
- [SDR SIMA20190519001](https://openairdocs.org/sdr/SIMA20190519001.md): Light · inoperative · May 19, 2019 · N838AE · Emb EMB135KL · Emergency Lighting
  > MOST AFT EMERGENCY LIGHT STRIP INOP. C/A-REMOVED AND REPLACED AFT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPC IS GOOD.
- [SDR SIMA201904098002](https://openairdocs.org/sdr/SIMA201904098002.md): A/C Pack · smoke · Apr 8, 2019 · N838AE · Emb EMB135KL · Cabin Cooling System
  > SMOKE IN CABIN REAR TO MIDDLE STRONG BURNING SMELL-C/A-FOLLOWED FIM TASK 21-20-00-810-801A FOUND RH ACM SEIZED RAR ACM #2 IAW AMM 21-51-03 PERFORMED GENERAL INSPECTION OF COOLING PACK SYS IAW AMM 21-51-00 OPS CHECK GOOD. NO SMELL NOTED
- [SDR SIMA20190227001](https://openairdocs.org/sdr/SIMA20190227001.md): Light · inoperative · Feb 27, 2019 · N838AE · Emb EMB135KL · Emergency Lighting
  > EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT 7A AND 8A INOP. C/A-DEFERRED EMERGENCY FLOOR PROXIMITY LIGHT AS PER MEL 33-30. REMOVED AND REPLACED EMERGENCY FLOOR PROX LIGHT IAW AMM 33-50-12. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MEL RESTORED
- [SDR SIMA20190123004](https://openairdocs.org/sdr/SIMA20190123004.md): Unknown · odor · Jan 23, 2019 · N838AE · Emb EMB135KL · Air Distribution System
  > OILY SMELL FROM PACKS WHEN TO THRUST IS APPLIED. GOES AWAY AFTER A FEW MIN "TRANSFERRED TO NRWC 838-DFW-02889". C/A- PERFORMED ETN-EM-72-034. RUNS CHECKED GOOD. NO ODORS DETECTED. PER FIM 72-00-00-810-814, REMOVED AND REPLACED LT ENGINE FUEL NOZZLES 3,4,5,6,13
- [SDR SIMA201811196002](https://openairdocs.org/sdr/SIMA201811196002.md): Controller · failed · Nov 16, 2018 · N838AE · Emb EMB135KL · Cabin Pressure Controller
  > AUTOMATIC PRESSURIZATION SYSTEM FAILED AS WE BEGAN OUR CLIMB.-C/A-RAR CABIN PRESS. CONTROL SYSTEM DIGITAL CONTROLLER IAW AMM 21-31-01. PERFORMED PRESS. CONTROL SYSTEM FUNCTIONAL TEST IN AUTO MODE IAW AMM 21-31-00. OPERATIONAL CHECK GOOD NO FURTHER DEFECTS NOTE
- [SDR SIMA201809042003](https://openairdocs.org/sdr/SIMA201809042003.md): Dau · failed · Sep 2, 2018 · N838AE · Emb EMB135KL · Central Computers
  > DAU NR 2 FAILED. PERFORMED FIM TASK 31-40-00-810-809-A. FOUND TO BE TRANSITORT CONDITION OF THE IC-60 COMPUTER. OPS CHECK OF IC-600 GOOD REF AMM 31-42-00. AIRCRAFT OK FOR CONTINUED SERVICE. REMOVED AND REPLACED NR 2 DAU IAW AMM 31-41-01. OPS CHECK GOOD AIRCRAF
- [SDR SIMA20180322005](https://openairdocs.org/sdr/SIMA20180322005.md): Shear Tie · corroded · Mar 22, 2018 · N838AE · Emb EMB135KL · Fuselage Internal Mounting Structure
  > FWD SHEAR TIE AFT OF FRAME 65 CORRODED. THE SHEAR WAS REPAIRED IAW SRM 53-31-04 RE.
- [SDR SIMA2018091115006](https://openairdocs.org/sdr/SIMA2018091115006.md): Relief Valve · failed · Mar 15, 2018 · N838AE · Emb EMB135KL · Landing Gear Brake System
  > FNC OF THE EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VALVE FAILED TEST. EMERGENCY PARKING BRAKE SYSTEM THERMAL RELIEF VALVE REPLACED IAW AMM 32-44-06.
- [SDR SIMA2018090615005](https://openairdocs.org/sdr/SIMA2018090615005.md): Door Sill · corroded · Mar 15, 2018 · N838AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > LT SILL NUMBER 5 CORRODED AT SEVERAL PLACES. LT SILL NUMBER 5 BLENDED IAW SRM 51-10-03 AND FOUND OUT OF LIMIT IAW SRM 5323-10 LT SILL NUMBER 5 REMOVED FOR REPLACEMENT IAW SRM 51-40-02. LT SILL NUMBER 5 INSTALLED IAW SRM 51-40-02.
- [SDR SIMA2018090615003](https://openairdocs.org/sdr/SIMA2018090615003.md): Door Sill · corroded · Mar 15, 2018 · N838AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CF2 FLOOR STRUCTURE LT SILL NR 3 BTW FR31 & FR35 CORRODED. CF2 FLOOR STRUCTURE LT SILL NR 3 OUT OF LIMITS AND REMOVED PER SRM 53-22-10 AND 51-40-20 AND INSTALLED A NEW PART WITH SOLID RIVET.
- [SDR SIMA2018090615004](https://openairdocs.org/sdr/SIMA2018090615004.md): Frame · corroded · Mar 15, 2018 · N838AE · Emb EMB135KL · Fuselage Main, Frame
  > IN RFI AT FR 65, FRAME Z PN 145-25672-203 FOUND CORRODED AROUND ANCHOR NUT HOLES. IN RFI AT Z FR65 ON LT SIDE CORROSION BLENDED IAW SRM 51-10-03. AFTER FURTHER INVESTIGATION, Z FR 65 WAS FOUND TO BE OUT OF LIMITS AND REMOVED FOR REPLACEMENT IAW SRM 51-40-02.
- [SDR SIMA2018090615002](https://openairdocs.org/sdr/SIMA2018090615002.md): Gusset · corroded · Mar 15, 2018 · N838AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED. CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED OUT OF LIMITS, REPLACED IAW SRM 51-40-02.
- [SDR SIMA20161101001](https://openairdocs.org/sdr/SIMA20161101001.md): Charger · failed · Nov 1, 2016 · N838AE · Emb EMB135KL · Emergency Lighting
  > WHILE PERFORMING PS-1 INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY HOLDER ASSY AND CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD.
- [SDR SIMA20160602004](https://openairdocs.org/sdr/SIMA20160602004.md): B-Nut · leaking · Jun 2, 2016 · N838AE · Emb EMB135KL · APU Engine Fuel and Control
  > WITH APU BLEED OPEN, GET A SRONG ODOR OF FUEL, POST FLIGHT INSPECTION REVEALS FUEL LEAKING FROM UNDER APU AREA. FOUND LOOSE B-NUT ON APU FUEL CONTROL INLET, ADJUSTED & OPS CHECK IAW AMM 49-31-01, FOUND SYS WORKING PROPERLY. OPERATIONS CHECKED, OPERATIONS CHE
- [SDR SIMA20160514003](https://openairdocs.org/sdr/SIMA20160514003.md): Smoke Warning · false activation · May 14, 2016 · N838AE · Emb EMB135KL · Smoke Detection
  > IN CRUISE FLIGHT AT 320 THE BAGGAGE SMOKE WARNING MSG APPEARED MOMENTARILY & THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED & STAYED ON REST OF FLIGHT. PERFORMED SEVERAL TEST OF BAGGAGE SMOKE DETECTION SYS IAW AMM 26-15-00. OPERATIONS CHECKED GOOD. PERFORMED A
- [SDR SIMA20160226003](https://openairdocs.org/sdr/SIMA20160226003.md): Inverter · inoperative · Feb 26, 2016 · N838AE · Emb EMB135KL · Emergency Lighting
  > SECOND & THIRD EMER FLOOR STRIP LIGHTING INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER IAW 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150923002](https://openairdocs.org/sdr/SIMA20150923002.md): Switch · dirty · Sep 23, 2015 · N838AE · Emb EMB135KL · Door Warning System
  > ANTI-ICE LGA ACCT MX & BAGGAGE DOOR, OPEN INDICATION RIGHT AFTER TAKEOFF FLIGHT CONTINUED. CLEAN BOTH MICRO SWITCHES IAW 52-76-01. OPERATIONS CHECKED GOOD, NO FAULT INDICATION.
- [SDR SIMA20150908003](https://openairdocs.org/sdr/SIMA20150908003.md): Engine · smoke · Sep 8, 2015 · N838AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > SMOKE COMING OUT OF ENG 2, AFTER SHUTDOWN WITH A STRONG SMELL OF BURNED OIL. COMPLIED WITH ETN-EM-79-015 STEPS 1 - 9. RETURNED ENG TO SERVICE. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SIMA20150122003](https://openairdocs.org/sdr/SIMA20150122003.md): Brake · failed · Jan 22, 2015 · N838AE · Emb EMB135KL · Trailing Edge Flap Control System
  > FLAP LOW SPEED EICAS MESSAGE ON APPROACH. M PROCEDURES COMPLIED WITH, NO CMC MESSAGE. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECKED GOOD. PERFORMED WIRE CHECK IAW FIM 27-51-00-810-814-A. ALL FOUND OK.
- [SDR SIMA20150116002](https://openairdocs.org/sdr/SIMA20150116002.md): Flap · malfunctioned · Jan 16, 2015 · N838AE · Emb EMB135KL · Trailing Edge Flap Control System
  > FLAP FAIL ON FINAL AT 2000 FT ALL SET FOR 22 FAILED AT 11 ON GLIDE SLOPE SLOWING THROUGH 120 KT 450 FPM DESCENT. RESET & PERFORMED OPERATIONS CHECK OF FLAP SYS IAW AMM 27-51-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR SIMA20141119006](https://openairdocs.org/sdr/SIMA20141119006.md): Flashlight · inoperative · Nov 19, 2014 · N838AE · Emb EMB135KL · Emergency Equipment
  > CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140902005](https://openairdocs.org/sdr/SIMA20140902005.md): Holder · broken · Sep 2, 2014 · N838AE · Emb EMB135KL · Emergency Equipment
  > FLIGHT ATTENDANT EMER FLASHLIGHT HOLDER BASE IS BROKEN. R & R FLIGHT ATTENDANT EMER FLASHLIGHT BRACKET IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20140722001](https://openairdocs.org/sdr/SIMA20140722001.md): Switch · inoperative · Jul 22, 2014 · N838AE · Emb EMB135KL · Aileron Control System
  > AILERON SYS 1 INOPERATIVE IN FLIGHT. R & R AIL SYS NR 1 PUSH BUTTON IAW AMM 20-13-08. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140701010](https://openairdocs.org/sdr/SIMA20140701010.md): Proximity Switch · out of adjust · Jul 1, 2014 · N838AE · Emb EMB135KL · Landing Gear Position and Warning
  > DOWN LOCK RELEASE BUTTON PRESSED FOR GEAR RETRACTION ON TAKEOFF. LG AIR & GND FAIL MSG AFTER GEAR SELECTED DOWN. FOUND PROXIMITY SWITCHES ON RT & LT MLGS OUT OF RANGE. ADJUSTED PROX SWITCHES IAW AMM 32-63-05 & PERFORMED EXT & RETRACTION OF GEARS IAW AMM 32-
- [SDR SIMA20140629010](https://openairdocs.org/sdr/SIMA20140629010.md): Skin · cracked · Jun 29, 2014 · N838AE · Emb EMB135KL · Fuselage Main, Plate/Skin
  > RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1R & 2R IAW ERS-EM-53MR-551.
- [SDR SIMA20140629011](https://openairdocs.org/sdr/SIMA20140629011.md): Skin · cracked · Jun 29, 2014 · N838AE · Emb EMB135KL · Fuselage Main, Plate/Skin
  > LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 2L IAW ERS-EM-53MR-550.
- [SDR SIMA20140628003](https://openairdocs.org/sdr/SIMA20140628003.md): Wire · broken · Jun 28, 2014 · N838AE · Emb EMB135KL · Light System Wiring
  > NUMBER 2 EMER PROXIMITY LIGHT STRIP HAS BROKEN & DAMAGED WIRES. R & R FWD GALLEY EMER LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20140620003](https://openairdocs.org/sdr/SIMA20140620003.md): Fitting · worn · Jun 20, 2014 · N838AE · Emb EMB135KL · Ailerons
  > RIGHT AILERON DAMPER FITTING WORN. REMOVED & INSTALL DAMPER FITTING IAW EO EM-27MR-112.
- [SDR SIMA20140606008](https://openairdocs.org/sdr/SIMA20140606008.md): Wire · broken · Jun 6, 2014 · N838AE · Emb EMB135KL · Light System Wiring
  > TWO EMER LIGHT STRIP WIRES ARE BROKEN AT FLOOR PANEL 261BF. INSTALLED SERVICEABLE PINS ON TWO EMER LIGHT STRIP WIRES, AT FLOOR PANEL 261BF IAW WM 91-10-02, SWPM 20-00-03 & SWPM 20-21-00. SEE BOW 157401 FOR OPERATIONS CHECK.
- [SDR SIMA20140606007](https://openairdocs.org/sdr/SIMA20140606007.md): Structure · cracked · Jun 6, 2014 · N838AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > BATTERY COMPARTMENT DOOR CUT OUT CRACKED, AFT EDGE MARKED. REPAIRED CRACK ON BATTERY COMPARTMENT DOOR CUT OUT AFT EDGE IAW ERS-EM-5300-527. SEE WIP & TASK ENTRIES FOR DETAILS.
- [SDR SIMA20140606006](https://openairdocs.org/sdr/SIMA20140606006.md): Door · dented · Jun 6, 2014 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER. MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5200-159. SEE TURNOVER FOR DETAILS.
- [SDR SIMA20140606005](https://openairdocs.org/sdr/SIMA20140606005.md): Door · gouged · Jun 6, 2014 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > MAIN DOOR GOUGED ALONG LOWER EDGE, METAL MOVED, NOT PAINT DAMAGE ONLY. MAIN DOOR GOUGED ALONG LOWER EDGE FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5200-159. SEE TASK & WIPS FOR DETAILS.
- [SDR SIMA20140606004](https://openairdocs.org/sdr/SIMA20140606004.md): Splice · corroded · Jun 6, 2014 · N838AE · Emb EMB135KL · Fuselage Miscellaneous Structure
  > CIRCUMFERENTIAL SPLICE IS CORRODED BETWEEN FRAME 12 & 13, STRINGER 21L & 21R. COMPLIED WITH ERS-EM-5300-528 JUNCTION 02 CIRCUMFERENTIAL SPLICE CORROSION BETWEEN FRAME 12 & 13 & BETWEEN STRINGER 21L - 21R. PERMANENT REPAIR SEE TASK & WIPS FOR DETAILS.
- [SDR SIMA20140424002](https://openairdocs.org/sdr/SIMA20140424002.md): Roller · lack of lube · Apr 24, 2014 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN PAX DOOR ROLLERS IAW MM 52-18-00, OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20140312002](https://openairdocs.org/sdr/SIMA20140312002.md): Isis · failed · Mar 12, 2014 · N838AE · Emb EMB135KL · Integrated Flight System
  > STANDBY ATT FAIL DURING ROTATION, DIVERT BACK TO LGA. R & R ISIS IAW AMM 34-01-01. OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 34-01-01.
- [SDR SIMA20140119007](https://openairdocs.org/sdr/SIMA20140119007.md): Door · lack of lube · Jan 19, 2014 · N838AE · Emb EMB135KL · Passenger/Crew Doors
  > MAIN CABIN ENTRY DOOR EXCESSIVE FORCE USED TO OPEN OR CLOSE DOOR USING INSIDE HANDLE. CLEANED & LUBED MAIN CABIN DOOR IAW MX STANDARD PRACTICES, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131222014](https://openairdocs.org/sdr/SIMA20131222014.md): Battery · discharged · Dec 22, 2013 · N838AE · Emb EMB135KL · Emergency Lighting
  > OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-17.
- [SDR SIMA20131214003](https://openairdocs.org/sdr/SIMA20131214003.md): Power Supply · inoperative · Dec 14, 2013 · N838AE · Emb EMB135KL · Emergency Lighting
  > RIGHT & LT AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04, OPERATIONS CHECKED GOOD.
- [SDR SIMA20131019003](https://openairdocs.org/sdr/SIMA20131019003.md): Flashlight · inoperative · Oct 19, 2013 · N838AE · Emb EMB135KL · Emergency Equipment
  > AFT FLASHLIGHT IN CABIN NOT CHARGING. R & R AFT FLASHLIGHT, OPS GOOD AMM 33-50-16.

Next page: https://openairdocs.org/aircraft/N838AE/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 = 'N838AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N838AE/reports

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