# Service difficulty reports: N13970, cancelled Jul 31, 2021

A list on [N13970, cancelled Jul 31, 2021](https://openairdocs.org/deregistered/N13970-2021-07-31.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 · 94 reports

- [SDR ASOA20140625153](https://openairdocs.org/sdr/ASOA20140625153.md): Skin · corroded · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, CORROSION WAS FOUND ON SKIN AROUND SCREW HOLES AND CORRODED NUTPLATES AT THE ADF ANTENNA LOCATION. MAINTENANCE REMOVED CORROSION ON SKIN AT THE ADF ANTENNA LOCATION,.002" MATERIAL LOSS, WITHIN LIMITS OF SRM 53-23-01, PERFORMED HFEC INSPECTION
- [SDR ASOA20140625152](https://openairdocs.org/sdr/ASOA20140625152.md): Strip · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT WING/FUSELAGE FILLET HAS CRACKS AT RIVET FRAME 48, 10MM AFT AND 6MM FWD, REQUIRES FINAL REPAIR IAW EC5320-01707. MAINTENANCE REPAIRED RT WING/FUSELAGE FILLET AT FRAME 48 IAW EC5320-01707 AND SRM 53-23-12. THE ACFT WAS APPROVED FOR RETURN
- [SDR ASOA20140625151](https://openairdocs.org/sdr/ASOA20140625151.md): Bulkhead · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Bulkhead
  > DURING C-CHECK, RT AFT WHEEL WELL WEB CRACKED OTBD SIDE. MAINTENANCE STOP DRILLED UPPER CRACK, CUT-OUT LOWER DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-23-12. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625150V](https://openairdocs.org/sdr/ASOA20140625150V.md): Shear Tie · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE AT FRAME 24 STRINGER 15R IS CRACKED. R & R SHEAR TIE IAW SRM 51-20-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625149V](https://openairdocs.org/sdr/ASOA20140625149V.md): Shear Tie · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE AT FRAME 24 STRINGER 16R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625148V](https://openairdocs.org/sdr/ASOA20140625148V.md): Shear Tie · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE FRAME 27, STRINGER 15R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625147V](https://openairdocs.org/sdr/ASOA20140625147V.md): Shear Tie · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK SHEAR TIE FRAME 26, STRINGER 15R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625146](https://openairdocs.org/sdr/ASOA20140625146.md): Shear Tie · cracked · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR TIE AT FRAME 80 IS CRACKED BETWEEN STRINGER 3-5R JUST FWD OF APU FIREWALL. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625145](https://openairdocs.org/sdr/ASOA20140625145.md): Plate · corroded · Jun 25, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, MULTIPLE AREAS OF CORROSION FOUND AROUND LOWER CARGO DOOR STRIKER PLATE AT FRAME 65. MAINTENANCE BLENDED CORROSION, MATERIAL LOSS IS.032" OUT OF LIMITS, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-31-04. THE ACFT WA
- [SDR ASOA20140613127](https://openairdocs.org/sdr/ASOA20140613127.md): Frame · corroded · Jun 12, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK THE CHANNEL ON FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608124](https://openairdocs.org/sdr/ASOA20140608124.md): Door Frame · corroded · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, CORROSION FOUND AROUND AFT TWO NUTPLATES ON INSIDE OF MAIN DOOR BOTTOM FRAME. REMOVED CORRODED LOWER AFT DOOR FRAME. LOCATED, DRILLED AND INSTALLED NEW FRAME IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608123](https://openairdocs.org/sdr/ASOA20140608123.md): Shear Tie · corroded · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, CORROSION FOUND ON SHEAR TIE AT FRAME 65. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-31-04. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-31-04. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608122](https://openairdocs.org/sdr/ASOA20140608122.md): Floor Support · cracked · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK LT OMEGA BEAM LOWER FLANGE IS CRACKED AT FRAMES 47-48. R & R FLOOR SUPPORT IAW SRM 51-20-03, AND 53-23-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608121](https://openairdocs.org/sdr/ASOA20140608121.md): Floor Support · corroded · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FLOOR SUPPORT FWD OF SERVICE DOOR FRAME CORRODED AROUND NUTPLATES. R & R FLOOR SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608120](https://openairdocs.org/sdr/ASOA20140608120.md): Floor Support · corroded · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION FOUND ON FLOOR SUPPOT AT Y=0.0 FRAME 61. R & R FLOOR SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608119](https://openairdocs.org/sdr/ASOA20140608119.md): Crossbeam · corroded · Jun 8, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, CROSSBEAM AT FRAME 61 CORRODED BETWEEN RT OMEGA BEAM AND RT OTBD FLOOR SUPPORT 100 PERCENT MATERIAL LOSS. R & R CROSSBEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608118](https://openairdocs.org/sdr/ASOA20140608118.md): Gusset · corroded · Jun 8, 2014 · N13970 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION FOUND AROUND POTABLE WATER LINES UNDER JAMB NUTS ON RT OMEGA BEAM GUSSETT FRAME 61. R & R GUSSET IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604102V](https://openairdocs.org/sdr/ASOA20140604102V.md): Floor Support · cracked · Jun 4, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM INBD LOWER FLANGE WAS FOUND TO BE CRACKED BETWEEN FRAMES 47-48. MAINTENANCE R & R THE BEAM FLANG IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604101](https://openairdocs.org/sdr/ASOA20140604101.md): Floor Support · cracked · Jun 4, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM OUTBOARD LOWER FLANGE WAS FOUND TO BE CRACKED BETWEEN FRAMES 47-48. MAINTENANCE REMOVED AND REPLACED THE BEAM FLANGE IAW EMB 145 SRM 51-40-02 AND 53-23-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604100](https://openairdocs.org/sdr/ASOA20140604100.md): Stiffener · corroded · Jun 4, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FRAME 65 STIFFENER BETWEEN STRINGERS 15-16L WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE STIFFENER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604099](https://openairdocs.org/sdr/ASOA20140604099.md): Door Sill · corroded · Jun 4, 2014 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140122012](https://openairdocs.org/sdr/ASOA20140122012.md): Skin · cracked · Jan 22, 2014 · N13970 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FOUND CRACK IN SKIN BETWEEN THE PILOTS WINDSHIELD AND THE DV WINDOW CUTOUTS IN THE SUPPORT FRAME. MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW EC 5310-01758. ALL WORK ACCOMPLISHED AND ACFT PRESSURIZED. ACFT RETURNED TO SERVICE.
- [SDR ASOA20131003393](https://openairdocs.org/sdr/ASOA20131003393.md): A/C Pack · odor · Oct 3, 2013 · N13970 · Emb EMB145LR · Cabin Cooling System
  > CREW NOTICED SMOKE IN THE COCKPIT AND RETURN TO DEPARTURE. MX TROUBLESHOTING FOR SMOKE IN COCKPIT IAW FIM 21-20-00-816-801-A. SMOKE AND HAZE APPEARS WHEN THE NR 1 PACK WAS SELECTED ON. NR 1 PACK WAS NOTED ON THE EICIAS OUT OF EWR AND MESSAGE CLEARED RESET
- [SDR ASOA20120722048](https://openairdocs.org/sdr/ASOA20120722048.md): Stringer · corroded · Jul 22, 2012 · N13970 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK. STRINGER 21R CORRODED BETWEEN FR 10-11. R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA234](https://openairdocs.org/sdr/C2XA11IA234.md): Display · shorted · Oct 9, 2011 · N13970 · Emb EMB145LR · Central Display
  > IAH - FLIGHT 4229 WAS DELAYED DUE TO CREW REPORT OF CAPTAINS MFD BLANKING OUT FOLLOWED BY STRONG ELECTRICAL SMELL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA198](https://openairdocs.org/sdr/C2XA11IA198.md): Flapper Valve · leaking · Sep 5, 2011 · N13970 · Emb EMB145LR · Fuel Storage
  > IAH - FLIGHT 2816, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLAPPER VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH112](https://openairdocs.org/sdr/C2XA11SH112.md): Ahrs · malfunctioned · Aug 2, 2011 · N13970 · Emb EMB145LR · Integrated Flight System
  > FLIGHT 2391 A/C N13970 AIR RETURN FROM EWR-"ON THE CLIMBOUT LOST TWICE ATT AND HDG ON CPT SIDE. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER 800 SERIES AND OPERATIONAL CHECK GOOD IAW 34-21-01 AND OPS CHECK GOOD IAW 34-21-00. RETURN TO CAT II. THE AIR
- [SDR C2XA11IA172](https://openairdocs.org/sdr/C2XA11IA172.md): Computer · inoperative · Jul 31, 2011 · N13970 · Emb EMB145LR · Attitude and Direction Data System
  > FLT 2391, CREW REPORTED TAHT THE CAPTAIN LOST ATT AND HDG TWICE DURING CLIMB. THE AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVE
- [SDR C2XA11RI120](https://openairdocs.org/sdr/C2XA11RI120.md): Proximity Switch · defective · Jul 3, 2011 · N13970 · Emb EMB145LR · Drag Control System
  > FLIGHT 2666 - EWR - FLIGHT CREW REPORTED SPOILER FAIL INDICATION AND SPOILER OPEN INDICATION ON EICAS DURING CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR REMOVED AND REPLACED LF O/B SPOILER PROX SWITCH AND PERFORMED OPERATIONAL CHECK SUCC
- [SDR C2XA11TY077](https://openairdocs.org/sdr/C2XA11TY077.md): Contactor · defective · Jun 6, 2011 · N13970 · Emb EMB145LR · Battery/Charger System
  > TYS - A/C WAS EN ROUTE FROM CLE TO GSP WHEN CREW GOT A CAUTION LIGHT OF THE BACKUP BATTERY OFF BUS. A/C DIVERTED INTO TYS WHERE MAINTENANCE REMOVED AND REPLACED THE BACKUP BATTERY CONTACTOR IAW EMB 145AMM 24-36-02. OPS CHECK GOOD AND WAS RELEASED LOG PAGE 27
- [SDR C2XA11IA071](https://openairdocs.org/sdr/C2XA11IA071.md): Signal Cond Unit · inoperative · Apr 11, 2011 · N13970 · Emb EMB145LR · Fuel Indicating System
  > FLIGHT 2769, THE CREW REPORTED A FUEL 1 - 2 LOW LEVEL INDICATION ON EICAS. THE AIRCRAFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE LOW LEVEL WARNING ON MEL 28-44-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR C2XA11IA021](https://openairdocs.org/sdr/C2XA11IA021.md): Proximity Switch · inoperative · Jan 20, 2011 · N13970 · Emb EMB145LR · Drag Control System
  > IAH - FLIGHT 2689, DURING CRUISE THE CREW REPORTED "SPOILER OPEN" AND "SPOILER FAIL" MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SPOILER PROXIMITY SWITCH, OPERATIONALLY TESTED WI
- [SDR C2XA10TY114](https://openairdocs.org/sdr/C2XA10TY114.md): Skin · cracked · Aug 12, 2010 · N13970 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > LEFT AND RIGHT AFT FUSELAGE SKIN HAS CRACKS AT FASTENERS LOCATED AT FRAMES 77 THRU 79. REAMED HOLES TO REMOVE CRACKS INSTALLED BUSHING AND RIVETS IAW EC5330-02203.
- [SDR C2XA10TY112](https://openairdocs.org/sdr/C2XA10TY112.md): Frame · corroded · Aug 3, 2010 · N13970 · Emb EMB145LR · Fuselage Main, Frame
  > BOTTOM AFT CORNER OF SERVICE DOOR FRAME HAS CORROSION. REPAIRED FRAME 22 IAW EC5310-01373.
- [SDR C2XA10TY108](https://openairdocs.org/sdr/C2XA10TY108.md): Sill · corroded · Aug 2, 2010 · N13970 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA10TY053](https://openairdocs.org/sdr/C2XA10TY053.md): Inverter · inoperative · Apr 8, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > EMERGENCY EXITS LIGHTS AT WING INOP. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.
- [SDR C2XA10CL036](https://openairdocs.org/sdr/C2XA10CL036.md): Battery · discharged · Feb 26, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE CABIN AISLE PATH LIGHT STRIP AND EMERGENCY EXIT DOOR SIGNS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10IA072](https://openairdocs.org/sdr/C2XA10IA072.md): Inverter · inoperative · Feb 15, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA067](https://openairdocs.org/sdr/C2XA10IA067.md): Inverter · inoperative · Feb 15, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > LCH - DURING MAINTENANCE INSPECTION, THE NUMBER FIVE AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA066](https://openairdocs.org/sdr/C2XA10IA066.md): Inverter · inoperative · Feb 15, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > LCH - DURING MAINTENANCE INSPECTION THE NUMBER TWO AND THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA10RI023](https://openairdocs.org/sdr/C2XA10RI023.md): Light · inoperative · Jan 22, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT BULBS ABOVE SEATS AT ROW 12 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10RI022](https://openairdocs.org/sdr/C2XA10RI022.md): Bulb · burned out · Jan 22, 2010 · N13970 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT BULBS ABOVE SEATS AT ROW 12 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09CL023](https://openairdocs.org/sdr/C2XA09CL023.md): Proximity Switch · faulty · Mar 5, 2009 · N13970 · Emb EMB145LR · Drag Control System
  > CLE FLIGHT 2351 - THE CREW REPORTED A SPOILER FAIL MESSAGE IN FLIGHT. SPOILER OPEN MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT INBOARD SPOILER PROXIMITY SWITCH. OPERATIONAL CHE
- [SDR C2XA09CL002](https://openairdocs.org/sdr/C2XA09CL002.md): Battery · discharged · Jan 4, 2009 · N13970 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX THE EMERGENCY FLOOR LIGHT CTR STRIP WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR C2XA08CL121](https://openairdocs.org/sdr/C2XA08CL121.md): Hydraulic System · contaminated · Nov 17, 2008 · N13970 · Emb EMB145LR · Hydraulic System, Main
  > MKE - FLIGHT 2948 - THE CREW REPORTED THE NR 1 HYDRAULIC SYSTEM FLUID SHOWED 1/4 LEVEL AFTER 43 MINUTES IN FLIGHT. THE SYSTEM WAS SERVICED PRIOR TO DEPARTURE FROM IAH. RECEIVED A HYD SYS 1 LOW QUANTITY ON FINAL APPROACH. EMERGENCY WAS DECLARED AND THE AIRCR
- [SDR C2XA08RI167](https://openairdocs.org/sdr/C2XA08RI167.md): Landing Gear · malfunctioned · Nov 14, 2008 · N13970 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > FLIGHT 2361 - EWR - FLIGHT CREW REPORTED NLG WOULD NOT RETRACT NORMALLY, CREW HAD TO USE DOWNLOCK RELEASE TO RETRACT GEAR, THEN GEAR EXTENDED NORMALLY. EWR MX PERFORMED A FLIGHT TEST AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT PASSED OPERATIONAL CHECK SUCC
- [SDR C2XA08CL108](https://openairdocs.org/sdr/C2XA08CL108.md): Battery · inoperative · Sep 24, 2008 · N13970 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX THE RT WING FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR C2XA08CL109](https://openairdocs.org/sdr/C2XA08CL109.md): Light · inoperative · Sep 24, 2008 · N13970 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX THE LT WING AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECKS WERE GOOD.
- [SDR C2XA08RI081](https://openairdocs.org/sdr/C2XA08RI081.md): Unknown · odor · Jun 2, 2008 · N13970 · Emb EMB145LR · Air Distribution System
  > FLIGHT 2251 - IND - FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. SYSTEM RESET WAS PERFORMED AND NO DEFECTS WAS NOTED. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)
- [SDR C2XA08TY050](https://openairdocs.org/sdr/C2XA08TY050.md): Bracket · damaged · May 13, 2008 · N13970 · Emb EMB145LR · Ailerons
  > TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON I/B PCA ACTUATOR ROD ATTACHMENT FITTING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC 5750-01177. A/C WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.

Next page: https://openairdocs.org/deregistered/N13970-2021-07-31/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 = 'N13970' AND deregistration_id = 'N13970-2021-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13970-2021-07-31/reports

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