# Service difficulty reports: N629AE

A list on [N629AE](https://openairdocs.org/aircraft/N629AE.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 · 150 reports

- [SDR HNAA2023050100148](https://openairdocs.org/sdr/HNAA2023050100148.md): Unknown · unknown · Apr 30, 2023 · N629AE · Emb EMB145LR · Flight Compartment Windows
  > LOUD WHOOSHING NOISE ON TAKEOFF ROLL, A/C NOT ACCELERATING PROPERLY. FACT 30APR23 21:42 PHL MX FOUND FO'S DV WINDOW TRIM SEAL PARTIALLY UNSEATED. APPLY RTV 230 SEALANT TO AFFECTED AREA REF SRM 51-20-01. PERFORMED PRESSURIZATION CHECK. NO LEAK
- [SDR HNAA2023030600060](https://openairdocs.org/sdr/HNAA2023030600060.md): None · none · Mar 5, 2023 · N629AE · Emb EMB145LR · Cabin Cooling System
  > DURING FLIGHT PACK 1 VLV CLOSED APPEARED ON EICAS AND WOULDNT RESET. PACK 2 CURRENTLY ON MEL, A/C COULD NOT HOLD PRESSURIZATION FACT 05MAR23 20:27 CLT FOUND MULTIPLE SLEEVES BLOWN ON PACK 1 A/C SYSTEM. R&R SLEEVES AS REQUIRED TO DUAL TEMP CTRL VALVE, DUCT
- [SDR HNAA2023010400015](https://openairdocs.org/sdr/HNAA2023010400015.md): Bleed Valve · failed · Jan 2, 2023 · N629AE · Emb EMB145LR · Compressor Bleed Valve
  > REJECTED TAKEOFF AT 60 KNOTS. BLEED 2 VALVE FAIL WITH TAKEOFF POWER SELECTED. R & R #2 ENGINE BLEED VALVE IRT AMM 36-11-05. OPS CHECK / LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.A/C OK FOR SERVICE.
- [SDR HNAA2022100500266](https://openairdocs.org/sdr/HNAA2022100500266.md): Bleed Valve · faulted · Oct 4, 2022 · N629AE · Emb EMB145LR · Compressor Bleed Valve
  > BLEED 2 VALVE FAILURE ON T/O POWER ( C/W RMM 36-11-05) T/S FIM 36-11-00-810-806-A STEPS 1 2 3 20 21 AND 22 R/R #2 HIGH STAGE PRESSURE SWITCH IAW AMM 36-11-07. OPS CHECK GOOD. NO OTHER DEFECTS NOTEDAT THIS TIME. CLEAR MEL 36-1-3.OK FOR SERVICE.
- [SDR HNAA2022061400223](https://openairdocs.org/sdr/HNAA2022061400223.md): None · none · Jun 12, 2022 · N629AE · Emb EMB145LR · Pneumatic Indicating System
  > PDIS 629 36-21 2116541 12JUN22 RIC CLOSE BLEED 1 LEAK IN FLT 29363 00 RS FACT 13JUN22 06:07 RIC FOUND THERMAL SWITCH WIRE NOT SOLDERED IN AFT AVIONIS BAY BY THE CROSS BLEED VALVE. S
- [SDR HNAA2022022000082](https://openairdocs.org/sdr/HNAA2022022000082.md): None · none · Feb 17, 2022 · N629AE · Emb EMB145LR · Air Conditioning System
  > PDIS 629 21-01 2706202 17FEB22 CAK CLOSE ELETRICAL BURNING SMELL DURING DESCENT LASTED FOR 30 SEC. SMELL WAS NOTICED FWD CABIN/FLT DECK AREA. 27933 00 RS FACT 17FEB22 00:26 CAK PERF
- [SDR HNAA2022020900068](https://openairdocs.org/sdr/HNAA2022020900068.md): Not Reported · not reported · Feb 7, 2022 · N629AE · Emb EMB145LR · Pneumatic Indicating System
  > PDIS 629 36-11 2706101 07FEB22 ISP CLOSE HS 1 VLV FAIL MSG DURING TAKE OFF ROLL. REJECTED TAKE OFF AT 65 KTS FULL THROTTLE FACT 07FEB22 11:24 ISP PERFORMED OPS TEST OF AIR BLEED SYS WITH CREW IAW AMM 36-00-00-700-803. OPS CHE
- [SDR HNAA2012081700384](https://openairdocs.org/sdr/HNAA2012081700384.md): Valve · faulted · Aug 14, 2021 · N629AE · Emb EMB145LR · Cabin Cooling System
  > ON TAKE OFF PACK 2 VALVE CLOSED MSG WOULD NOT CLEAR UNTIL LANDING. DURING INSPECTION OF AIR CON/PNUMATIC PANEL FOUND AND REPAIRED BROKEN WIRE IAW SWPM 20-5000 (SHORT SIGN)CHANGED RELAYS K0320, K0263, K0262, K0184 IAW AMM 20-13-02. REMOVED AND REPLACED PACK 2
- [SDR HNAA2021071300320](https://openairdocs.org/sdr/HNAA2021071300320.md): Pipe · leaking · Jul 10, 2021 · N629AE · Emb EMB145LR · Compressor Bleed Valve
  > BLEED 1 LEAK MSG DURING CLIMB. T/S IN REF W/FIM TASK 36-20-00-810-801-A. FOUND Y-PIPE AFTER #100 ENG BLD VLV TO BE DAMAGED. R&R'D Y-PIPE AFTER #100 ENG BLD VLV IN REF W/AMM 36-11-09. OPS CHECKED IN REF W/AMM 36-00-00. OPS CK GOOD. RE-ACTIVATED #100 ENGINE BLD
- [SDR HNAA2021062400295](https://openairdocs.org/sdr/HNAA2021062400295.md): Uplock · faulted · Jun 22, 2021 · N629AE · Emb EMB145LR · Landing Gear Retraction/Extension System
  > AFTER GEAR RETRACTION, RIGHT MAIN INDICATION ALTERNATED BETWEEN UP AND LOCKED AND IN TRANSIT. R&R'D R/H MLG UP LOCK BOX IAW AMM 32-33-10-04. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR HNAA2021062400294](https://openairdocs.org/sdr/HNAA2021062400294.md): Uplock · malfunctioned · Jun 22, 2021 · N629AE · Emb EMB145LR · Landing Gear Retraction/Extension System
  > AFTER GEAR RETRACTION CONTINUOUS THUMPING NOISE HEARD FROM NOSE BAY AREA. AFTER R/H MLG UP LOCK BOX WAS R&R'D REF LOG PAGE 260829-2. NO NOISE HEARD IN NOSE BAY AREA. NO DEFECT NOTED.
- [SDR HNAA2021060900235](https://openairdocs.org/sdr/HNAA2021060900235.md): Actuator · faulted · Jun 8, 2021 · N629AE · Emb EMB145LR · Stabilizer Position Indicating
  > PITCH TRIM BACK UP INOP. R&R HORIZONTAL STABILIZE ACTUATOR IAW EMB 145 AMM 27-40-02-000/A00-801A REQUIRES ZERO RIG CHECK AMM TASK 27-40-02-700-801-A/500. PERFORMED ELECTRICAL ZERO POSITION OF HORIZONTAL STABILIZER IAW AMM 27-40-02-801-A/500 OPS CHECK GOOD P/N
- [SDR HNAA2021052500225](https://openairdocs.org/sdr/HNAA2021052500225.md): Control Unit · failed · May 21, 2021 · N629AE · Emb EMB145LR · Stabilizer Control System
  > PDIS 629 27-41 2580431 21MAY21 CLT CLOSE PITCH TRIM MAIN INOP MESSAGE AT 6000 FT AFTER TAKE OFF FACT 21MAY21 15:06 CLT R/R HORIZONTAL STAB CONTROL UNIT IAW AMM 27-40-01.OPS CHECK GOOD OK FOR SERVICE.
- [SDR HNAA2019082300235](https://openairdocs.org/sdr/HNAA2019082300235.md): Control Module · malfunctioned · Aug 22, 2019 · N629AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE DISPLAYED. REMOVED AND REPLACED CONTROL MODULE ASSY IAW AMM 33-21-01 SUBTASK 33-25-00-700-801-A AND 33-50-00-700-801-A. OPS CHECK GOOD,OK FOR SERVICE
- [SDR HNAA2019042200111](https://openairdocs.org/sdr/HNAA2019042200111.md): Bleed Valve · failed · Apr 20, 2019 · N629AE · Emb EMB145LR · Compressor Bleed Valve
  > PDIS 629 36-10 2048721 20APR19 PHL CLOSE BLD 2 VLV FAIL WHEN ENTERING ICING CONDITIONSFACT 20APR19 15:10 PHL R&R'D ENG BLEED VALVE 2 IAW EMB 145 AMM 36-11-05 OPS CHECK GOOD AT THIS TIME
- [SDR HNAA2019041700102](https://openairdocs.org/sdr/HNAA2019041700102.md): Inverter · failed · Apr 16, 2019 · N629AE · Emb EMB145LR · Emergency Lighting
  > 629 33-51 0014160 16APR19 RIC CLOSE EMERGENCY LIGHT OVER SERVICE DOOR DOORWAY WILL NOT ILLUMINATE 27751 00 NGR FACT 16APR19 09:57 RIC DISCONNECTED EMERGENCY LIGHT INVERTER + RESEATED
- [SDR HNAA2018120500304](https://openairdocs.org/sdr/HNAA2018120500304.md): Display · malfunctioned · Dec 2, 2018 · N629AE · Emb EMB145LR · Central Display
  > DURING TAXI IN TO GATE. FO'S PFD WENT BLANK ALONG WITH ELECTRICAL ODOR. SELECTED AVIONICS BUSS 2 OFF. SWAPED FO'S PFD AND MFD PER AMM 34-22-01 AND DEACTIVATED MFD PER MEL.
- [SDR HNAA2018092800236](https://openairdocs.org/sdr/HNAA2018092800236.md): Wire · chafed · Sep 27, 2018 · N629AE · Emb EMB145LR · Light System Wiring
  > DISCREPANCY: THE EMERGENCY LIGHTS CONNECTED TO THE #2 POWER SUPPLY DID NOT COME ON DURING OPS CHECK. CORRECTIVE ACTION: REMOVED CIELING PANEL IN FRONT OF GALLEY TO GAIN ACCESS TO #2 POWER SUPPLY. FOUND CHAFFED WIRES NEAR #2 POWER SUPPLY, REPLACED WIRES AND REI
- [SDR HNAA2018072500168](https://openairdocs.org/sdr/HNAA2018072500168.md): Module · malfunctioned · Jul 23, 2018 · N629AE · Emb EMB145LR · Cabin Pressure Control System
  > ABSENCE OF PRESSURIZATION INDICATIONS ON EICAS PANEL. DASH LINES IN BOXES. R&R CPAM, C/W OP AND ALT CK'S REF 21-32-01, C/W NR 3 STATIC SYSTEM LK CK. OK IAW TASK 34-13-00-790-804.
- [SDR HNAA2018042000085](https://openairdocs.org/sdr/HNAA2018042000085.md): Pitch Control · malfunctioned · Apr 19, 2018 · N629AE · Emb EMB145LR · Elevator Control System
  > MAIN PITCH TRIM IS INOPERATIVE. INSPECTED & OPERATED THE MAIN & B/U PITCH TRIM SWITCHES WITH NO FAULTS, COMPLIED WITH FIM 27-43-00-810-801-A, AND 27-43-810-802-A, NO FAULTS FOUND. R & R THE HSCU IAW AMM 27-40-01. OPS CHECKED GOOD.
- [SDR HNAA2018011600009](https://openairdocs.org/sdr/HNAA2018011600009.md): Warning Message · false indication · Jan 15, 2018 · N629AE · Emb EMB145LR · Airfoil Anti/De-ice System
  > ICE CONDITION ADV MESSAGE DISPLAYED. ACFT WAS NOT IN ICING CONDITIONS. MESSAGE WENT OUT AT 13000 FEET AND CREW SMELLED SOMETHING BURNING. PERFORMED ICE DETECTION SYSTEM OPS CHECK IAW AMM 30-80-00. ALL OPS CHECKED GOOD. ICE PROTECTION ELECTRICAL TEST ACCO
- [SDR HNAA2018011200005](https://openairdocs.org/sdr/HNAA2018011200005.md): Duct · unsecure · Jan 11, 2018 · N629AE · Emb EMB145LR · Cabin Pressure Control System
  > RAPID DEPRESSURIZATION WHILE HOLDING SHORT IN AUTOMATIC MODE. MANUAL MODE OVER PRESSURIZED. INSPECTED THE NR 1 PACK AREA AND FOUND A DUCT LOOSE. SECURED THE DUCT. PRESSURIZED IAW AMM 21-31-00. OPS CHECKED GOOD. OKAY FOR SERVICE.
- [SDR SIMA20171128003](https://openairdocs.org/sdr/SIMA20171128003.md): Skin · damaged · Nov 28, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING POST INSPECTION WALK AROUND, FOUND A DENT AND SCRAPE UNDER CARGO DOOR. REPAIRED IAW ERS-EM-53MR-3025.
- [SDR SIMA20171117002](https://openairdocs.org/sdr/SIMA20171117002.md): Control Rod · corroded · Nov 17, 2017 · N629AE · Emb EMB145LR · Landing Gear Door Retract Section
  > LEFT AND RIGHT, FORWARD AND AFT, FOUR MAIN LANDING GEAR DOOR CONTROL RODS ARE CORRODED. REMOVED AND REPLACED THE CONTROL RODS IAW AMM 32-10-06, STEPS 1, 5, & 9, AND ETN-EM-32-256.
- [SDR SIMA20171109007](https://openairdocs.org/sdr/SIMA20171109007.md): Attach Fitting · worn · Nov 9, 2017 · N629AE · Emb EMB145LR · Wing, Attach Fittings
  > INBOARD SPOILER FITTING ON REAR SPAR 3 HAS A WORN HAT BUSH BORE. REMOVED AND REPLACED INBD SPOILER ATTACH BRACKET (INCLUDED NEW HAT BUSHINGS) IAW AMM 57-51-02.
- [SDR SIMA20171108008](https://openairdocs.org/sdr/SIMA20171108008.md): Attach Angle · cracked · Nov 8, 2017 · N629AE · Emb EMB145LR · Wing, Attach Fittings
  > LEFT WING EIGHTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.
- [SDR SIMA20171108009](https://openairdocs.org/sdr/SIMA20171108009.md): Attach Angle · cracked · Nov 8, 2017 · N629AE · Emb EMB145LR · Wing, Attach Fittings
  > LEFT WING FIFTH AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142 IAW NRTC E605570.
- [SDR SIMA20171108007](https://openairdocs.org/sdr/SIMA20171108007.md): Attach Angle · cracked · Nov 8, 2017 · N629AE · Emb EMB145LR · Wing, Attach Fittings
  > RIGHT WING THIRD AFT LOWER ATTACH ANGLE FOR LATERAL PANEL IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN ER ETN-EM-53-142.
- [SDR SIMA20171107009](https://openairdocs.org/sdr/SIMA20171107009.md): Skin Panel · gouged · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > CENTER FUSELAGE UPPER SKIN PANEL BETWEEN FR 35-36 STRG 1R-3R GOUGES, PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2836.
- [SDR SIMA20171107008](https://openairdocs.org/sdr/SIMA20171107008.md): Frame · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Frame
  > COCKPIT LT FRAME 10 IS CRACKED, BELOW DV WINDOW. REMOVED AND REPLACED COCKPIT LT FRAME 10 SECTION BELOW DV WINDOW IAW SRM 51-40-02.
- [SDR SIMA20171107002](https://openairdocs.org/sdr/SIMA20171107002.md): Attach Angle · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > COCKPIT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. REMOVED AND REPLCED THE ATTACH ANGLE IAW SRM 51-40-02.
- [SDR SIMA20171107003](https://openairdocs.org/sdr/SIMA20171107003.md): Frame · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Frame
  > COCKPIT FRAME 10 IS CRACKED, BELOW WINDOW. REMOVED AND REPLACED THE FRAME IAW 51-40-02.
- [SDR SIMA20171107004](https://openairdocs.org/sdr/SIMA20171107004.md): Cleat · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > COCKPIT LT FRAME 10 CLEAT IS CRACKED. -INSTALLED A NEW CLEAT IAW SRM 51-40-02.
- [SDR SIMA20171107005](https://openairdocs.org/sdr/SIMA20171107005.md): Attach Angle · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Main, Attach Fittings
  > COCKPIT LT FRAME 10 ATTACH ANGLE AT TOP OF FRAME IS CRACKED. INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.
- [SDR SIMA20171107006](https://openairdocs.org/sdr/SIMA20171107006.md): Support Bracket · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FORWARD TORSION BAR SUPPORT BRACKET AT FRAME 61 CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.
- [SDR SIMA20171107007](https://openairdocs.org/sdr/SIMA20171107007.md): Attach Angle · cracked · Nov 7, 2017 · N629AE · Emb EMB145LR · Wing, Attach Fittings
  > LEFT WING SECOND AFT LOWER ATTACH ANGLE IS CRACKED IN SEVERAL PLACES. -INSTALLED A NEW ATTACH ANGLE IAW ETN-EM-53-142.
- [SDR SIMA20170927002](https://openairdocs.org/sdr/SIMA20170927002.md): A/C Pack · malfunctioned · Sep 27, 2017 · N629AE · Emb EMB145LR · Cabin Cooling System
  > NR 2 PACK OVERLOAD IN FLIGHT AT FL 250 WITH THE NR 1 PACK. REMOVED AND REPLACED THE RT PACK VALVE IAW AMM 21-51-01. OPS CHECK FAILED. OPEN
- [SDR SIMA20170824001](https://openairdocs.org/sdr/SIMA20170824001.md): Lamp · cracked · Aug 24, 2017 · N629AE · Emb EMB145LR · Exterior Lighting
  > NR 1 LANDING LIGHT CRACKED. R & R THE LANDING LIGHT LAMP IAW AMM 33-41-02. OPS CHECKED OK.
- [SDR SIMA20170626003](https://openairdocs.org/sdr/SIMA20170626003.md): Light · inoperative · Jun 26, 2017 · N629AE · Emb EMB145LR · Emergency Lighting
  > LEFT OVERWING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING PANEL EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR ASOA20160609054](https://openairdocs.org/sdr/ASOA20160609054.md): Connector · disconnected · Jun 9, 2016 · N629AE · Emb EMB145LR · Light System Wiring
  > THE CREW REPORTED THAT THE FRONT DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE WHEN IN EMERGENCY LIGHT MODE. MAINTENANCE INSPECTED THE ACFT AND FOUND THAT THE SIGN WAS DISCONNECTED. MAINTENANCE RECONNECTED THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFE
- [SDR SIMA20150515006](https://openairdocs.org/sdr/SIMA20150515006.md): Skin · cracked · May 15, 2015 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED ON FRAME 75 AT THIRD FASTENER BELOW STRINGER 2R, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN CRACK ON FRAME 75 AT THIRD FASTENER IAW ERS-EM-53MR-1308.
- [SDR SIMA20150515005](https://openairdocs.org/sdr/SIMA20150515005.md): Access Door · cracked · May 15, 2015 · N629AE · Emb EMB145LR · Electrical/Electronic Compartment Doors
  > REAR ELECTRONICS ACCESS HATCH 272DR IS CRACKED UNDER EYELET BRACKET. REPAIRED IAW ERS-EM-52MR-334.
- [SDR SIMA20150514004](https://openairdocs.org/sdr/SIMA20150514004.md): Skin · chafed · May 14, 2015 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > AIRLINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB. PERFORMED PERMANENT REPAIR OF AIR LINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB IAW ERS-EM-53MR-1307.
- [SDR SIMA20150514005](https://openairdocs.org/sdr/SIMA20150514005.md): Skin · cracked · May 14, 2015 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN JUST AFT OF FRAME 75 ABOVE
- [SDR SIMA20150511007](https://openairdocs.org/sdr/SIMA20150511007.md): Wire · broken · May 11, 2015 · N629AE · Emb EMB145LR · Light System Wiring
  > EMERGENCY LIGHT STRIP NR 3 HAS BROKEN WIRE ON LIGHT STRIP SIDE. R & R EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150511006](https://openairdocs.org/sdr/SIMA20150511006.md): Connector · damaged · May 11, 2015 · N629AE · Emb EMB145LR · Light System Wiring
  > POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 HAS A DAMAGED CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 6 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR OPERATIONS CHECK.
- [SDR SIMA20150511005](https://openairdocs.org/sdr/SIMA20150511005.md): Connector · missing · May 11, 2015 · N629AE · Emb EMB145LR · Light System Wiring
  > POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IS MISSING A CONNECTOR. INSTALLED CONNECTOR & PIN ON POWER SUPPLY HARNESS, ACFT SIDE, TO EMER LIGHT STRIP NR 4 IAW SWPM 20-21-00, 20-50-00 & 20-50-01. SEE NRTC E450553 FOR OPERATIONS CHECK.
- [SDR SIMA20150511003](https://openairdocs.org/sdr/SIMA20150511003.md): Wire · broken · May 11, 2015 · N629AE · Emb EMB145LR · Light System Wiring
  > EMERGENCY LIGHT STRIP NR 2 HAS BROKEN WIRE ON LIGHT STRIP SIDE. EMER LIGHT STRIP NR 2 IS INOPERATIVE. R & R EMER LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150510010](https://openairdocs.org/sdr/SIMA20150510010.md): Power Supply · inoperative · May 10, 2015 · N629AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT STRIP NR 1 IS INOPERATIVE. R & R NR 2 BATTERY POWER SUPPLY & BATTERY PACK IAW AMM 33-50-04 & AMM 20-10-01. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150421015](https://openairdocs.org/sdr/SIMA20150421015.md): Skin · cracked · Apr 21, 2015 · N629AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH. REPAIRED SKIN CRACK AT FRAME 75 & STRINGER 2L IAW ERS-EM-53MR-1309.

Next page: https://openairdocs.org/aircraft/N629AE/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 = 'N629AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N629AE/reports

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