# Service difficulty reports: N722AE, cancelled Sep 9, 2019

A list on [N722AE, cancelled Sep 9, 2019](https://openairdocs.org/deregistered/N722AE-2019-09-09.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 · 67 reports

- [SDR SIMA20130918008](https://openairdocs.org/sdr/SIMA20130918008.md): Battery · inoperative · Sep 18, 2013 · N722AE · Emb EMB135LR · Emergency Lighting
  > NR 4 EMERGENCY BATTERY DEAD. R & R NR 4 EMERGENCY BATTERY IAW WC 33-700-19.
- [SDR SIMA20130918007](https://openairdocs.org/sdr/SIMA20130918007.md): Battery · discharged · Sep 18, 2013 · N722AE · Emb EMB135LR · Emergency Lighting
  > NR 3 EMERGENCY BATTERY DEAD. R & R NR 3 EMERGENCY BATTERY IAW W/C 33-700-19
- [SDR SIMA20130524001](https://openairdocs.org/sdr/SIMA20130524001.md): Handle · out of adjust · May 24, 2013 · N722AE · Emb EMB135LR · Passenger/Crew Doors
  > THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN FROM INSIDE. THE ACFT WAS REMOVED FROM SERVICE. RE-ADJUSTED INTERIOR MAIN CABIN DOOR HANDLE IAW AMM 52-18-05. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
- [SDR SIMA20130509001](https://openairdocs.org/sdr/SIMA20130509001.md): Fairing · damaged · May 8, 2013 · N722AE · Emb EMB135LR · Elevator, Plate/Skin
  > ON FLIGHT 4563 THE CREW REPORTED THAT ON APPROACH THE AIRCRAFT WAS STRUCK BY LIGHTNING 2 SEPARATE TIMES. LOSS OF INSTRUMENTATION COLOR ON BOTH PFD'S BUT ALL SYSTEMS SHOWED NORMAL. THE CREW DECLARED AN EMERGENCY AS A PRECAUTION AND LANDED WITHOUT INCIDENT. T
- [SDR SIMA20130429005](https://openairdocs.org/sdr/SIMA20130429005.md): Wire Harness · faulty · Apr 29, 2013 · N722AE · Emb EMB135LR · Flight Control System Wiring
  > ON FLIGHT 4477 THE CREW REPORTED THE MAIN PITCH TRIM WAS INOPERABLE DURING CLIMBOUT. BACKUP PITCH TRIM WORKED FINE. THE CREW DECLARED AN EMERGENCY AND FOLLOWED AOM-1 PROCEDURES. THE CREW REQUESTED FOR CFR TO STANDBY FOR LANDING AS A PRECAUTIONARY MEASURE.
- [SDR SIMA20130402002](https://openairdocs.org/sdr/SIMA20130402002.md): Wire · broken · Apr 2, 2013 · N722AE · Emb EMB135LR · Light System Wiring
  > DURING B INSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND BROKEN WIRE AT SP7376. REPAIRED WIRE IAW STANDARD WIRING PRACTICES MANUAL 20-21-00. THE AIRCRAFT WAS RETURNED TO SER
- [SDR SIMA20130322005](https://openairdocs.org/sdr/SIMA20130322005.md): Light · inoperative · Mar 22, 2013 · N722AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY SIDEWALL LIGHTS OUT AT PASSENGER SEATS 11 AND 12 B / C. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY SIDEWALL LIGHT AT PASSENGER SEAT 11 AND 12B/C IAW EMB AMM 33-21-06. THE OPERA
- [SDR SIMA20130311006](https://openairdocs.org/sdr/SIMA20130311006.md): Servo · malfunctioned · Mar 11, 2013 · N722AE · Emb EMB135LR · Autopilot Main Servo
  > ON FLIGHT 4513 - THE CREW REPORTED THE ELEVATOR FLUCTUATED IN MODERATE TURBULENCE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELEVATOR AUTO PILOT SERVO IAW EMB 135 AMM 22-11-04-000-801 / 22-11-04-40
- [SDR SIMA20130116008](https://openairdocs.org/sdr/SIMA20130116008.md): Duct · defective · Jan 16, 2013 · N722AE · Emb EMB135LR · Pneumatic Distribution System
  > ON FLIGHT 4521 THE CREW REPORTED THEY ENCOUNTERED A BLEED 1 LEAK THRU FL 1200 IN ICING CONDITIONS. THE CREW RAN THE EMERGENCY PROCDURES VOL 1. ALL INDICATIONS OF A BLEED LEAK WENT AWAY LESS THAN 1 MINUTE FROM CLOSING THE EBV. THE CREW HAD TO CLIMB TO FL250
- [SDR SIMA20121001002](https://openairdocs.org/sdr/SIMA20121001002.md): Unknown · odor · Oct 1, 2012 · N722AE · Emb EMB135LR · Air Distribution System
  > ON FLIGHT 4419 THE CREW REPORTED THE FLIGHT ATTENDANT SMELLED ELECTRICAL BURNING IN PSU AT SEAT 7A, VERY SLIGHT ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND OPEN PSU. NO ODOR NOTICED AT THIS TIME. PERFORMED OPERATIONAL CHECK IAW AMM 33-25-00-
- [SDR SIMA20120708001](https://openairdocs.org/sdr/SIMA20120708001.md): Battery · discharged · Jul 8, 2012 · N722AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR, FORWARD AISLE OVERHEAD, COCKPIT STEP AND EXTERIOR LEFT FORWARD EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER ASSEMBLY IAW EMB 135 AMM 3
- [SDR SIMA20120406009](https://openairdocs.org/sdr/SIMA20120406009.md): Inverter · failed · Apr 6, 2012 · N722AE · Emb EMB135LR · Emergency Lighting
  > DURING B-INSPECTION, FOUND THE EMERGENCY LIGHT AT ROWS 3/4 AND 5/6 FAILED TO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA20120323001](https://openairdocs.org/sdr/SIMA20120323001.md): Wire · broken · Mar 23, 2012 · N722AE · Emb EMB135LR · Light System Wiring
  > DURING MAINTENANCE INSPECTION FOUND SEAT ROW 10 FLOOR PROXIMTY LIGHT STRIP WIRES BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SEAT ROW 10 FLOOR PROXIMTY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT W
- [SDR SIMA20120229005](https://openairdocs.org/sdr/SIMA20120229005.md): Light · inoperative · Feb 29, 2012 · N722AE · Emb EMB135LR · Emergency Lighting
  > DURING B-INSPECTION FOUND LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-07. OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA2012039005](https://openairdocs.org/sdr/SIMA2012039005.md): Flashlight · intermittent · Feb 8, 2012 · N722AE · Emb EMB135LR · Emergency Equipment
  > ON FLIGHT 4512, THE CREW REPORTED THE FLIGHT ATTENDANT`S FLASHLIGHT INTERMITTENTLY COMES ON & OFF DOES NOT STAY ON ALL THE TIME. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF THE FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-51-01. OPERATIO
- [SDR SIMA201202702](https://openairdocs.org/sdr/SIMA201202702.md): Duct · leaking · Jan 26, 2012 · N722AE · Emb EMB135LR · Cabin Cooling System
  > ON FLIGHT 4525 THE CREW REPORTED AT FLIGHT LEVEL 360 THE CABIN PRESSURE STARTED CLIMBING TO 9700. THE CREW DESCENDED BUT IT KEPT CLIMBING. THE CREW SAID THEY FINALLY GOT A CABIN WARNING MESSAGE AND DID THE CHECK LISTS BUT IT NEVER STABILIZED. THE CREW DECLA
- [SDR SIMA2012025005](https://openairdocs.org/sdr/SIMA2012025005.md): Door · lack of lube · Jan 24, 2012 · N722AE · Emb EMB135LR · Passenger/Crew Doors
  > ON FLIGHT 4489 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. THE DOOR OPEN HANDLE NEEDED EXCESSIVE FORCE AT THE MIDWAY POINT. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR IAW EMB 135 AMM 52-18-00. NO PARTS REMOVED O
- [SDR SIMA2012013008](https://openairdocs.org/sdr/SIMA2012013008.md): Wire · broken · Dec 30, 2011 · N722AE · Emb EMB135LR · Light System Wiring
  > DURING MAINTENANCE INSPECTION, FOUND EMERGECNY PATH LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RE-SECURED BROKEN WIRE ON EMERGENCY LIGHT IAW WM 20-30-00. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA2011325003](https://openairdocs.org/sdr/SIMA2011325003.md): Flashlight · inoperative · Nov 19, 2011 · N722AE · Emb EMB135LR · Emergency Equipment
  > ON FLIGHT 4411 THE CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AE ERJ AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SIMA201129805](https://openairdocs.org/sdr/SIMA201129805.md): Fitting · excess play · Oct 22, 2011 · N722AE · Emb EMB135LR · Aileron Control System
  > DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON POWER CONTROL ACTUATOR ATTACHMENT HAS PLAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ACTUATOR FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201129804](https://openairdocs.org/sdr/SIMA201129804.md): Fitting · defective · Oct 22, 2011 · N722AE · Emb EMB135LR · Aileron Control System
  > DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPER FITTING REQ'S REPLACEMENT (WILL NOT FIT IN ALLIGNMENT JIG.) THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201128504](https://openairdocs.org/sdr/SIMA201128504.md): Frame · cracked · Oct 10, 2011 · N722AE · Emb EMB135LR · Fuselage Main, Frame
  > DURING MAINTENANCE BASE VISIT FOUND FRAME 67 CRACKED JUST ABOVE STRINGER 16 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 67 AT STRINGER 16 LEFT IAW EMB SRM 53-00-04. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA201128505](https://openairdocs.org/sdr/SIMA201128505.md): Sill · corroded · Oct 9, 2011 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING INSECTION, FOUND CARGO DOOR SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA201128002](https://openairdocs.org/sdr/SIMA201128002.md): Sill · corroded · Oct 6, 2011 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02.
- [SDR SIMA201128001](https://openairdocs.org/sdr/SIMA201128001.md): Floor Support · corroded · Oct 6, 2011 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE BASE INSPECTION VISIT FOUND THE CENTER OMEGA BEAM CORRODED AT CARBON CROSSMEMBER BETWEEN FRAMES 24 AND 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. CENTER OMEGA BEAM CORRODED AT CARBON CROSSMEMBER BETWEEN FRAMES 24 AND 25. THE AIRCRAFT WAS
- [SDR SIMA201127901](https://openairdocs.org/sdr/SIMA201127901.md): Floor Support · corroded · Oct 6, 2011 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION FOUND THE LEFT OMEGA BEAM HAS CORROSION BY THE CARBON CROSSMEMBER AT FRAME 20. ACFT REMOVED FROM SERVICE. REPAIRED LEFT HAND OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10. ACFT RETURNED TO SERVICE.
- [SDR SIMA201126204](https://openairdocs.org/sdr/SIMA201126204.md): Power Supply · inoperative · Sep 16, 2011 · N722AE · Emb EMB135LR · Emergency Lighting
  > LT OVERWING EXTERIOR LIGHT INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY POWER SUPPLY IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD.
- [SDR SIMA201123510](https://openairdocs.org/sdr/SIMA201123510.md): Control Unit · malfunctioned · Aug 6, 2011 · N722AE · Emb EMB135LR · Stabilizer Control System
  > ON FLIGHT 2983 THE CREW REPORTED A PTRIM MAIN INOPERABLE WARNING MESSAGE ON EICAS. THE CREW FOLLOWED AOM VOL 1 DESELECTED MAIN SYSTEM CUTOUT, THE BACK UP SEEMS TO WORK. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FRO
- [SDR SIMA201123509](https://openairdocs.org/sdr/SIMA201123509.md): Trim Switch · inoperative · Aug 6, 2011 · N722AE · Emb EMB135LR · Stabilizer Control System
  > ON FLIGHT 2977 DURING CRUISE AT FL 340, THE CREW REPORTED A PTRIM MAIN INOPERABLE WARNING MESSAGE ON EICAS. THE CREW FOLLOWED AOM1 PROCEDURES, BACK UP SYSTEM OK. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVIC
- [SDR SIMA201119902](https://openairdocs.org/sdr/SIMA201119902.md): Potentiometer · faulty · Jul 15, 2011 · N722AE · Emb EMB135LR · Landing Gear Steering System
  > ON FLIGHT 3339 THE CREW REPORTED AN UNCOMMANDED SWERVE TO THE LEFT DURING THE INITIAL TAKEOFF ROLL. THE CREW DID NOT RECEIVE AURAL WARNING FOR BRAKES, SPOILER, FLAPS, OR TRIM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE AIRCRAFT WAS REMOVED F
- [SDR SIMA201118203](https://openairdocs.org/sdr/SIMA201118203.md): Roller · lack of lube · Jul 1, 2011 · N722AE · Emb EMB135LR · Passenger/Crew Doors
  > UPON ARRIVAL TO GATE, F/A REPORTED MAIN PASSENGER DOOR HARD TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLERS IAW EMB-135 AND AMM53-21-02. LUBRICATED ACTUATING AND LOCKING MECHANISM AND OPS CHECK GOOD IAW EMB-135 AMM 52-1800.
- [SDR SIMA201111503](https://openairdocs.org/sdr/SIMA201111503.md): Gust Lock · binding · Apr 23, 2011 · N722AE · Emb EMB135LR · Gust Lock Damper System
  > ON FLIGHT 2865 ON TAKEOFF THE CREW REPORTED THE ELECTRO GUST LOCK WOULD NOT RELEASE. THE GUST LOCK REMAINED ILLUMINATED AND THE LOWER LEVEL WOULD NOT RELEASE AND THE ELEVATOR WOULD NOT MOVE. THE CAPTAIN ABORTED THE TAKEOFF. THE AIRCRAFT WAS REMOVED FROM SER
- [SDR SIMA201109801](https://openairdocs.org/sdr/SIMA201109801.md): Windshield · cracked · Apr 6, 2011 · N722AE · Emb EMB135LR · Flight Compartment Windows
  > ON FLIGHT 3278 DURING THE CLIMBOUT THE CAPTAINS LEFT FRONT WINDSCREEN OUTER PANE CRACKED AFTER TAKEOFF. NO BIRD RESIDUE OBSERVED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FRONT WINDSHIELD IAW EMB 135 AMM 56-10-01. THE OPERATIONAL
- [SDR SIMA201109601](https://openairdocs.org/sdr/SIMA201109601.md): Windshield · cracked · Apr 4, 2011 · N722AE · Emb EMB135LR · Flight Compartment Windows
  > ON FLIGHT 2820 THE CREW REPORTED THAT DURING THE LANDING ROLL OUT AT APPROXIMATELY 120 KNOTS THE FIRST OFFICER’S FORWARD COCKPIT WINDSHIELD SHATTERED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE FIRST
- [SDR SIMA201100502](https://openairdocs.org/sdr/SIMA201100502.md): Ground Stud · loose · Jan 5, 2011 · N722AE · Emb EMB135LR · Light System Wiring
  > FOR FLIGHT 4413 MAINTENANCE DISCOVERED THE MAIN PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE GROUND ON EMERGENCY LIGHT SOCKET. RE-TIGHTENED THE LOOSE GROUND IAW WM 20-13-05. THE OPERATIONAL TEST WAS GO
- [SDR SIMA201027102](https://openairdocs.org/sdr/SIMA201027102.md): Inverter · inoperative · Sep 28, 2010 · N722AE · Emb EMB135LR · Emergency Lighting
  > DURING MAINTENANCE BASE VISIT FOUND THE NR 4 EMERGENCY LIGHT PROXIMITY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 INVERTER IAW EMB135 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED
- [SDR SIMA201017201](https://openairdocs.org/sdr/SIMA201017201.md): Unknown · odor · Jun 17, 2010 · N722AE · Emb EMB135LR · Air Distribution System
  > ON FLIGHT 4400 DURING THE DESCENT THE FLIGHT ATTENDANT REPORTED A BURNING ODOR IN THE GALLEY NO VISIBLE SMOKE WAS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED VISUAL INSPECTION OF OVERHEAD LIGHT ASSEMBLY, HOT CONTAINER HEATING SYSTEM AND CD PLA
- [SDR SIMA201015401](https://openairdocs.org/sdr/SIMA201015401.md): Battery · discharged · Jun 3, 2010 · N722AE · Emb EMB135LR · Emergency Equipment
  > DURING PHASE 3A MAINTENANCE VISIT FOUND THE CO-PILOT’S FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CO-PILOT'S FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR SIMA 200922203](https://openairdocs.org/sdr/SIMA%20200922203.md): Stringer · damaged · Aug 7, 2009 · N722AE · Emb EMB135LR · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR, DURING THE MAIN BASE VISIT INSPECTION PERMANENT REPAIR OF DEFERRED LIGHTNING STRIKE DAMAGE AT FRAME 15 AND STRINGER 18 LEFT. CUT OUT DAMAGED SECTION ON STRINGER 18 LEFT. FABRICATED A 40 INCH SPLICE SECTION FROM PART NUMBER PE11001-F4. PREPPED
- [SDR SIMA200922202](https://openairdocs.org/sdr/SIMA200922202.md): Skin · cracked · Aug 7, 2009 · N722AE · Emb EMB135LR · Fuselage Main, Plate/Skin
  > MAJOR REPAIR DURING MAINTENANCE BASE INSPECTION THE FUSELAGE SKIN WAS FOUND CRACKED FORWARD AND AFT OF RIVET ON FRAME 75 AND STRINGER 2 LEFT CUT OUT DAMAGE. FABRICATED A.8" X.78" FILLER, A 9.5" X 7.4" DOUBLER AND A.9" X 2.7" SHIM USING AL2024T3 0.063". PR
- [SDR SIMA200922204](https://openairdocs.org/sdr/SIMA200922204.md): Angle · cracked · Aug 6, 2009 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > MAJOR REPAIR DURING MAIN BASE VISIT INSPECTION THE LEFT HAND FUSELAGE TO VERTICAL "L" PROFILE WAS FOUND CRACKED APPROXIMATELY 6" FROM THE AFT END. CUT OUT DAMAGED AREA. FABRICATED A 2.7" X 8.6" FILLER AND A 7.8" X 2.5" SPLICE USING AL2024T3 0.100". PREPPED,
- [SDR SIMA200726002](https://openairdocs.org/sdr/SIMA200726002.md): Battery Pack · inoperative · Sep 17, 2007 · N722AE · Emb EMB135LR · Emergency Lighting
  > EMERGENCY LIGHTS ON BOTH OVERWING AND BACK SECTION OF CENTER AISLE EMERGENCY LIGHTS COME ON AND THEN GO DIM UNTIL COMPLETELY OFF. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTING ASSEMBLY IAW EMB AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE
- [SDR SIMA200719803](https://openairdocs.org/sdr/SIMA200719803.md): Landing Gear · inoperative · Jul 16, 2007 · N722AE · Emb EMB135LR · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT, GEAR LEVER WOULD NOT MOVE. RETURNED TO LGA.
- [SDR SIMA200720706](https://openairdocs.org/sdr/SIMA200720706.md): Floorbeam · corroded · Jun 27, 2007 · N722AE · Emb EMB135LR · Fuselage Main, Floor Beam
  > LEFT OMEGA BEAM AT FRAME 21 CORRODED. BLENDED OUT CORROSION AND RESTORE FINISH IAW EMB SRM 51-40-02, 51-20-03, 51-40-06 AND EMB IC2007-145/04209, DATED JUNE 21, 2007. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200720430](https://openairdocs.org/sdr/SIMA200720430.md): Beam · corroded · Jun 27, 2007 · N722AE · Emb EMB135LR · Fuselage Main, Structure
  > CARGO DOOR LOWER BEAM CORRODED. REMOVED AND REPLACED BEAM IAW EMB SRM 51-40-02, 51-20-03 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200720509](https://openairdocs.org/sdr/SIMA200720509.md): Frame · dented · Jun 26, 2007 · N722AE · Emb EMB135LR · Fuselage Main, Frame
  > FRAME 68 WEB BETWEEN STRINGERS 10L AND 11L DENTED AND CHAFED. FABRICATED AND INSTALLED DOUBLER IAW EMB IC2007-145/04209, PARAGRAPH 2, DATED JUNE 21,2007. AIRCRAFT RETURNED TO SERVICE.
- [SDR SIMA200529305](https://openairdocs.org/sdr/SIMA200529305.md): Floor Support · corroded · Oct 14, 2005 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER, REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K)
- [SDR SIMA200529303](https://openairdocs.org/sdr/SIMA200529303.md): Floor Support · damaged · Oct 14, 2005 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > DAMAGED FASTENER HOLE WAS DISCOVERED ON THE LT OMEGA BEAM FLOOR SUPPORT TOWER AT FRAME 20. PERFORMED A CUT OUT OF THE SUPPORT TOWER TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K)
- [SDR SIMA200529008](https://openairdocs.org/sdr/SIMA200529008.md): Floor Support · corroded · Oct 13, 2005 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K)
- [SDR SIMA200529302](https://openairdocs.org/sdr/SIMA200529302.md): Sill · corroded · Oct 13, 2005 · N722AE · Emb EMB135LR · Fuselage Miscellaneous Structure
  > THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS ON THE SILL TO REMOVED THE CORROSION. FABRICATED 3 REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW2120060542) (K)

Next page: https://openairdocs.org/deregistered/N722AE-2019-09-09/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 = 'N722AE' AND deregistration_id = 'N722AE-2019-09-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N722AE-2019-09-09/reports

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