# Service difficulty reports: N621AE

A list on [N621AE](https://openairdocs.org/aircraft/N621AE.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 · 182 reports

- [SDR HNAA2022032800127](https://openairdocs.org/sdr/HNAA2022032800127.md): None · none · Mar 23, 2022 · N621AE · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > PDIS 621 30-42 2669531 23MAR22 RIC CLOSE WINDSHIELD HEAT 1 FAIL IN ICING CONDITIONS FACT 25MAR22 18:04 RIC PERFORMED FIM TASK 30-42-00-810-801-A PAGE 220. BLOCK 1=NO, BLOCK 2=NO, BLOCK 3=NO,BLOCK 4=NO, BLOCK 5=NO, BLOCK 6=NO, BLOCK 7=YES, BLOC
- [SDR HNAA2022030900121](https://openairdocs.org/sdr/HNAA2022030900121.md): None · none · Mar 7, 2022 · N621AE · Emb EMB145LR · Airfoil Anti/De-ice System
  > PDIS 621 30-10 2697351 07MAR22 PHL CLOSE IN ICING CONDITIONS AT 20000 FT, STAB A/I SW DID NOT ILLUMINATE THEN GOT STAB A/I FAIL THEN ICE COND A/I INOP EICAS MSGS. FACT 07MAR22 21:06 PHL PERFORMED ANTI ICE OPS CHECK IAW AMM 30-
- [SDR HNAA2022030700118](https://openairdocs.org/sdr/HNAA2022030700118.md): None · none · Mar 3, 2022 · N621AE · Emb EMB145LR · Engine Thrust Reverser
  > PDIS 621 78-34 2697301 03MAR22 BTV CLOSE DURING T/O ROLL ENG 1 REV DISAGREE MESSAGE APPEARED ON EICAS FACT 06MAR22 03:58 PHL UNLOCKED #1 TR I.A.W AMM 78-31-01. PREFORMED OPS CHECK OF #1 TR I.A.W AMM 78-31-01. OPS CHECK GOOD. OK FOR SERVICE AT
- [SDR HNAA2021110100526](https://openairdocs.org/sdr/HNAA2021110100526.md): Unknown · odor · Oct 29, 2021 · N621AE · Emb EMB145LR · Air Distribution System
  > LEVELING AT CRUISE FLIGHT SMELLED BURNING ODOR EXPERIENCED BY ALL CREW MEMBERS, RAN QRH AND AFTER TURNING OFF GASPER SMELL WENT AWAY. FOLLOWED FIM 21-20-00-810-801-A FOUND SLIGHT ELECTRICAL SMELL ON BOTH FLIGHT DECK FLASHLIGHTS. REM AND INSP FLASHLIGHT ASSY
- [SDR HNAA2021100400473](https://openairdocs.org/sdr/HNAA2021100400473.md): None · none · Oct 2, 2021 · N621AE · Emb EMB145LR · Door Warning System
  > SUPPLEMENTAL INFORMATION - ERROR - UNIQUE CONTROL NUMBER CHANGE FROM HNAAA20211004733 TO HNAA2021100400473 PDIS 621 52-71 2482261 02OCT21 OAJ CLOSE BAG DOOR INDICATION ON TAKE OFF MEL 02OCT21 13:17 OAJ C27509 52-3-2 B
- [SDR HNAAA20211004733](https://openairdocs.org/sdr/HNAAA20211004733.md): None · none · Oct 2, 2021 · N621AE · Emb EMB145LR · Door Warning System
  > PDIS 621 52-71 2482261 02OCT21 OAJ CLOSE BAG DOOR INDICATION ON TAKE OFF MEL 02OCT21 13:17 OAJ C27509 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING FACT 03OCT21 01:28 SBY OPERATED BAG BAY DOOR NUMEROU
- [SDR HNAA2021061600264](https://openairdocs.org/sdr/HNAA2021061600264.md): Wire · broken · Jun 15, 2021 · N621AE · Emb EMB145LR · Light System Wiring
  > COCKPIT THRESHOLD STEP, EMERGENCY LIGHT SIGN IS INOP. REMOVED COCKPIT THRESHOLD PANEL, FOUND WIRE BROKEN AT QUICK DISCONNECT CONNECTOR, INSTALLED NEW CONTACT PIN AND MALE CONNECTOR ONTO WIRE, CONNECTED QUICK DISCONNECT CONNECTORS, OPS CHECKED LIGHTS, OPS CHECK
- [SDR HNAA2021010700007](https://openairdocs.org/sdr/HNAA2021010700007.md): Controller · failed · Jan 6, 2021 · N621AE · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > WINDSHIELD HEAT 1 FAIL MESSAGE ON EICAS. C/W FLT CREW PROCEDURES. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER, REFERENCE AMM 30-42-01-000-801-A AND 30-42-01-400-801-A. OPERATIONS CHECK GOOD. OK FOR SERVICE.
- [SDR HNAA2020123100382](https://openairdocs.org/sdr/HNAA2020123100382.md): Battery Pack · inoperative · Dec 29, 2020 · N621AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHT ABOVE FA SEAT DOES NOT TURN ON THE EXIT SIGN. R & R NR 100 EMERGENCY LIGHT SYSTEM BATTERY PACK, IAW AMM 33-50-04.
- [SDR HNAA2020123100381](https://openairdocs.org/sdr/HNAA2020123100381.md): Battery · not seated · Dec 29, 2020 · N621AE · Emb EMB145LR · Emergency Lighting
  > CABIN CEILING EMERGENCY EXIT AFT SIGN LIGHT DOES NOT TURN ON. RESET C/B NO FIX. REMOVED LT CABIN FLOOR PANEL 251JF TO ACCESS EMERGENCY BATTERY RESEATED NR 3 EMERGENCY BATTERY CANNON PLUG. OPERATIONS CHECK GOOD INSTALLED FLOOR PANEL 251JF USING RETAINED HARD
- [SDR HNAA2020121200351](https://openairdocs.org/sdr/HNAA2020121200351.md): Skin · deformed · Dec 5, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN DEFORMED BETWEEN FR 12A/13 STR 6R/7R. ACCOMPLISHED REPAIR OF FUSELAGE EXTERNAL SKIN AT UPPER AFT CORNER OF RT DV WINDOW BETWEEN FR 12A-13 STGR 6R-7R, IAW PIEDMONT EO1--53-20-0422.
- [SDR HNAA2020121200355](https://openairdocs.org/sdr/HNAA2020121200355.md): Skin · cracked · Dec 1, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77. ONE BETWEEN STRINGERS 3L-4L, AND ONE BETWEEN STRINGERS 4L-5L, AND ONE BETWEEN STRINGERS 6L-7L. FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77. ONE BETWEEN STRINGERS 3L-4L, AND ONE BETWEEN STRINGERS 4L-5L AND ONE
- [SDR HNAA2020121200353](https://openairdocs.org/sdr/HNAA2020121200353.md): Trunnion · cracked · Nov 13, 2020 · N621AE · Emb EMB145LR · Wing, Landing Gear Attach Fittings
  > LT MLG AFT UPPER TRUNNION HAS POSSIBLE CRACK IN RADIUS ABOVE FASTENER. PERFORMED HFEC INSPECTION ON AFT UPPER TRUNNION AND FOUND TO BE CRACKED, IAW EASI NDT MANUAL NR 6581 (400 KHZ H 60.6 V72.6 ANGLE 127 DEGREES). REMOVED AND INSTALLED SERVICEABLE LT AFT TRU
- [SDR HNAA2020121200352](https://openairdocs.org/sdr/HNAA2020121200352.md): Stringer · cracked · Nov 5, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 6R CRACKED AT FR 13. REMOVED AND INSTALLED SERVICEABLE STRINGER 6R AT FR 13, IAW EMB145 SRM 51-40-02 AND SRM 51-20-01.
- [SDR HNAA2020121100348](https://openairdocs.org/sdr/HNAA2020121100348.md): Floor Support · corroded · Nov 4, 2020 · N621AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > FWD DIGITAL IS CORRODED AROUND SCREW HOLE ON CENTEROMEGA BEAM BETWEEN FR 16-17. FABRICATED REPAIR DOUBLERS AND SHIMS, IAW EMB 145 SRM 53-21-10. INSTALLED REPLACEMENT DIGITAL SECTION REPAIR DOUBLER AND SHIM, IAW EMB 145 SRM 53--21-10 AND PIEDMONT EO1-05-20-0
- [SDR HNAA2020121100347](https://openairdocs.org/sdr/HNAA2020121100347.md): Door Sill · corroded · Nov 4, 2020 · N621AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SSI 53-20-10 SERVICE DOOR CENTER SILL IS CORRODED AROUND 3 SCREW HOLES. BLENDED CORROSION ON SERVICE DOOR CENTER SILL AROUND 3 SCREW HOLES, IAW EMB 145 SRM51-10-03. REMAINING THICKNESS AT CENTER AND AFT BLENDED AREAS ON SERVICE DOOR CENTER SILL FOUND TO BE W
- [SDR HNAA2020121100346](https://openairdocs.org/sdr/HNAA2020121100346.md): Door Sill · corroded · Nov 4, 2020 · N621AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SSI 53-30-48 CARGO DOOR LOWER SILL HAS CORROSION AND BARE METAL, MARKED. REMOVED CORROSION BY BLENDING, IAW EMB 145 SRM 51-10-03. PERFORMED HFEC INSPECTION AND UT THICKNESS, IAW EASI NDTM. NO RELEVANT INDICATION NOTED.055"-.074" MATERIAL REMAINING ET EASI
- [SDR HNAA202000346](https://openairdocs.org/sdr/HNAA202000346.md): Door Sill · corroded · Nov 4, 2020 · N621AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SSI 53-30-48 CARGO DOOR LOWER SILL HAS CORROSION AND BARE METAL, MARKED. REMOVED CORROSION BY BLENDING, IAW EMB 145 SRM 51-10-03. PERFORMED HFEC INSPECTION AND UT THICKNESS, IAW EASI NDTM. NO RELEVANT INDICATION NOTED,.055"-.074" MATERIAL REMAINING ET EASI
- [SDR HNAA2020121100345](https://openairdocs.org/sdr/HNAA2020121100345.md): Frame · cracked · Nov 4, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Frame
  > SSI 53-20-43, FRAME 25 IS CRACKED BETWEEN STRINGERS 15R AND 16R, MARKED. FABRICATED, PREPPED AND INSTALLED SERVICEABLE FR 25 LOWER RT FRAME SECTION INTERNAL SPLICE DOUBLER, IAW EMB 145 SRM 53-00-04, ITEM 4, FIGURE 201 AND EMB 145 SRM 51-20-03 AND 51--40-02 AN
- [SDR HNAA2020121100344](https://openairdocs.org/sdr/HNAA2020121100344.md): Bracket · cracked · Nov 3, 2020 · N621AE · Emb EMB145LR · Passenger/Crew Doors
  > MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET CRACKED, MARKED. REMOVED AND REPLACED MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET, IAW EMB 145 SRM 51-40-02. USED INCORRECT UNIQUE CONTROL NUMBER HNAA2020003444 SHOULD BE HNAA2020121100344.
- [SDR HNAA2020003444](https://openairdocs.org/sdr/HNAA2020003444.md): Bracket · cracked · Nov 3, 2020 · N621AE · Emb EMB145LR · Passenger/Crew Doors
  > MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET CRACKED, MARKED. REMOVED AND REPLACED MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020121100343](https://openairdocs.org/sdr/HNAA2020121100343.md): Structure · corroded · Nov 3, 2020 · N621AE · Emb EMB145LR · Passenger/Crew Doors
  > MAIN DOOR LOWER EDGE HAS CORROSION AROUND FOUR NUT PLATE HOLES, MARKED. ACCOMPLISHED REPAIR AT FWD NUTPLATE HOLE, IAW EMB 145 SRM 52-10-04 ITEM 3 FIGURE 201 SHEET 3 AND EO1-52-20-0426.
- [SDR HNAA2020121200354](https://openairdocs.org/sdr/HNAA2020121200354.md): Profile · corroded · Nov 2, 2020 · N621AE · Emb EMB145LR · Emergency Exits
  > LT EMERGENCY EXIT LOWER PROFILE L CORRODED UNDER TEFLON GUIDES. REMOVED AND INSTALLED SERVICEABLE LT EMERGENCY EXIT LOWER PROFILE LUNDER TEFLON GUIDES, IAW EMB 145 SRM 51--40-02 AND SRM 51-20-03.
- [SDR HNAA2020121100342](https://openairdocs.org/sdr/HNAA2020121100342.md): Skin · chafed · Nov 2, 2020 · N621AE · Emb EMB145LR · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL LOWER SKIN CHAFFED FWD OF ROD CLIP HOLDER, MARKED. REMOVED AND INSTALLED NEW CARGO DOOR INTERNAL SKIN, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020121100341](https://openairdocs.org/sdr/HNAA2020121100341.md): Spar · cracked · Nov 2, 2020 · N621AE · Emb EMB145LR · Wing Spar
  > LT WING SPAR 1 CRACKED AT SECOND SCREW HOLE OUTBOARD OF RIB 9, CRACK IS APPROXIMATELY 3/8" LONG, FROM FWD FLANGE EDGE TO SCREW HOLE. EASI NR 6581 USED, FREQ=400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. ACCOMPLISHED REPAIR OF LT WING SPAR I AT RIB 9, IAW EMB 14
- [SDR HNAA2020121100340](https://openairdocs.org/sdr/HNAA2020121100340.md): Profile · corroded · Nov 2, 2020 · N621AE · Emb EMB145LR · Emergency Exits
  > RT EMERGENCY EXIT LOWER PROFILE L CORRODED UNDER TEFLON GUIDES. REMOVED AND REPLACED RT EMERGENCY EXIT LOWER L-PROFILE, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020121100339](https://openairdocs.org/sdr/HNAA2020121100339.md): Spar · cracked · Nov 2, 2020 · N621AE · Emb EMB145LR · Wing Spar
  > RT WING SPAR 1 CRACKED ON LOWER FLANGE AT SCREW HOLE JUST OUTBOARD OF RIB 9. CRACK IS APPROXIMATELY 1/4 INCH, END IS MARKED. ACCOMPLISHED REPAIR OF RT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 2 AND EO-1-57-20-0412.
- [SDR HNAA2020121100338](https://openairdocs.org/sdr/HNAA2020121100338.md): Access Door · cracked · Nov 2, 2020 · N621AE · Emb EMB145LR · Fuselage Structure (General)
  > ACCESS HATCH 272DR UPPER BEAM CRACKED, MARKED. REMOVED AND REPLACED ACCESS HATCH 272DR UPPER BEAM, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020121200359](https://openairdocs.org/sdr/HNAA2020121200359.md): Skin · cracked · Nov 1, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77 BETWEEN STRINGERS 6R-7R. REPAIRED FUSELAGE EXTERNAL SKIN AT FRAME77 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM53-32-01 AND EO1-53-20-0423.
- [SDR HNAA2020121200358](https://openairdocs.org/sdr/HNAA2020121200358.md): Skin · cracked · Nov 1, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 6R-7R. FABRICATED AND INSTALLED SKIN BUSHING REPAIR AT FRAME 79 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0423.
- [SDR HNAA2020121200357](https://openairdocs.org/sdr/HNAA2020121200357.md): Skin · cracked · Nov 1, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 3L-4L. FABRICATED AND INSTALLED BUSHING RE-PAIR AT FRAME 79 BETWEEN STRINGERS 3L-4L, IAW EMB145 SRM 53-32-01-RE AND EO1-53-20-0424.
- [SDR HNAA2020121200356](https://openairdocs.org/sdr/HNAA2020121200356.md): Skin · cracked · Nov 1, 2020 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 78. ONE BETWEEN STRINGERS 4L-5L, AND ONE BETWEEN STRINGERS 6L-7L. FABRICATE AND INSTALLED SKIN BUSHING REPAIR AT FRAME 78 BETWEEN STRINGERS 6L-7L, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0424, NO RELEVANT INDICATI
- [SDR HNAA2020121100337](https://openairdocs.org/sdr/HNAA2020121100337.md): Drag Angle · cracked · Nov 1, 2020 · N621AE · Emb EMB145LR · Vertical Stabilizer
  > RT DRAG ANGLE BETWEEN VERTICAL STAB AND FUSELAGE IS CRACKED AT FRAME 76 STRINGER 3R. REMOVED AND REPLACED VERTICAL STAB DRAG ANGLE TO FUSELAGE AT FR 76 STRG 3R AND REINSTALLED PREVIOUS REPAIR, IAW EMB 145 SRM 51-40-02.
- [SDR HNAA2020103000292](https://openairdocs.org/sdr/HNAA2020103000292.md): Roller · seized · Oct 29, 2020 · N621AE · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle
  > ON TAKEOFF, EICAS SHOWED LG AIR GROUND FAIL. COUPLED WITH LOUD BANG ON NLG EXTENSION: MAINTENANCE: TESTED ALL WOW PROX SWITCHES, IAW AMM 32 63 05. ALL TESTED GOOD. FOUND NOSE UP LOCK ROLLER SEIZED DUE TO PRC. REMOVED PART OF THE PRC AS REQ. NO OTHER DEFEC
- [SDR HNAA2020101200285](https://openairdocs.org/sdr/HNAA2020101200285.md): Battery Pack · inoperative · Oct 7, 2020 · N621AE · Emb EMB145LR · Emergency Lighting
  > NDIS 621 33-50 0025060 07OCT20 RIC CLOSE. EMERGENCY LIGHTS AT 13A THRU 18A, LT EXTERNAL EMERGENCY LIGHTS, MAIN SERVICE DOOR EMERGENCY LIGHTS AND CABIN CEILING EMERGENCY EXIT MARKER WILL NOT ILLUMINATE. 37208 00 NGR FACT 07OCT20 07:47 RIC. R & R BATTERY POW
- [SDR HNAA2020091700255](https://openairdocs.org/sdr/HNAA2020091700255.md): Inverter · inoperative · Sep 16, 2020 · N621AE · Emb EMB145LR · Emergency Lighting
  > CABIN FLOOR EMERGENCY STRIPS INOPERABLE REAR OF CABIN. R & R NR 6 EMERGENCY LIGHT DC/AC/INVERTER IN REF TO AMM 33-50-11-000/400-801-A. OPT CHECK GOOD, OK FOR SERVICE.
- [SDR HNAA201910160001](https://openairdocs.org/sdr/HNAA201910160001.md): Sign · inoperative · Oct 15, 2019 · N621AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE FAS SEAT INOPERATIVE. R&RD EXIT SIGN.
- [SDR HNAA2019042200115](https://openairdocs.org/sdr/HNAA2019042200115.md): Connector · not seated · Apr 21, 2019 · N621AE · Emb EMB145LR · Light System Wiring
  > NDIS 621 33-51 0012890 21APR19 RIC CLOSE EMERGENCY LIGHT ABOVE F/A SEAT INOP 28805 00 BSH FACT 21APR19 09:11 RIC RESEATED EMERGENCY LIGHT ABOVE F/A SEAT
- [SDR HNAA2019030100052](https://openairdocs.org/sdr/HNAA2019030100052.md): Unknown · malfunctioned · Mar 1, 2019 · N621AE · Emb EMB145LR · Landing Gear Retraction/Extension System
  > AFTER SELECTING GEAR UP. NOSE GEAR MADE THUMPING NOISE AND NOSE GEAR INDICATION ALTERNATED AMBER TO UP FOR FOR 8 MINS. CREW PERFORMED ALTERNATE EXTENSION, GEAR EXTENDED NORMALLY. INSPECTED NOSE LANDING GEAR FOR OBVIOUS DEFECTS NONE NOTED ON RELAY MSG ON CMC CH
- [SDR HNAA2019010400006](https://openairdocs.org/sdr/HNAA2019010400006.md): Skin · corroded · Dec 24, 2018 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > NDIS 621 53-30 0009070 03JAN19 SBY CLOSE FOUND CORROSION AT F24 & STR. 194. DOESNOT EXTEND OUT OF CHEM MILLED AREA. (SEE SEQ. 4 FOR DETAILS) FACT 03JAN19 12:46 SBY REMOVED ATTACHMETN RIVETS FROM STRINGER 19R AND REMOVED FRAME LEGS OF FR24 & 25 AT STR 19R. INST
- [SDR HNAA2019010400005](https://openairdocs.org/sdr/HNAA2019010400005.md): Rivet · missing · Dec 24, 2018 · N621AE · Emb EMB145LR · Fuselage Main, Plate/Skin
  > NDIS 621 53-30 0009060 03JAN19 SBY CLOSE FOUND 1 RIVET MISSING & 1 RIVET POPPED AT F24 XSTR 19R. FACT 03JAN19 12:34 SBY REMOVED ATTACDHMENT RIVETS FROM STRINGER 19R AND REMOVED FRAME LEGS OF FR 24 & 25 AT STR 19R. INSTALLED FRAME LEGS FOR FR24 & 25 AND SKIN RI
- [SDR HNAA2018122600329](https://openairdocs.org/sdr/HNAA2018122600329.md): Sign · inoperative · Dec 24, 2018 · N621AE · Emb EMB145LR · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE FWD FA'S SEAT INOP. RESET EMERGENCY LIGHT C/B, OPS CHECK FOR EMERGENCY SIGN ABOVE FWD F/A'S SEAT IS GOOD.
- [SDR HNAA2018081300196](https://openairdocs.org/sdr/HNAA2018081300196.md): Autopilot Sys · malfunctioned · Aug 12, 2018 · N621AE · Emb EMB145LR · Autopilot System
  > ACFT DID A UNCOMMANDED HARD RIGHT TURN WITH AUTOPILOT ENGAGED. PILOT COMPLIED WITH AN IMMEDIATE EMERGENCY ACTION ITEMS WITH AUTO PILOT FAIL ON EICAS AND AUTO RED AP ON FLIGHT MODE ANNUNCIATOR ON PFD. COMPLIED WITH MX PROCEDURE. COULD NOT DUPLICATE THE DISCR
- [SDR HNAA2018072600172](https://openairdocs.org/sdr/HNAA2018072600172.md): Warning System · false activation · Jul 24, 2018 · N621AE · Emb EMB145LR · Cabin Pressure Control System
  > CABIN ALTITUDE ALERT MSG AT 14,000. REACTIVATED PRESSURIZATION SYS OUTFLOW VALVES IAW MM 21-31-03-440-801-A AND 21-31-04-440-801-A. OPS CHECKED PRESSURIZATION WITH BOTH PACKS IAW MM 21-31-00-700-801-A, NO DEFFECTS NOTED.
- [SDR RAIA2018041900003](https://openairdocs.org/sdr/RAIA2018041900003.md): Door Sill · corroded · Mar 8, 2018 · N621AE · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL IS CORRODED. R & R THE CARGO DOOR LOWER SILL.
- [SDR RAIA201803080002](https://openairdocs.org/sdr/RAIA201803080002.md): Shear Tie · corroded · Mar 8, 2018 · N621AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 68, SHEAR TIE WAS FOUND CORRODED. REPAIRED THE SHEAR TIE.
- [SDR RAIA201803080001](https://openairdocs.org/sdr/RAIA201803080001.md): Shear Tie · corroded · Mar 8, 2018 · N621AE · Emb EMB145LR · Fuselage Internal Mounting Structure
  > FRAME 65, SHEAR TIE IS CORRODED. R & R THE SHEAR TIE.
- [SDR RAIA201803013001](https://openairdocs.org/sdr/RAIA201803013001.md): Door Frame · dented · Mar 6, 2018 · N621AE · Emb EMB145LR · Fuselage Main, Structure
  > CARGO DOOR LOWER FRAME PROFILE IS DENTED. R & R CARGO DOOR LOWER FRAME PROFILE.
- [SDR RAIA201803050002](https://openairdocs.org/sdr/RAIA201803050002.md): Skin · dented · Mar 5, 2018 · N621AE · Emb EMB145LR · Passenger/Crew Doors
  > PAX DOOR LOWER CENTER EXTERIOR SKIN, 6 INCHES FROM BOTTOM HAS 2 DENTS. REPAIRED THE DOOR SKIN.
- [SDR RAIA201801260001](https://openairdocs.org/sdr/RAIA201801260001.md): Handle · broken · Jan 26, 2018 · N621AE · Emb EMB145LR · Passenger/Crew Doors
  > MAIN PAX DOOR EXTERNAL HANDLE BROKEN. REPLACED THE HANDLE. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N621AE/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 = 'N621AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N621AE/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.