# Service difficulty reports: N620DL

A list on [N620DL](https://openairdocs.org/aircraft/N620DL.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 · 107 reports

- [SDR IXXA20190401002](https://openairdocs.org/sdr/IXXA20190401002.md): Gcu · unsecure · Mar 16, 2019 · N620DL · Boeing 757232 · AC Generator-Alternator
  > FLIGHT DEPARTED, ENROUTE ON INITIAL CLIMB, PILOT REPORTED A LOSS OF CAPTAIN EFIS DISPLAY, TOP EICAS DISPLAY, AND LEFT FLIGHT MANAGEMENT COMPUTER SYSTEM. FORWARD EQUIPMENT OVERHEAT INDICATION. LOSS OF FLAP AND BRAKE PRESSURE INDICATIONS. LEFT AND CENTER IN
- [SDR IXXA20180621029](https://openairdocs.org/sdr/IXXA20180621029.md): Stringer · corroded · Jun 11, 2018 · N620DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L WAS CORRODED, BS 1455. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, AND REA 46971REA64.
- [SDR IXXA20180621028](https://openairdocs.org/sdr/IXXA20180621028.md): Stringer · corroded · Jun 11, 2018 · N620DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > BS 1455, STRINGER 28L WAS CORRODED. REMOVED AND REPALCED THE STRINGER IAW SRM 53-00-003, FIG 201, AND REA 46971REA64,
- [SDR IXXA20161213198](https://openairdocs.org/sdr/IXXA20161213198.md): Floorbeam · corroded · Nov 30, 2016 · N620DL · Boeing 757232 · Fuselage Main, Floor Beam
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FLOORBEAM LOWER HORIZONTAL FLANGE CORRODED AT STATION 740 LBL 18. REPAIR LOWER CHORD STATION 740 LBL 18 IN ACCORDANCE WITH SRM 53-00-51.
- [SDR IXXA20161213197](https://openairdocs.org/sdr/IXXA20161213197.md): Web · cracked · Nov 18, 2016 · N620DL · Boeing 757232 · Leading Edge Devices
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 SLAT AFT SIDE COVE STRUCTURE HAS 2 CRACKS, LOCATED ABOVE THE INBOARD MAIN TRACK FITTING. ONE CRACK IS ABOUT 2 1/4" AND THE OTHER IS ABOUT 1 3/8" IN LENGTH, AT APPROXIMATELY OUTBOARD SLAT STATION 737. REMOVED AND RE
- [SDR IXXA20161213196](https://openairdocs.org/sdr/IXXA20161213196.md): Web · cracked · Nov 18, 2016 · N620DL · Boeing 757232 · Leading Edge Devices
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 SLAT AFT SIDE COVE STRUCTURE HAS 2 CRACKS, LOCATED ABOVE THE INBOARD MAIN TRACK FITTING. ONE CRACK IS ABOUT 2 1/4" AND THE OTHER IS ABOUT 1 3/8" IN LENGTH, AT APPROXIMATELY OUTBOARD SLAT STATION 737. REMOVED AND RE
- [SDR IXXA20161213195](https://openairdocs.org/sdr/IXXA20161213195.md): Attach Bracket · cracked · Nov 10, 2016 · N620DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NUMBER 1 PYLON, LINK AT FORWARD LEFT SIDE OF HYDRAULIC BAY, LOWER ATTACH BRACKET BROKEN.
- [SDR IXXA20150723083](https://openairdocs.org/sdr/IXXA20150723083.md): Battery Pack · inoperative · Jul 21, 2015 · N620DL · Boeing 757232 · Emergency Lighting
  > DURING THE COURSE OF DAILY CHECK, EMERGENCY EXIT LIGHTING FOUND TO BE INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECKED SATISFACTORY. ACFT RELEASED TO SERVICE.
- [SDR IXXA20150518080](https://openairdocs.org/sdr/IXXA20150518080.md): Rod · bent · May 17, 2015 · N620DL · Boeing 757232 · Passenger/Crew Doors
  > L1 ENTRY DOOR ROLLERS DO NOT ALWAYS ENGAGE, UPPER LOCK ROD BENT. R & R UPPER ROD IAW AMM 52-12-00. OPERATIONAL CHECKED SATISFACTORY. ACFT RELEASED TO SERVICE.
- [SDR IXXA20141231038](https://openairdocs.org/sdr/IXXA20141231038.md): Engine · making metal · Dec 31, 2014 · N620DL · Boeing 757232 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT AT FL300, RT ENG OIL PRESS DROPPED INTO RED FOLLOWED BY EICAS MSG. PRECAUTIONARY SHUTDOWN OF NR 2 ENG. ACFT RETURNED, GNDED NO OPS. CHIP DETECTORS PULLED. MASTER CHIP DETECTOR & MAIN GEARBOX CHIP DETECTOR WERE CONTAMINATED WITH CHIPS. DET
- [SDR IXXA20141001023](https://openairdocs.org/sdr/IXXA20141001023.md): Valve · defective · Sep 29, 2014 · N620DL · Boeing 757232 · Cargo/Baggage Doors
  > MAIN CARGO DOOR WARNING LIGHT DISPLAYED & CABIN PRESS NOT WITHIN PARAMETERS. CREW NOTED PRESSURIZATION AS DECREASING. BITE CHECK OF BOTH CABIN PRESS CONTROLLERS ACCOMPLISHED IAW FIM 21-30 FT 802. SYSTEMS CHECKED SATISFACTORY, NO FAULTS NOTED. HOLDING VLV AS
- [SDR IXXA20140829019](https://openairdocs.org/sdr/IXXA20140829019.md): Metering Unit · malfunctioned · Aug 29, 2014 · N620DL · Boeing 757232 · Master Cylinder/Brake Valve
  > DURING THE TAKE OFF, BEFORE COMPLETE RETRACTION OF THE FLAPS, EICAS MESSAGE DISPLAYED "L HYD PRESSURE" FOLLOWED BY FURTHER MESSAGES INDICATING A LEFT HYDRAULIC SYS PRESS. UPON EVALUATION OF SYSTEM FAULT WAS ISOLATED TO A SEPERATION OF AUTOBRAKE ACTUATOR FROM B
- [SDR IXXA20140814015](https://openairdocs.org/sdr/IXXA20140814015.md): Module · defective · Aug 14, 2014 · N620DL · Boeing 757232 · Emergency Lighting
  > ON DAILY CHECK FOUND EMER LIGHT UNARMED. ANNUNCIATOR LIGHT INTERMITTENT. EMER LIGHT ANNUNCIATOR LIGHT LENS CAP MODULE R & R IAW AMM 33-16-02 201. OPERATIONAL CHECKED SATISFACTORY.
- [SDR IXXA201306120002](https://openairdocs.org/sdr/IXXA201306120002.md): Skin Panel · corroded · May 13, 2013 · N620DL · Boeing 757232 · Wing, Plate/Skin
  > CORROSION WAS DISCOVERED ON THE RT WING UPPER SKIN PANEL AT FSS404 FWD OF FRONT SPAR. REMOVED CORROSION IAW SRM 57-20-01. PERFORMED HFEC INSP OF BLENDED AREA IAW NDT MANUAL 51-00-19. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER FROM.071" 7075-T6 AND INSTAL
- [SDR IXXA20130612001](https://openairdocs.org/sdr/IXXA20130612001.md): Skin Panel · corroded · May 13, 2013 · N620DL · Boeing 7572Y0 · Wing, Plate/Skin
  > CORROSION WAS DISCOVERED ON THE RT WING UPPER SKIN PANEL AT WS285.65. DAMAGE IS LOCATED NEAR THE AFT EDGE OF THE SKIN PANEL BETWEEN THE REAR SPAR AND STRINGER S-1. REMOVED CORROSION IAW SRM 57-20-01. PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDT MANUAL 5
- [SDR IXXA20130612032](https://openairdocs.org/sdr/IXXA20130612032.md): Seat Track · cracked · May 12, 2013 · N620DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS AFT OTBD SEAT TRACK IS CRACKED AT THE AFT STOP. R & R THE CAPTAINS AFT OTBD SEAT TRACK IAW AMM 25-11-01.
- [SDR IXXA201306120007](https://openairdocs.org/sdr/IXXA201306120007.md): Stanchion · corroded · May 12, 2013 · N620DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > LOWER SECTION OF STANCHION AT BS 1440, RBL 19 CORRODED. FABRICATED STANCHION IAW DWG 284N1695 USING EXTRUSION AND 10140-2002 7075-T6511. RT STANCHION IAW DWG 284N1695.
- [SDR IXXA201306120006](https://openairdocs.org/sdr/IXXA201306120006.md): Floor Support · corroded · May 12, 2013 · N620DL · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED ON THE UPPER CARGO FLOOR SUPPORT BS 1075, LBL 47, FLOOR AREA INBD SURFACE. BLENDED AREA OF CORROSION IAW SRM 53-00-52. PERFORMED ULTRASONIC INSPECTION OF AREA IAW NDT MM PART 4, 51-00-10. MATERIAL REMOVED IS OUT OF LIMITS. FABRICATE
- [SDR IXXA201306120005](https://openairdocs.org/sdr/IXXA201306120005.md): Seat Track · corroded · May 12, 2013 · N620DL · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS DISCOVERED ON THE UPPER CARGO SEAT TRACK UPPER CHORD AT STATION 1180-1580, RBL 24. DAMAGE CAUSED BY CORROSION IN SEVERAL AREAS ALONG THE UPPER SURFACE WERE FOUND TO BE BEYOND ALLOWABLE AND REPAIRABLE LIMITATIONS. FABRICATED NEW SEAT TRACK SECTI
- [SDR IXXA201306120004](https://openairdocs.org/sdr/IXXA201306120004.md): Sill · corroded · May 12, 2013 · N620DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > INNER CHORD OF AFT LOWER CARGO DOOR LOWER SILL CORRODED. THE DAMAGE WAS ISOLATED TO THE LOWER HORIZONTAL FLANGE OF THE CHORD SPANNING FROM STATION 1340 - 1440 AT S27R. CORROSION WAS REMOVED IAW SRM 53-60-15, FIG 101, EXCEEDING PUBLISHED LIMITS. A HFEC OPE
- [SDR IXXA201306120003](https://openairdocs.org/sdr/IXXA201306120003.md): Skin · corroded · May 12, 2013 · N620DL · Boeing 7572Y0 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN CORRODED AT AFT LOWER CARGO DOOR CUTOUT THRESHOLD AT STATION 1401 S27R - S28R. CORROSION WAS REMOVED IAW SRM 53-00-01, FIG 101, EXCEEDING PUBLISHED LIMITS. THE DAMAGED SKIN WAS TRIMMED OUT AND A FILLER WAS FABRICATED. A HFEC OPEN HOL
- [SDR IXXA130512ILN025S](https://openairdocs.org/sdr/IXXA130512ILN025S.md): Cargo Track · broken · May 12, 2013 · N620DL · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO TRACK AT BS 1100, RBL 24 IS BROKE OUT ON UPPER FLANGE AT NUTPLATE. ALSO 3 AREAS OF POSSIBLE CRACKS. REMOVED SEAT TRACK CROWN AT BS 1100 RBL 24 FOR REPLACEMENT. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK IAW SRM 51-40-02.
- [SDR IXXA130512ILN022S](https://openairdocs.org/sdr/IXXA130512ILN022S.md): Support Angle · cracked · May 12, 2013 · N620DL · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE CRACKED AT FORWARD LOWER CARGO FWD DOOR FRAME JUST INBD OF THE THIRD DOOR STOP DOWN AT BS 560. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE. HEAT TREATED ANGLE IAW 5602, REV AF 28 DATED AUG 2001. TREATED, PRIMED AND PAINTED ANGLE IAW SRM 51-
- [SDR IXXA20130613033](https://openairdocs.org/sdr/IXXA20130613033.md): Skin · corroded · May 1, 2013 · N620DL · Boeing 757232 · Wing, Plate/Skin
  > RT WING REAR SPAR AT WBL 95 HAS CORROSION ON WING SKIN. REMOVED CORROSION FROM WING SKIN IAW SRM 57-20-01. PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDT MANUAL 51-00-19. NO DEFECTS NOTED. PERFORMED THICKNESS CHECK OF BLENDED AREA IAW NDT MANUAL 51-00-1
- [SDR IXXA20130612031](https://openairdocs.org/sdr/IXXA20130612031.md): Frame · corroded · Apr 25, 2013 · N620DL · Boeing 757232 · Fuselage Main, Frame
  > CORROSION WAS FOUND IN THE AFT LOWER CARGO COMPARTMENT, ON THE FWD SIDE OF THE FRAME AT BS 1480 BETWEEN S26-27R. BLENDED AREA OF CORROSION IAW SRM 53-00-07, FIG 101. COMPLIED WITH HFEC SURFACE SCAN IAW NDT MM 51-00-19, PART 6. NO DEFECTS NOTED. FABRICATED
- [SDR FOTR3519821257](https://openairdocs.org/sdr/FOTR3519821257.md): Skin · debonded · Jan 5, 2012 · N620DL · Boeing 757232 · Wing, Plate/Skin
  > LT WING FIXED L/E UPPER SURFACE IS DISBONDED WS 231.0, REPAIRED BY REMOVED DAMAGE, CLEAN AND PREPPED LT WING FIXED L/E UPPER SURFACE, APPLIED REPAIR 23" X 18" AND RESTORED FINISH IAW SRM 51-70-07.
- [SDR C8GA201111150026](https://openairdocs.org/sdr/C8GA201111150026.md): Warning Light · false activation · Nov 15, 2011 · N620DL · Boeing 757232 · Central Warning
  > DURING TAKEOFF, SPOILER CAUTION LIGHT ILLUMINATED WITH THE TAKEOFF WARNING HORN AND THE SPOILER EICAS MESSAGE DISPLAYED. ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION PERFORMED. CONDUCTED CONFIGURATION TAKE OFF TEST, UNABLE TO DUPLIC
- [SDR C8GA2011000010](https://openairdocs.org/sdr/C8GA2011000010.md): Pitot Tube · obstructed · Jul 5, 2011 · N620DL · Boeing 757232 · Airspeed/Mach Indicator
  > DURING TAKEOFF ROLL IT WAS NOTED THAT THERE WAS NO AIRSPEED INDICATION ON THE CAPTAINS SIDE. THE TAKEOFF WAS ABORTED WITH LIGHT BRAKING. ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE CAPTAINS PITOT TUBE WAS
- [SDR C8GA2011000002A](https://openairdocs.org/sdr/C8GA2011000002A.md): Control Valve · inoperative · Mar 30, 2011 · N620DL · Boeing 757232 · Cabin Cooling System
  > DURING CRUISE OPERATION AN EICAS MESSAGE APPEARED " R PACK OFF" & R ENG BLEED OFF" MESSAGES APPEARED. THE ACFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND WAS RELEASED TO SERVICE, FURTHER INVESTIGATION LEAD TO THE REMOVAL AND
- [SDR C8GA201000058](https://openairdocs.org/sdr/C8GA201000058.md): Unknown · unknown · Oct 24, 2010 · N620DL · Boeing 757232 · Auto Flight System
  > DURING TAKEOFF ROLL WITH THROTTLES ADVANCED AND EPR CALLED, THE THROTTLERS DID NOT ENGAGE FOR TAKEOFF. THE TAKEOFF WAS ABORTED. POST FLIGHT INSP WAS PERFORMED WITH NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR ABXR201006272010](https://openairdocs.org/sdr/ABXR201006272010.md): Flap Track · corroded · Jun 27, 2010 · N620DL · Boeing 757232 · Trailing Edge Flaps
  > DURING MX, THE LEFT OTBD FLAP, OTBD TRACK WAS BLEEDING RUST. UPON DISASSEMBLY, THE TRACK WAS FOUNDED CORRODED. THE CORROSION WENT BEYOND THE CMM LIMITS. MFG ENGINEERING ISSUED AN REA TO FURTHER CLEAN THE CORROSION WITH ADDITIONAL LIMITS ESTABLISHED. THE CORRO
- [SDR ABXR201006270020](https://openairdocs.org/sdr/ABXR201006270020.md): Skin · delaminated · Jun 26, 2010 · N620DL · Boeing 757232 · Leading Edge Devices
  > DURING MX, THE BOTTOM WEDGE OF THE NR 10 SLAT WAS FOUND DELAMINATED ON INBD END. REPAIRED DELAMINATED AREA IAW THE SRM. REPAIR FOUND TO COMPLY WITH SB 757-57A0038, REV 6. ITEM RETURNED TO SERVICE.
- [SDR ABXR201006270019](https://openairdocs.org/sdr/ABXR201006270019.md): Intercostal · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > DURING MX, INTERCOSTAL BETWEEN S29L-S30L STA 1400-1420 FOUND CORRODED. CORROSION OUTSIDE OF SRM LIMITS. REMOVED AND FABRICATED NEW INTERCOSTAL WITH 7075 T-6 0.032". REINSTALLED INTERCOSTAL IAW THE SRM. ITEM RETURNED TO SERVICE.
- [SDR ABXR201006270018](https://openairdocs.org/sdr/ABXR201006270018.md): Frame · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Ailerons
  > DURING MX, THE LT WING AILERON WAS FOUND DELAMINATED. REMOVED CONDUCTIVE FRAME. FABRICATED NEW FRAME FROM 6061 T4 0.020" AND INSTALLED FRAME IAW THE SRM. REMOVED FIBERGLASS ISOLATION PLY, NO FURTHER DAMAGE NOTED. REPLACED ISOLATION PLY. PREPPED AND PAINTED A
- [SDR ABXR201006270017](https://openairdocs.org/sdr/ABXR201006270017.md): Floorbeam · cracked · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Main, Floor Beam
  > DURING MX, A FLOOR SUPPORT LBL 46-LBL 62 BS 1060 FOUND CRACKED. ISSUED FOR FABRICATION INSTRUCTIONS. FABRICATED THE CRACKED FLOOR SUPPORT/INTERCOSTAL FROM 7075-0 0.050" HAND HEAT TREATED. REINSTALLED INTERCOSTAL AND ITEM RETURNED TO SERVICE.
- [SDR ABXR201006270016](https://openairdocs.org/sdr/ABXR201006270016.md): Support Fitting · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > DURING MX, CORROSION WAS FOUND ON A SEAT TRACK SUPPORT FITTING (CHORD). CORROSION WAS FOUND OUT OF SRM LIMITS. ISSUED WITH GREATER CLEANUP ALLOWED. ITEM RETURNED TO SERVICE.
- [SDR ABXR201006270015](https://openairdocs.org/sdr/ABXR201006270015.md): Attach Fitting · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > DURING MX, CORROSION WAS FOUND ON A FLOOR PANEL ATTACH CHORD ADJACENT TO NUTPLATES. THE CORROSION WAS BEYOND MFG LIMITS AND THE DAMAGE CHORD REMOVED. FABRICATED NEW CHORD FROM EXTRUSION BAC 1506-1108 EXTRUSION. INSTALLED THE NEW CHORD SECTION IAW THE SRM. ITEM
- [SDR ABXR201006270014](https://openairdocs.org/sdr/ABXR201006270014.md): Frame · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Main, Frame
  > DURING MX, CORROSION WAS FOUND ON THE FLC AFT BULKHEAD LOWER CTR FRAME. CUTOUT CORROSION DAMAGE AND REPAIRED DAMAGE IAW THE SRM USING 7075 T6 0.050" AND 7075-T6 0.063". ITEM RETURNED TO SERVICE.
- [SDR ABXR201006270013](https://openairdocs.org/sdr/ABXR201006270013.md): Floor Support · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE INSPECTION EVENT, CORROSION WAS FOUND ON A FLOOR SUPPORT ANGLE AT FS 780 BL0. THE CORROSION WAS FOUND BEYOND LIMITS. FABRICATED A NEW SUPPORT ANGLE FROM 7075-0, 0.063". HEAT TREATED ANGLED. CORROSION TREATED ANGLE AND REINSTALLED. ITEM RET
- [SDR ABXR201006270012](https://openairdocs.org/sdr/ABXR201006270012.md): Floor Support · corroded · Jun 26, 2010 · N620DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > DURING A MX, CORROSION WAS FOUND ON A FLOOR SUPPORT ANGLE AT FS 780 LBL 6. THE CORROSION WAS FOUND BEYOND LIMITS. FABRICATED A NEW SUPPORT ANGLE FROM 7075-0, 0.063". HEAT TREATED ANGLED. CORROSION TREATED ANGLE AND REINSTALLED. ITEM RETURNED TO SERVICE.
- [SDR ABXR201006220005](https://openairdocs.org/sdr/ABXR201006220005.md): Skin · corroded · Jun 22, 2010 · N620DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING A HEAVY MX INSP EVENT, THE FUSELAGE SKIN WAS FOUND BULGED AT STA 1460 BETWEEN STRINGERS 27L & 30L. DEFECT WAS FOUND TO BE CORROSION ON THE STRINGERS AND INTERCOSTAL. R & R STRINGERS, FABRICATED INTERCOSTAL AND INSTALLED IAW SRM. ITEM WAS RETURNED TO SER
- [SDR ABXR201006210004](https://openairdocs.org/sdr/ABXR201006210004.md): Stringer · corroded · Jun 21, 2010 · N620DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > DURING A HEAVY MX INSP EVENT THE FUSELAGE SKIN WAS BULGED AT STATION 1466, STRINGER 29L. DEFECT WAS FOUND TO BE CORROSION OF THE STRINGER AND INTERCOSTAL BETWEEN STA 1400 AND STA 1420. R & R STRINGER, FABRICATED INTERCOSTAL AND INSTALLED. ITEM WAS RETURNED TO
- [SDR ABXR20100621005](https://openairdocs.org/sdr/ABXR20100621005.md): Skin · corroded · Jun 21, 2010 · N620DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING A HEAVY MX INSP EVENT CORROSION BETWEEN STR 29L AND THE FUSELAGE SKIN AT STA 1467. THE UNDERLYING SKIN WAS ALSO CORRODED RESULTING IN A 2.4"LONG X 1.0" WIDE CUT OUT LOCATED AT STA 1467, S29L. AN ADDITIONAL SKIN CUT OUT WAS REQUIRED AT STA 1484, S29L TH
- [SDR C8GA20090195](https://openairdocs.org/sdr/C8GA20090195.md): Shutoff Valve · malfunctioned · Sep 3, 2009 · N620DL · Boeing 757232 · Pneumatic Distribution System
  > FLT 165 FROM MIA TO TOL WHILE CLIMBING THROUGH FL340 EICAS MSG "L" ENGINE BLEED OFF CAUTION APPEARED. WHILE PERFORMING APPROPRIATE PROCEDURES THE EICAS "R" ENGINE BLEED OFF CAUTION LIGHT APPEARED. APPROPRIATE PROCEDURES WERE PERFORMED AND AN EMERGENCY WAS DECL
- [SDR C8GA20090177](https://openairdocs.org/sdr/C8GA20090177.md): Bleed Valve · cracked · Aug 10, 2009 · N620DL · Boeing 757232 · Compressor Bleed Valve
  > DURING CLIMB OUT THE NR 2 ENG EXCEEDED THE EGT LIMIT OF 657 DEG FOR 16 SEC THIS DID NOT OCCUR DURING A SURGE. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. THE 14TH STAGE BLEED VALVE WAS REMOVED AND REPLACED PN 5
- [SDR DL757090865](https://openairdocs.org/sdr/DL757090865.md): Acoustic Panel · delaminated · May 15, 2009 · N620DL · Boeing 757232 · Engine Cowling System
  > DURING SHOP VISIT, LARGE DELAMINATIONS WERE FOUND ON THE PN 314N3011-170, ENGINE INLET ACOUSTIC PANEL, REQUIRING REPLACEMENT OF THE DELAMINATED SKINS. REPAIRED IAW ERA 474812-14.
- [SDR C8GA20080032](https://openairdocs.org/sdr/C8GA20080032.md): Engine · damaged · Nov 20, 2008 · N620DL · Boeing 757232 · Engine (Turbine/Turboprop)
  > FLT 201 FROM MIA TO CCS - AFTER TAKEOFF WITH FLAPS RAISED APPROX 1800 FEET AND CLIMB THRUST SELECTED, 3 QUICK COMPRESSOR STALLS WERE HEARD AND FELT FROM THE NR 1 ENGINE. APPROPRIATE CHECKLIST WAS PERFORMED, EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO
- [SDR C8G2008F00007](https://openairdocs.org/sdr/C8G2008F00007.md): Door · out of adjust · Jun 20, 2008 · N620DL · Boeing 757232 · Passenger/Crew Doors
  > DURING CLIMB OPERATION THE FWD ENTRY DOOR EICAS MESSAGE APPEARED WITH THE ASSOCIATED OVERHEAD LIGHT. THE ACFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE FWD ENTRY DOOR WAS NOT CENTERED IN THE DOOR FRAME WHEN CLOSED. THE FW
- [SDR C8G2008F00004](https://openairdocs.org/sdr/C8G2008F00004.md): Hinge · damaged · Jun 20, 2008 · N620DL · Boeing 757232 · Fuselage, Door Hinge
  > DURING CLIMB OPERATION THE FWD ENTRY DOOR EICAS MESSAGE APPEARED WITH THE ASSOCIATED OVERHEAD LIGHT. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE FWD ENTRY DOOR WAS NOT CENTERED IN THE DOOR FRAME WHE
- [SDR C8GA20080017](https://openairdocs.org/sdr/C8GA20080017.md): Eec · malfunctioned · Jun 4, 2008 · N620DL · Boeing 757232 · Fuel Controlling System
  > FLT P0002 FROM PTY TO MFA. DURING CLIMB OPERATION OIL PSI WENT TO -4, N1=0, N2=0 ENG SHUTDOWN. ACFT RETURNED TO PTY WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND EEC TO BE AT FAULT. REMOVED AND REPLACED EEC, OPS CHECKS GOOD. NO FURTHER DE

Next page: https://openairdocs.org/aircraft/N620DL/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 = 'N620DL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N620DL/reports

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