# Service difficulty reports: N610DL, cancelled Feb 12, 2019

A list on [N610DL, cancelled Feb 12, 2019](https://openairdocs.org/deregistered/N610DL-2019-02-12.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 DALA2014110605970](https://openairdocs.org/sdr/DALA2014110605970.md): Cover · damaged · Nov 2, 2014 · N610DL · Boeing 757232 · Service Doors
  > AFT RT R4 BUSTLE DAMAGED. REPLACED BUSTLE COVER.
- [SDR DALA2014081104411](https://openairdocs.org/sdr/DALA2014081104411.md): Warning Message · false activation · Aug 9, 2014 · N610DL · Boeing 757232 · Fire Detection
  > LT ENGINE FIRE EICAS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED ENGINE FIRE AND OVERHEAT DETECTION SYSTEM BITE IAW MM 26-11. BITE TESTED GOOD.
- [SDR DALA14014260610](https://openairdocs.org/sdr/DALA14014260610.md): Doubler · cracked · Mar 1, 2014 · N610DL · Boeing 757232 · Auxiliary Power Unit (APU) Doors
  > RIGHT APU COMPARTMENT DOOR 316AR REPAIR DOUBLER AT THE MIDDLE CLOSE LATCH HAS TWO CRACKS AT CUTOUT. REMOVED CRACKS AS REQUIRED. NDT ACCOMPLISHED-NO DEFECTS FOUND. ACCOMPLISHED REDIAL AS REQUIRED.
- [SDR DALA14014250610](https://openairdocs.org/sdr/DALA14014250610.md): Skin · damaged · Mar 1, 2014 · N610DL · Boeing 757232 · Electrical/Electronic Compartment Doors
  > LOWER EXTERIOR FUSELAGE, E & E COMPARTMENT DOOR EXTERIOR SKIN HAS A DENT WITH GOUGE IN CENTER. BLEENDED SKIN OF E/E DOOR IAW SRM B757 52-40-01. FOUND TO BE OUT OF LIMITS. R & R DOOR REF AMM.
- [SDR DALA1318100610](https://openairdocs.org/sdr/DALA1318100610.md): Latch · failed · Sep 2, 2013 · N610DL · Boeing 757232 · Passenger Oxygen System
  > SHIP 610, DURING PASS OXYGEN DOOR DEPLOYMENT TEST THE FOLLOWING DOORS FAILED TO OPEN. 20ABC, 21ABC, 27DEF, 29ABC, 33ABC, 38ABC, 41DEF. REPLACED AFFECTED DOORLATCH ACTUATORS IAW AMM 35-21-06.
- [SDR DALA1318090610](https://openairdocs.org/sdr/DALA1318090610.md): Latch · failed · Sep 2, 2013 · N610DL · Boeing 757232 · Passenger Oxygen System
  > MASKS FAILED TO DEPLOY WHEN LOSS OF CABIN PRESSURE -3A/B, 26ABC, 36DEF. REPLACED DOOR LATCH ACTUATORS 3A/B AND 26ABC. OPS CHECKED OK INCLUDING 36DEF. REF AMM 35-21-06 AND 35-21-00.
- [SDR DALA1317950610](https://openairdocs.org/sdr/DALA1317950610.md): Controller · failed · Sep 2, 2013 · N610DL · Boeing 757232 · Cabin Pressure Controller
  > AUTO INOP LIGHT ILLUMINATED WITH CABIN ALTITUDE, DEPLOYED PASSENGER OXYGEN MASKS. BITE CHECKED BOTH CABIN PRESSURE CONTROLLERS NR 1 FAULTS AC PWER LOSS REPLACED SAME. REPLACED UPPER POS PRESSURE RELIEF VALVE. PERFORMED O2 MASK DROP TEST INCLUDING ALT SWITC
- [SDR DALA1317410610](https://openairdocs.org/sdr/DALA1317410610.md): Light · inoperative · Aug 15, 2013 · N610DL · Boeing 757232 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE SEAT 1B AND 4B INOPERATIVE, REPLACED LIGHT ASSY AT 1B AND FUSE ON POWER SUPPLY, OPS NORMAL.
- [SDR DALA1317240610](https://openairdocs.org/sdr/DALA1317240610.md): Charger · inoperative · Aug 2, 2013 · N610DL · Boeing 757232 · Emergency Lighting
  > EMERGENCY LIGHTS OUT AT ROW 40C. R & R AFT EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA1309040610](https://openairdocs.org/sdr/DALA1309040610.md): Doubler · corroded · Apr 9, 2013 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION FOUND ON LWR TCAS ANTENNA AND DOUBLER. REMOVED OLD DOUBLER AND CLEANED IAW SRM 43-00-01. PERFORMED DETAILED INSPECTION. TREATED AND PRIMED IAW PS 900-4-1-N2 AND 900-3-6N3 R/R TCAS ANTENNA DOUBLER IAW DELTA EO NR 6-59954-3, REV D. R &
- [SDR DALA1301060610](https://openairdocs.org/sdr/DALA1301060610.md): Stanchion · damaged · Jan 11, 2013 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > DURING OPS 25505, FOUND ONE STANCHION MISSING OFF RT SIDE OF RESTRAINT AFT OF DOOR. REPAIRED AND INSTALLED STANCHION IAW SRM 51-70-11, FIG 1.
- [SDR DALA1300480610](https://openairdocs.org/sdr/DALA1300480610.md): Filter · leaking · Jan 4, 2013 · N610DL · Boeing 757232 · Fuel Controlling System
  > SUSPECTED LT ENG FUEL LEAK DUE TO FUEL CONFIG LIGHT ILLUM WITH 3.7 IN LT TANK AND 6.3 IN RT TANK. LT FUEL QTY DROPPING. MX REPLACED THE FUEL PUMP FILTER AND RAN ENGINE AT IDLE AND TAKEOFF POWER, NO LEAKS, CHECKED GOOD.
- [SDR DALA1232480610](https://openairdocs.org/sdr/DALA1232480610.md): Wire · broken · May 16, 2012 · N610DL · Boeing 757232 · Light System Wiring
  > DURING INSPECTION, MAINTENANCE DISCOVERED SEAT ROW 42D EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN LIGHT ASSY WIRING AND REPLACED LIGHT ASSY. OPERATES NORMAL.
- [SDR DALA1156940610](https://openairdocs.org/sdr/DALA1156940610.md): Floor Support · punctured · Oct 4, 2011 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > DUE ERA 49384-14MA TIME LIMITED REPAIR AT PUNCTURE AFT CARGO FLOOR STATION 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA REV C. HFEC INSP PER ERA 489384-14MA REV C. NO CRACKS FOUND. INSTALLED DOUBLER TO COMPLETE TEMP TIME LIMITED
- [SDR DALA1156930610](https://openairdocs.org/sdr/DALA1156930610.md): Floor Support · punctured · Oct 4, 2011 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > PUNCTURE IN AFT CARGO FLOOR CENTERLINE AT STA 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA. HFEC INSP PER ERA 489384-14MA REV C. NO CRACKS FOUND. INSTALLED DOUBLER TO COMPLETE TEMP TIME LIMITED SEC 11 DOUBLER PER ERA 489384-14MA.
- [SDR DALA1125210610](https://openairdocs.org/sdr/DALA1125210610.md): Light · inoperative · Apr 9, 2011 · N610DL · Boeing 757232 · Emergency Lighting
  > DURING A LAYOVER CHECK, MAINTENANCE FOUND THE AFT TWO OVERHEAD COMPARTMENT EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1011760610](https://openairdocs.org/sdr/DALA1011760610.md): Unknown · odor · May 28, 2010 · N610DL · Boeing 757232 · Air Distribution System
  > BURNED BALLAST SMELL NOTED IN OVERHEAD ABOVE SEAT 3DEF. TURNED LIGHTS OFF AND ODOR DISSIPATED. INSPECTED OVERHEAD LIGHTS, BALLASTS, PSUS AROUND ROW 31DEF. RAN BOTH ENGINES AND PACKS. ALL LIGHTS NORMAL. NO ODOR NOTED.
- [SDR DL757100237](https://openairdocs.org/sdr/DL757100237.md): Power Supply · inoperative · Feb 1, 2010 · N610DL · Boeing 757232 · Emergency Lighting
  > DURING EMERGENCY EGRESS LIGHTING TEST, AISLE LIGHTING AT ROWS 39-44 FAILED AFTER ONE MINUTE. REPLACED AFT POWER SUPPLY AND BATTEY PACK, CHECKS OK.
- [SDR DL757081815](https://openairdocs.org/sdr/DL757081815.md): Mount · worn · Dec 30, 2008 · N610DL · Boeing 757232 · Fuselage, Equipment Attach Fittings
  > DURING HMV, THE RT MLG DOOR CENTER MOUNT FITTING, HINGE SUPPORT AND BRACKET ATTACHMENT HOLES WERE FOUND TO BE WORN AND ELONGATED. THE HOLES WERE CLEANED UP TO ROUND DIAMETERS AND OVERSIZE BOLTS WERE INSTALLED IN SOME OF THE HOLES.
- [SDR DL757081802](https://openairdocs.org/sdr/DL757081802.md): Skin · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND UNDER THE AIRFONE ANTENNA BLANKING DOUBLER AT STA 1510, RT. THE CORRODED SKIN SECTION WAS CUT OUT AND AN SRM SKIN REPAIR WAS INSTALLED. A 12 MONTH DTA RESTRICTION WAS IMPOSED DUE TO CLOSE PROXIMITY OF ANOTHER EXISTING REPAIR D
- [SDR DL757081811](https://openairdocs.org/sdr/DL757081811.md): Skin · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN AT BS 1510-1520 UNDER RT AIRPHONE ANTENNA HAS CORROSION. COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81723520001.
- [SDR DL757081810](https://openairdocs.org/sdr/DL757081810.md): Sill · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP BETWEEN BS 1380 TO 1440 RBL 21 HAS THE LOWER SILL OF NR 2 CARGO DOOR WITH SEVERAL CORRODED AREAS AT UPPER SURFACE, CP53-156-021/COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81719980001.
- [SDR DL757081809](https://openairdocs.org/sdr/DL757081809.md): Stringer · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FUSELAGE S28L BS 1506 HAS EXFOLIATION CORROSION C/W AT SAA - SAT ON NON ROUTINE 81720380001.
- [SDR DL757081805](https://openairdocs.org/sdr/DL757081805.md): Stringer · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BETWEEN STA, 1500 AND STA, 1520 STRINGER S-29R FOUND WITH CORROSION AS MARKED. COMPLIED WITH AT SAA, SAT ON NON-ROUTINE 8172105000.
- [SDR DL757081804](https://openairdocs.org/sdr/DL757081804.md): Seat Track · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORRSION ON TOP SURFACE INBD FLANGE AT SAT, 1435 LBL48 AS MARKED W/L 208-10/COMPLIED WITH AT SAA -SAT ON NON- ROUTINE 81720150001.
- [SDR DL757081803](https://openairdocs.org/sdr/DL757081803.md): Intercostal · corroded · Dec 29, 2008 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO BETWEEN SAT, 1540 - SAT: 1560 BETWEEN STRINGERS S-26R AND S-27R FOUND SUPPORT WEB (INTERCOSTAL) WITH CORROSION AS MARKED C53-162-01L, COMPLIED WITH AT SAA-SAT ON NON ROUTINE 81721150001.
- [SDR DL757081797](https://openairdocs.org/sdr/DL757081797.md): Seat Track · corroded · Dec 27, 2008 · N610DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN COMPT FLOOR SEAT TRACK FOUND WITH CORROSION ON TOP SURFACE INBOARD FLANGE AT BS 1435 LBL 48 AS MARKEDW/L08-10. COMPLIED WITH AT SAA- SAT ON NON ROUTINE 81720150001.
- [SDR DL757081796](https://openairdocs.org/sdr/DL757081796.md): O2 Generator · damaged · Dec 27, 2008 · N610DL · Boeing 757232 · Passenger Oxygen System
  > FOUND ONE BLOWN OXYGEN CHEMICAL GENERATOR SN ARYD-F010-510 ON INSPECTION OF OXYGEN GENERATORS. COMPLIED WITH AT SAA- SAT ON N/R 81698450001 AND N/R 81707610001.
- [SDR DL757081795](https://openairdocs.org/sdr/DL757081795.md): Failsafe · corroded · Dec 27, 2008 · N610DL · Boeing 757232 · Fuselage Main, Frame
  > FAIL/SAFE STRAP CORRODED AT STA 900 SKIN BUTT JOINT BELOW WINDOW BELT RT SIDE OF FUSELAGE. COMPLIED WITH AT SAA SAT ON NON ROUTINE 81716550001.
- [SDR DL757081793](https://openairdocs.org/sdr/DL757081793.md): Fitting · corroded · Dec 27, 2008 · N610DL · Boeing 757232 · Cargo/Baggage Doors
  > FITTING AT BOTTOM OF AFT CARGO DOOR OPENING CORRODED ON BOTTOM STA 1400, NEW DOOR FITTING EXISTING PLATE AND NEW TIE DOWN FITTING INSTALLED IAW SRM 51-40-02 PG 39 FIG 12.
- [SDR DL757081790](https://openairdocs.org/sdr/DL757081790.md): Bellmouth · cracked · Dec 24, 2008 · N610DL · Boeing 757232 · APU Cowling/Containment
  > DURING HMV, CRACKS WERE FOUND IN THE APU AIR INTAKE PLENUM BELLMOUTH. THE CRACKING WAS ADDRESSED IN BOEING SERVICE BULLETIN 757-49-0011 AND THE CRACKED BELLMOUTH WAS REPLACED WITH A MODIFIED BELLMOUTH ASSEMBLY AS DIRECTED BY THE SERVICE BULLETIN.
- [SDR DL757081305](https://openairdocs.org/sdr/DL757081305.md): Skin · damaged · Oct 6, 2008 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE WAS FOUND IN THE FUSELAGE SKIN FORWARD OF STA 560 AT S-9R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ER/A 06-450569-14 WITH BOEING APPROVAL.
- [SDR DL757080833](https://openairdocs.org/sdr/DL757080833.md): Duct · cracked · May 4, 2008 · N610DL · Boeing 757232 · Pneumatic Distribution System
  > AT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPENED ISOLATION VLV AT FLT LVL 260 RIGHT ENGINE BLEED LIGHT ILLUM. CABIN PRESSURE CLIMBED THROUGH 10K DEPLOYED MASKS. DECLARED EMERGENCY INTO
- [SDR DL757070631](https://openairdocs.org/sdr/DL757070631.md): Skin · damaged · May 26, 2007 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING DAMAGE IN FUSELAGE SKIN S-4L LAP SPLICE. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS.
- [SDR DL75K060561](https://openairdocs.org/sdr/DL75K060561.md): Skin · lightning strike · Jul 8, 2006 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > REPAIR TO LIGHTNING STRIKE REQUIRED REMOVAL AND INSTALLATION WITH SOLID FASTENERS. CORRECTIVE ACTION PER ERA 450656-14 REV B.
- [SDR DL75K060401](https://openairdocs.org/sdr/DL75K060401.md): Valve · malfunctioned · May 17, 2006 · N610DL · Boeing 757232 · Nose/Tail Landing Gear
  > ON T/O FROM LGA, HAD DOOR LIGHT ILLUMINATE AND GEAR DOOR EICAS MSG WITH GEAR HANDLE UP, SAME LIGHT WHEN PUT GEAR DOWN T/S PER M/M CYCLED NOSE GEAR DOOR OPS NML. REPLACED DOOR, SAFETY VALVE PER M/M 32-35-23-004-001 AS PRECAUTIONARY MEASURE NEEDS OPS CHK. REMO
- [SDR DL757081592](https://openairdocs.org/sdr/DL757081592.md): Skin · cracked · Oct 27, 2005 · N610DL · Boeing 757232 · Passenger/Crew Doors
  > SUPPLEMENTAL SDR FUSELAGE/SKIN L-1 DOOR CUTOUT/UPPER FWD CORNER-CRACK IAW ERA 090914-14. C/W ERA 090914-14.
- [SDR DL75K050610](https://openairdocs.org/sdr/DL75K050610.md): Skin Panel · damaged · Sep 23, 2005 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 520 ABOVE STR 10R. INSTALLED REPAIR DOUBLER PER ER/A 450613-14.
- [SDR DL75K050595](https://openairdocs.org/sdr/DL75K050595.md): Skin · lightning strike · Sep 23, 2005 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 878, ABOVE STRINGER 4R. DAMAGE TO OUTER SKIN ONLY AT A PRODUCTION FASTENER LOCATION. REPAIR DOUBLER INSTALLED TO REPAIR THE DAMAGE CUTOUT.
- [SDR DL757030991](https://openairdocs.org/sdr/DL757030991.md): Pseu · faulty · Nov 8, 2003 · N610DL · Boeing 757232 · Landing Gear Position and Warning
  > DIVERSION TO PHX - APPARENT GROUND PROX SYS ERROR-AT CRUISE ALT GOT F/O PITOT- RT AUX PITOT- TAT - A/T DISC - PROBE HEAT CAUTIONS. LEFT GREEN SIDE OF NOSE AND RIGHT MAIN GEAR LIGHTS ILLUMINATED. STATUS MSGS GROUND PROX SYS - LANDING GEAR MONITOR - NOSE A/G D
- [SDR DL757030033](https://openairdocs.org/sdr/DL757030033.md): Fitting · cracked · Jan 3, 2003 · N610DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF EO 6-75079-3 OPN 0206, A CRACK WAS FOUND IN THE RIGHT WING UPPER LINK WING FITTING OUTBOARD LUG. REPAIRED PER ER/A 389433-14. BORE OVERSIZED AND OVERSIZED BUSHING INSTALLED.
- [SDR DL757030017](https://openairdocs.org/sdr/DL757030017.md): Sill · corroded · Jan 2, 2003 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > THE OUTER CHORD OF THE C2 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CHORD, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER ENDS REMOVED. A NEW SECTION OF SILL CHORD WAS INSTALLED, AND THE FRAME WEB AND CHORD SPLICED BACK IN PLACE WITH ALUM
- [SDR DL757030016](https://openairdocs.org/sdr/DL757030016.md): Floorbeam · corroded · Jan 2, 2003 · N610DL · Boeing 757232 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE FS 377 FLOORBEAM WAS FOUND CORRODED. THE UPPER CAP WAS TRIMMED OFF AND A NEW SECTION FABRICATED. DURING INSTALLATION OF THE NEW SECTION, SEVERAL ATTACH HOLES COMMON TO THE FS 377 FRAME AT LBL 65 WERE DAMAGED. THE AFFECTED HOLES WERE OVE
- [SDR DL757030015](https://openairdocs.org/sdr/DL757030015.md): Skin · dented · Jan 2, 2003 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1694 / STRG. 13L-15L: DENT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED ABOVE AN EXISTIN REPAIR FOR A SMALL CUTOUT. THE DENT WAS CUTOUT AND THE EXISTING REPAIR REMOVED. THE
- [SDR DL757030014](https://openairdocs.org/sdr/DL757030014.md): Floorbeam · corroded · Jan 2, 2003 · N610DL · Boeing 757232 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE ALL OF THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF FROM LBL 60 TO RBL 60. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 384247-14, REV A.
- [SDR DL757030013](https://openairdocs.org/sdr/DL757030013.md): Sill · corroded · Dec 31, 2002 · N610DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > THE INNER CHORD OF THE LOWER SILL OF THE C1 DOOR OPENING WAS FOUND WITH CORROSION AND TOOLING DAMAGE. THE INNER CHORD WAS REMOVED AND DISCARDED. A NEW CHORD WAS INSTALLED PER ER/A 384233-14.
- [SDR DL757021485](https://openairdocs.org/sdr/DL757021485.md): Skin · gouged · Dec 29, 2002 · N610DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 600 / STRG. 26L-27L: GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH 3 GOUGES AT FS 600 BETWEEN STRINGERS 26L & 27L. THE GOUGES WERE REMOVED WITH A SINGLE CUTOUT. THE CUTOUT
- [SDR DL757021454](https://openairdocs.org/sdr/DL757021454.md): Support Fitting · damaged · Dec 17, 2002 · N610DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure
  > DURING COMPLETION OF PYLON MOD EO 6-70332-3AD, HOLE NR 2 IN LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389426-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, AND INSTALLED EO FASTENER.
- [SDR DL757021453](https://openairdocs.org/sdr/DL757021453.md): Support Fitting · tool damage · Dec 17, 2002 · N610DL · Boeing 757232 · Nacelle/Pylon Structure
  > DURING ACCOMPLISHMENT OF PYLON MOD EO 6-70332-3AD, HOLE 5 IN THE LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389427-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, THE
- [SDR DL757021452](https://openairdocs.org/sdr/DL757021452.md): Fitting · gouged · Dec 17, 2002 · N610DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure
  > WHILE WORKING PYLON MOD EO 6-70332-3AD, HOLE NR 65 IN RIGHT WING SIDE LOAD FITTING WAS GOUGED. REPAIRED PER ER/A 389430-14AD. REPAIR OVERSIZED HOLE TO REMOVE DAMAGE AND INSTALLED OVERSIZED FASTENER.

Next page: https://openairdocs.org/deregistered/N610DL-2019-02-12/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 = 'N610DL' AND deregistration_id = 'N610DL-2019-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N610DL-2019-02-12/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.