# Service difficulty reports: N609DL, cancelled Feb 12, 2019

A list on [N609DL, cancelled Feb 12, 2019](https://openairdocs.org/deregistered/N609DL-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.

- [SDR DALA14036110609](https://openairdocs.org/sdr/DALA14036110609.md): Lens · cracked · Jun 16, 2014 · N609DL · Boeing 757232 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT LENS CRACKED. INSTALLED LENS ASSY IAW AMM 33-51.
- [SDR DALA14026410609](https://openairdocs.org/sdr/DALA14026410609.md): Skin · damaged · Apr 25, 2014 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BS 884, S14R LAP JOINT UPPER ROW, HAS A SHEARED RIVET. REPAIRED IAW ERA 514437-14, REV A.
- [SDR DALA13065910609](https://openairdocs.org/sdr/DALA13065910609.md): Door · lack of lube · Nov 30, 2013 · N609DL · Boeing 757232 · Passenger/Crew Doors
  > DOOR CLOSED AND COULD NOT ARM. REMOVED AND REINSTALLED SLIDE LUBED DOOR.
- [SDR DALA1315640609](https://openairdocs.org/sdr/DALA1315640609.md): Connector · damaged · Jun 17, 2013 · N609DL · Boeing 757232 · Light System Wiring
  > EMERGENCY LIGHTS TEST RT SEATS 38 AND AFT WILL NOT COME ON. REPLACED POWER SUPPLY M9102 AND BATTERY PACK. REPLACED ADT LT EMERGENCY TEST SWITCH ABOVE LT PASS DOOR. REPAIRED GROUND WIRE CONNECTOR ON S10295-AFT EMERGENCY LIGHT TEST SWITCH. EMERGENCY LIGHTS TES
- [SDR DALA1313350609](https://openairdocs.org/sdr/DALA1313350609.md): Battery Pack · inoperative · May 20, 2013 · N609DL · Boeing 757232 · Emergency Lighting
  > ON SERVICE CHECK FOUND EMERGENCY LIGHTS FROM ROW 38AFT INOPERATIVE. FOUND BATTERY PACK FAILURE. REPLACED BATTERY PACK CHECKED NORMAL IAW AMM 33-52.
- [SDR DALA1311670609](https://openairdocs.org/sdr/DALA1311670609.md): Skin · damaged · Apr 28, 2013 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE AT BS 1190, 2 INCHES BELOW STRINGER 9L. REPAIRED IAW SRM 53-00-01.
- [SDR DALA1311650609](https://openairdocs.org/sdr/DALA1311650609.md): Structure · damaged · Apr 28, 2013 · N609DL · Boeing 757232 · Engine Thrust Reverser
  > NR 1 ENGINE OTBD THRUST REVERSTER T/E HAS LIGHTNING DAMAGE. BETWEEN 630 AND 830. REPAIRED IAW SRM SRM 54-31-01.
- [SDR DALA1308350609](https://openairdocs.org/sdr/DALA1308350609.md): Skin · damaged · Apr 4, 2013 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FOUND SKIN DAMAGE AT RT SIDE OF ACFT STRINGER 17, STATION 382. BURNISHED GOUGE IAW SRM 53-00-01. HFEC INSPECTED BURNISHED AREA IAW SRM 53-00-01. NO CRACKS INDICATED. FINISHED REPAIR SRM 53-00-01.
- [SDR DALA1243640609](https://openairdocs.org/sdr/DALA1243640609.md): Structure · punctured · Jul 23, 2012 · N609DL · Boeing 757232 · Engine Thrust Reverser
  > DURING WALK AROUND MAINTENANCE DISCOVERED TWO PUNCTURES ON LT ENGINE REVERSER COWL INBD AT 4 O'CLOCK POSITION. COMPLIED WITH REPAIR PER SRM 54-31-01. TOUCHED UP PAINT PER AMM 51-21.
- [SDR DL757090970](https://openairdocs.org/sdr/DL757090970.md): Doubler · corroded · May 31, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF JAM NUT ON MID LAV PAN T- HANDLE CABLE FOUND LAV SERVICE PAN INTERNAL DOUBLER CORRODED AT STA 700 RBL 50 IN FWD PIT CP53-122-01I. C/W AT SAA - SAT ON N/R 122605 JOB 82876050001.
- [SDR DL757090969](https://openairdocs.org/sdr/DL757090969.md): Sill · corroded · May 31, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SILL UPPER CHORD LOWER SURFACE FOUND CORROSION UNDER AND AROUND NUT PLATES STA 1380 TO 1440 (AFT CARGO DOOR CUTOUT) CP53-156-01I, C/W AT SAA- SAT ON N/R 122091 JOB 82874020001.
- [SDR DL757090968](https://openairdocs.org/sdr/DL757090968.md): Skin · dented · May 31, 2009 · N609DL · Boeing 757232 · Leading Edge Devices
  > NR 10 SLAT HAS AREA OF HAIL DAMAGE, C/W AT SAA - SAT ON N/R 113285 JOB 82869040001.
- [SDR DL757090967](https://openairdocs.org/sdr/DL757090967.md): Fitting · corroded · May 31, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FSTS 1376 S25L BOTTOM STOP PAN FITTING HAS SURFACE CORROSION CP53-153-03I/ C/W AT SAA - SAT ON N/R 108399 JOB 82873190001.
- [SDR DL757090949](https://openairdocs.org/sdr/DL757090949.md): Failsafe · corroded · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Main, Structure
  > FUSELAGE FAIL SAFE STRAP CORRODED RT SIDE AT STA900. C/W AT SAA - SAT ON N/R 114038 JOB 82866730001.
- [SDR DL757090947](https://openairdocs.org/sdr/DL757090947.md): Intercostal · corroded · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO CCOMPARTMENT FLOOR STRUCTURE AT STA 1458 TO 1472 INTERCOSTAL AND SUPPORT PLATE ARE CORRODED RBL 13.50, CP53-156-01I.
- [SDR DL757090946](https://openairdocs.org/sdr/DL757090946.md): Attach Angle · corroded · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > CORROSION INTERCOSTAL AT ATTACH ANGLE TO SKIN AT FS 740 TO 760 IN FWD CARGO COMPARTMENT RBL10 ( CP53-127-01). C/W AT SAA, SAT ON N/R 122053 JOB 82874/840001.
- [SDR DL757090945](https://openairdocs.org/sdr/DL757090945.md): Skin · dented · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE STA 1310-1330 S29L TO S28R PREVIOUS BLENDOUTS MULTIPLE SHARP DENTS, NO TAG C/W AT SAA - SAT ON N/R 107953 JOB 82866150001.
- [SDR DL757090944](https://openairdocs.org/sdr/DL757090944.md): Support Channel · corroded · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 353 LBL 60 AT L1 DOOR SUBFLOOR SUPPORT CHANNEL HAS HEAVY CORROSION (CP53-221-01I) C/W AT SAA - SAT ON N/R 122071 JOB 82874520001.
- [SDR DL757090943](https://openairdocs.org/sdr/DL757090943.md): Shim · migrated · May 29, 2009 · N609DL · Boeing 757232 · Trailing Edge Flaps
  > R/W NR 8 FLAP TRACK CORRODED BETWEEN AFT SHIM AND TRACK. SHIM MIGRATED C/W AT SAA - SAT ON N/R 129961 JOB 82868960001.
- [SDR DL757090942](https://openairdocs.org/sdr/DL757090942.md): Cusp Web · corroded · May 29, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > CUSP WEB INNER CHORD CORRODED AT BS 1030 RBL 62 IN MAIN CABIN (CP53-242-01-02-02I) C/W AT SAA - SAT ON N/R 114200 JOB 82873320001.
- [SDR DL757090941](https://openairdocs.org/sdr/DL757090941.md): Reservoir · damaged · May 29, 2009 · N609DL · Boeing 757232 · Passenger/Crew Doors
  > DURING L2 DOOR RIG FOUND EMERGENCY ASSIST RESERVOIR DISCHARGED. REMOVED AND REPLACED EMERGENCY POWER ASSIST RESERVOIR PER AMM 52-11-404-013 AT SAA - SAT ON N/R 125725 JOB 82876300001.
- [SDR DL757090876](https://openairdocs.org/sdr/DL757090876.md): Seat Track · corroded · May 17, 2009 · N609DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STA 750 -0900 SEAT TRACK SECTION AT LBL 45 HAS MODERATE CORROSION AT STA 800 -830 - 860 ( WORK WITH NR 108454 / C/W AT SAA - SAT ON N/R 108453 JOB 82874430001 AND N/R 108454.
- [SDR DL757090875](https://openairdocs.org/sdr/DL757090875.md): Angle · cracked · May 17, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT AREA CRACKED INTERCOASTAIL UPPER ANGLE BETWEEN STA 1580-1600 BLO/ C/W AT SAA - SAT ON N/R 108393 JOB 82873280001.
- [SDR DL757090861](https://openairdocs.org/sdr/DL757090861.md): Crease Beam · cracked · May 15, 2009 · N609DL · Boeing 757232 · Fuselage Main, Structure
  > MAIN CABIN STA 410 STRINGER 17L AT CREASE BEAM. CREASE BEAM WEB IS CRACKED / C/W AT SAA - SAT ON N/R 122068 JOB 82874500001.
- [SDR DL757090860](https://openairdocs.org/sdr/DL757090860.md): Sill · corroded · May 15, 2009 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. DOOR CUT OUT STRUCTURE LOWER SILL STA 1380 TO 1440 WEB HAS CORROSION ON MULTIPILE PLACES CP53 - 154 -01I/ C/W AT SAA - SAT ON N/R 122162 JOB 82873960001.
- [SDR DL757081344](https://openairdocs.org/sdr/DL757081344.md): Intercostal · damaged · Oct 8, 2008 · N609DL · Boeing 757232 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BS 860-880 BL 0 WL 208 HAS DAMAGED HOLES REMOVED AND REPLACED PER SRM 51-40-02 STEP 4.
- [SDR DL757081333](https://openairdocs.org/sdr/DL757081333.md): Floor Panel · corroded · Oct 6, 2008 · N609DL · Boeing 757232 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL AT STATION 1510 LBL 17 TO RBL 17. REPAIRED ON NR 00031 PER 53-00-53.
- [SDR DL757081338](https://openairdocs.org/sdr/DL757081338.md): Stringer Splice · corroded · Oct 1, 2008 · N609DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO CORROSION NOTED ON STRINGER SPLICE RADIUS STA 605 LBL 15. REPAIRED IAW SRM 53-00-03 FIG 201.
- [SDR DL757071044](https://openairdocs.org/sdr/DL757071044.md): Skin · dented · Aug 8, 2007 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DENTS IN FUSELAGE SKIN NEAR RADOME AT FS 220, LT SIDE, S-23L. CUTOUT DENTS AND INSTALLED DOUBLER.
- [SDR DL757081686](https://openairdocs.org/sdr/DL757081686.md): Structure · dented · Aug 7, 2007 · N609DL · Boeing 757232 · Fuselage Main, Structure
  > MAJOR REPAIR ER/A 463313-14. THREE DENTS NEAR A/C NOSE REPAIRED.
- [SDR DL75K060395](https://openairdocs.org/sdr/DL75K060395.md): Skin · cracked · May 10, 2006 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND IN THE FUSELAGE SKIN AT THE EDGE OF THE L1 DOOR OPENING UPPER FORWARD CORNER. A DOUBLER WAS INSTALLED, REF. AD 2004-09-32, 2001-20-12.
- [SDR DL75K060245](https://openairdocs.org/sdr/DL75K060245.md): Outflow Valve · leaking · Apr 4, 2006 · N609DL · Boeing 757232 · Pressure Regulator/Outflow Valve
  > AT FL410 - CABIN ALT WARNING, CABIN ALT EXCEEDED 10,000 FT. OUTFLOW VALVE CLOSED. ALL BLEEDS AND PACKS NORM. RECIRC FAN ON. C/W QRH PROCEDURES. DIVERTED TO MCO. BITE OF CABIN PRESSURE CONTROLLERS 1 AND 2 SHOW NO FAULTS. AMM TASK 05-51-24-702-001 HAS EXC
- [SDR DL757030828](https://openairdocs.org/sdr/DL757030828.md): Power Supply · discharged · Sep 9, 2003 · N609DL · Boeing 757232 · Emergency Lighting
  > ON L/O FOUND EMERGENCY EXIT LIGHTS INOP AT RT OVERWING EXIT, RT AISLE, RIGHT AFT WING ILUM, AND RIGHT MID WING ILLUM POSITIONS. REPLACED PWR SUPPLY M10568 AND BATTERY. EMERGENCY LIGHTS NOW CHECK GOOD.
- [SDR DL757030470](https://openairdocs.org/sdr/DL757030470.md): Battery · discharged · May 18, 2003 · N609DL · Boeing 757232 · Emergency Equipment
  > MEGAPHONE L1 CLOSET INOPERATIVE. REPLACED BATTERIES
- [SDR DL757030463](https://openairdocs.org/sdr/DL757030463.md): Skin · corroded · May 12, 2003 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE COMMON TO THE VHF ANTENNA CUTOUT AND THE REINFORCING DOUBLERS AT FS 1470 AND BL 0. THE EXISTING DOUBLERS WERE REMOVED AND THE ANTENNA CUTOUT ENLARGED TO REMOVE THE CORROSION. TWO LARGER ALUMINUM EXTERNAL DOU
- [SDR DL757030456](https://openairdocs.org/sdr/DL757030456.md): Skin · dented · May 10, 2003 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > DENT CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND WITH MULTIPLE DENT LOCATIONS BETWEEN FS 1570 & 1615 AND BETWEEN STRINGERS 18L & 22L. THE DENTS WERE REMOVED WITH CUTOUTS TO THE SKIN AND REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 3
- [SDR DL757030426](https://openairdocs.org/sdr/DL757030426.md): Skin · dented · May 3, 2003 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1710 JUST BELOW THE STRINGER 14R SKIN LAP JOINT. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384813-14, REV A.
- [SDR DL757030425](https://openairdocs.org/sdr/DL757030425.md): Skin · dented · May 3, 2003 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE SKIN WAS FOUND WITH 4 DENTS BETWEEN FS 601 & 630 AND BETWEEN STRINGERS 15L & 16L. THE DENTS WERE REMOVED WITH 4 SMALL CUTOUTS AND REPAIRED WITH A SINGLE EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384778-14, REV A.
- [SDR DL757002525](https://openairdocs.org/sdr/DL757002525.md): Warning System · unserviceable · Dec 28, 2000 · N609DL · Boeing 757232 · Trailing Flap Position Indicating System
  > WHEN FLAPS SET TO 1 DEG T/E FLAP LIGHT CAME ON, WOULD NOT RESET. WENT THROUGH PROCEDURE USED ALT FLAP 20 DEG FOR LANDING. WHEN ALT SELECTED TO 20 DEG, ON FINAL SLAT DIS AGREE LIGHT CAME ON NO ABNORMAL CONTROL. CHECKED T/E FLAPS FOR DAMA
- [SDR DL757991055](https://openairdocs.org/sdr/DL757991055.md): Skin · gouged · May 13, 1999 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND GOUGED AT FS 1150. THE DAMAGED AREA OF UPPER SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 367340-14.
- [SDR DL757980444](https://openairdocs.org/sdr/DL757980444.md): Skin · dented · Feb 20, 1998 · N609DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN BETWEEN FS 1580 AND 1600 BETWEEN STR 18L AND 22L WAS BADLY TORN AND DENTED FROM GROUND EQUIPMENT. THE DAMAGE WAS CUT OUT AND A SKIN DOUBLER WAS INSTALLED PER ER/A 364067-14, REV A. THE UNDERLYING STRINGERS WERE REPAIRED PER THE B757 SRM.
- [SDR DL757954014](https://openairdocs.org/sdr/DL757954014.md): Radome · damaged · Jun 11, 1995 · N609DL · Boeing 757232 · Aerodynamic Fairings
  > RADOME CAVED IN DURING DESCENT. SHOP INSPECTION FOUND WHITE AND YELLOW MARKS OF PAINT IN CAVED AREA. THIS AREA SEEMED TO BE HIT. REBUILD RADOME COMPLETE USING 757 MOLD AND BOEING SPEC MATERIAL.
- [SDR DL757951681](https://openairdocs.org/sdr/DL757951681.md): Weight · cracked · Apr 19, 1995 · N609DL · Boeing 757232 · Ailerons
  > AT HMV, THE LWR L/E AT THE O/B END OF THE I/B WEIGHT ON THE RT AILERON WAS FOUND CRACKED. THIS WAS REPAIRED PER SRM 57-60-01.
- [SDR DL757951726](https://openairdocs.org/sdr/DL757951726.md): Wedge · worn · Apr 17, 1995 · N609DL · Boeing 757232 · Leading Edge Devices
  > LOWER AFT EDGE IS WORN ON NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 REF AD 90-23-06. FOUND AND REPAIRED DURING HMV.
- [SDR DL757951680](https://openairdocs.org/sdr/DL757951680.md): Floorbeam · corroded · Apr 17, 1995 · N609DL · Boeing 757232 · Fuselage Main, Floor Beam
  > AT HMV, CORROSION WAS FOUND ON FLOORBEAM BL0 TO RT FUSELAGE SKIN STA 324. REMOVED CORR AND CK LIMITS PER SRM 53-10-8 FIG 101. DRILLED REPAIR SPLICE ANGLES PER SRM 53-10-8 AND INSTALLED PER SAME.
- [SDR DL757951600](https://openairdocs.org/sdr/DL757951600.md): Floorbeam · corroded · Apr 17, 1995 · N609DL · Boeing 757232 · Fuselage Main, Floor Beam
  > AT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 760 FROM LBL 15 TO RBL 15. THE CORROSION WAS REMOVED AT BL0 TO RBL 15 WITHIN LIMITS PER SRM 53-00-51 FIG 101. CORR REM AT LBL 5 TO BL 0 NOT IN EXCESS OF.040 DEPTH. REPAIR FABRICATED PER SRM 53-30-51 FIG
- [SDR DL757951599](https://openairdocs.org/sdr/DL757951599.md): Floorbeam · corroded · Apr 17, 1995 · N609DL · Boeing 757232 · Fuselage Main, Floor Beam
  > AT HMV, THE CABIN FLOORBEAM UPPER CAP WAS FOUND TO BE CORRODED FROM LBL 10 TO 16. REPAIRED PER SRM 53-30-51 FIG 202.
- [SDR DL757951682](https://openairdocs.org/sdr/DL757951682.md): Skin · damaged · Apr 13, 1995 · N609DL · Boeing 757232 · Nacelle/Pylon, Plate/Skin
  > AT HMV, PERM REPAIR OF NR 2 ENG NACELLE STRUT SKIN I/B WAS SCHEDULED. THE DAMAGE WAS ROUTED OUT, INSP FOR CRACKS (NONE DETECTED), AND DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED PER SRM 54-51-01.
- [SDR DL757950067](https://openairdocs.org/sdr/DL757950067.md): Flap · gouged skin · Jan 5, 1995 · N609DL · Boeing 757232 · Trailing Edge Flaps
  > DURING LETTER CHECK, RIGHT WING NR 4 AFT FLAP LOWER SKIN WAS FOUND GOUGED BETWEEN THE NR 7 AND NR 8 FLAP FAIRING. REPAIRED PER SMR 57-70-05.

## 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 = 'N609DL' AND deregistration_id = 'N609DL-2019-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N609DL-2019-02-12/reports

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