# Service difficulty reports: N518DA, cancelled Oct 23, 2013

A list on [N518DA, cancelled Oct 23, 2013](https://openairdocs.org/deregistered/N518DA-2013-10-23.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 · 76 reports

- [SDR DL72S021391](https://openairdocs.org/sdr/DL72S021391.md): Actuator · failed · Nov 30, 2002 · N518DA · Boeing 727232 · Leading Edge Slat Actuator
  > AFTER T/O AMBER LED LIGHT REMAINED ILLUMINATED AT FLAPS 2. POSITION TEST SHOWED NR 4 L/E DEVICE NOT RETRACTED. REPLACED NR 4 SLAT ACTUATOR.
- [SDR DL72S021252](https://openairdocs.org/sdr/DL72S021252.md): Light · broken · Oct 27, 2002 · N518DA · Boeing 727232 · Emergency Lighting
  > SEAT 20DEF EMERGENCY LIGHT BROKEN, (FWD,RED) CA RPLD LIGHT.
- [SDR DL72S020069](https://openairdocs.org/sdr/DL72S020069.md): Light · inoperative · Jan 19, 2002 · N518DA · Boeing 727232 · Emergency Lighting
  > OVERWING EMERGENCY EXIT SIGN ILLUM, INOP SEAT LOC 22A. REPLACED LIGHT ASSY.
- [SDR DL72S020020](https://openairdocs.org/sdr/DL72S020020.md): Skin · cracked · Jan 1, 2002 · N518DA · Boeing 727232 · Empennage Structure
  > FOUND ON E2 LETTER CK 3/8 INCH CRACK VERT STAB OUTER SKIN APPROX 6 INCHES ABOVE 3RD FROM TOP VORTEX GENERATOR R/H SIDE. REPAIRED PER SRM 55-30-3.
- [SDR DL72S011886](https://openairdocs.org/sdr/DL72S011886.md): Power Supply · discharged · Dec 2, 2001 · N518DA · Boeing 727232 · Emergency Lighting
  > FOUND FWD CLOSET, ROW 1-4, ROW 10-11 EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY AND BATTERY PACK CKS GOOD
- [SDR DL72S011829](https://openairdocs.org/sdr/DL72S011829.md): Power Supply · discharged · Nov 19, 2001 · N518DA · Boeing 727232 · Emergency Lighting
  > FIRST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED FIRST CLASS EMERGENCY LIGHT POWER SUPPLY/CHARGER.
- [SDR DL72S010593](https://openairdocs.org/sdr/DL72S010593.md): Skin · cracked · Apr 9, 2001 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE YIELDED CRACK INDICATIONS. INTERNAL MFEC INSPECTION CONFIRMED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL AT FS 383 & 384. THE CRACKED AREA WAS ROUTED OUT AND A REPAIR DOUBLER AND STRUCTURAL FILLE
- [SDR DL72S002252](https://openairdocs.org/sdr/DL72S002252.md): Compressor · stalled · Nov 19, 2000 · N518DA · Boeing 727232 · Turbine Engine Compressor Section
  > COMPRESSOR STALL ON T/O ROLL NR 2 ENG. ABORT AT 30 KTS RETURN TO GATE. INSP INLET AND EXAUST. RAN ENG PER PFHB. ALL CK NORMAL, 13 KNT CROSS WIND GUSTING TO 19 KNTS.
- [SDR DL72S001724](https://openairdocs.org/sdr/DL72S001724.md): Charger · inoperative · Sep 7, 2000 · N518DA · Boeing 727232 · Emergency Lighting
  > BATTERY CHARGER INOP DAL (P/N 334701744) (S/N 7744).
- [SDR DL72S001567](https://openairdocs.org/sdr/DL72S001567.md): Megaphone · intermittent · Aug 16, 2000 · N518DA · Boeing 727232 · Emergency Equipment
  > CABIN MEGAPHONE INTERMITTANT OPS. REPLACED SAME.
- [SDR DL72S001548](https://openairdocs.org/sdr/DL72S001548.md): Skin · corroded · Aug 11, 2000 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH SEVERAL AREAS OF CORROSION BETWEEN FS 1010 & 1070 AND BETWEEN STRINGERS 26L & 26R. THE SKIN WAS CUT NEAR FS 1070 FROM THE SKIN SPLICE AT STRINGER 26L TO THE SKIN SPLICE AT STRINGER 26R. THE SECTION OF SKIN FROM THE CUT TO TH
- [SDR DL72S001530](https://openairdocs.org/sdr/DL72S001530.md): Attach Angle · cracked · Aug 11, 2000 · N518DA · Boeing 727232 · Trailing Edge Flaps
  > A.75 INCH CRACK AT I/B UPPER CORNER OF NR 5 LEADING EDGE FLAP ACTUATOR ATTACH ANGLE. REPAIRED SAME.
- [SDR DL72S001543](https://openairdocs.org/sdr/DL72S001543.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING MV4 VISIT CORROSION INSIDE STR 27L STA 950B TO 950C. DRILLED UP NEW STR 27L STA 950 TO STA 1010.
- [SDR DL72S001542](https://openairdocs.org/sdr/DL72S001542.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION AT O/B VERT LEG OF STR 26L STA 1010 - 1030. REMOVED AND REPLACED STR SECTION FROM STA 1010 TO STA 1183.
- [SDR DL72S001541](https://openairdocs.org/sdr/DL72S001541.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STR 26L O/B VERT LEG STA 950D - 950E. REMOVED AND REPLACED STRINGER FROM STA 950 - 1010.
- [SDR DL72S001540](https://openairdocs.org/sdr/DL72S001540.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION INSIDE STR 29L STA 1110 - 1130. REMOVED AND REPLACED STR 29L FROM STA 1010 TO 1183 PER SRM 53-10-1.
- [SDR DL72S001539](https://openairdocs.org/sdr/DL72S001539.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING MV4 VISIT CORROSION INSIDE STR 30 STA 970 - 990. REMOVED AND REPLACED STR 30 FROM 950 TO 1010 PER SRM 53-10-1.
- [SDR DL72S001535](https://openairdocs.org/sdr/DL72S001535.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING MV4 CORROSION VISIT NRC 375 CORROSION INSIDE STR 30 STA 1110 - 1130. REPLACED STR 30 FROM STA 1010 TO 1183.
- [SDR DL72S001534](https://openairdocs.org/sdr/DL72S001534.md): Stringer · corroded · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING MV4 CORROSION VISIT NRC 335 CORROSION INSIDE STR 27L FROM STA 1010 TO 1030. REPLACED STR 27L FROM STA 1010 TO STA 1130.
- [SDR DL72S001462](https://openairdocs.org/sdr/DL72S001462.md): Frame · cracked · Aug 2, 2000 · N518DA · Boeing 727232 · Fuselage Main, Frame
  > THE FS 950F FRAME WAS FOUND WITH A 3 INCH LONG CRACK AT STRINGER 26L. THE CRACK IS TYPICAL OF BAC S/B 727-53A0195. THE FRAME WAS REPAIRED WITH A B727 SRM REPAIR AS REQUIRED OF THE S/B AND DOCUMENTED PER ER/A 378052-14AD.
- [SDR DL72S001457](https://openairdocs.org/sdr/DL72S001457.md): Threshold · corroded · Aug 1, 2000 · N518DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE OUTER CHORD OF THE C2 DOOR CUTOUT LOWER SILL WAS FOUND WITH CORROSION ON THE O/B FLANGE BETWEEN FS 950E AND FS 990. THE CORROSION WAS BLENDED AWAY, ROTO PEENED, AND TREATED FOR CORROSION PREVENTION. AN EXTERNAL REPAIR STRAP WAS INSTALLED TO REPAIR THE DA
- [SDR DL72S001439](https://openairdocs.org/sdr/DL72S001439.md): Rib · cracked · Jul 28, 2000 · N518DA · Boeing 727232 · Wing, Rib/Bulkhead
  > THE RBL 70.5 WING RIB WAS FOUND WITH A CRACK AT FS 760.96. THE CRACK IS TYPICAL OF BAC S/B 727-57-0112 AND PROGRESSED BETWEEN TWO FASTENER HOLES. THE HOLES WERE OVERSIZED TO ENSURE CRACK CONTAINMENT AND A REPAIR ANGLE INSTALLED PER S/B 727-57-0112 AND ER/A
- [SDR DL72S001360](https://openairdocs.org/sdr/DL72S001360.md): Stringer · corroded · Jul 18, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION INSIDE STR 25L STA 950D TO 950E AROUND RIVETS. REPLACED STR 25L FROM STA 950 TO 1010 DUE TO OUT OF LIMIT CORROSION ON ENTIRE LENGTH OF STRINGER. (REF NR''S 207, 214, 218, 221, 224).
- [SDR DL72S001359](https://openairdocs.org/sdr/DL72S001359.md): Stringer · corroded · Jul 18, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION INSIDE STR 24L STA 950D TO 950E AROUND RIVETS. REPLACED STR 23L FROM STA 950 TO 1010 DUE TO OUT OF LIMIT CORROSION ON ENTIRE LENGTH OF STRINGER. (REF NR''S 209, 210, 213, 219, 222, 225, 229).
- [SDR DL72S001358](https://openairdocs.org/sdr/DL72S001358.md): Stringer · corroded · Jul 18, 2000 · N518DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > CORROSION INSIDE STR 23L STA 950D TO 950E. REPLACED STR 23L FROM STA 950 TO 1010 DUE TO OUT OF LIMIT CORROSION ON ENTIRE LENGTH OF STR 23L (REF NR''S 99, 206, 208, 211, 212, 220, 223, 226, 230).
- [SDR DL72S001538](https://openairdocs.org/sdr/DL72S001538.md): Attach Angle · cracked · Jul 10, 2000 · N518DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING MV4 VISIT,.75 INCH CRACK AT I/B UPPER CORNER NR 5 L/E FLAP ACT ATTACH ANGLE. REMOVED L/E SUPPORT ROD AND INSTALLED DOUBLER PER MM 57-20-21 FIG 807. INSTALLED L/E SUPPORT ROD.
- [SDR DL72S001364](https://openairdocs.org/sdr/DL72S001364.md): Rib · cracked · Jul 10, 2000 · N518DA · Boeing 727232 · Leading Edge Devices
  > A 2 INCH CRACK IN NR 5 SLAT L/E RIB LWR AFT CORNER I/B OF ACT ROD END. REPAIRED PER 727 M/M 57-54-0 PG 805.
- [SDR DL72S000495](https://openairdocs.org/sdr/DL72S000495.md): Flap Track · corroded · Mar 13, 2000 · N518DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL OF THE I/B FLAP TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS; AND TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS AND THE MLG DOOR HINGE FITTING ATTACH HOLES. PART REPAIRED PER ER/A 387423-14AD AND BF GOOD
- [SDR DL72S992132](https://openairdocs.org/sdr/DL72S992132.md): Light · contaminated · Sep 24, 1999 · N518DA · Boeing 727232 · Exterior Lighting
  > DURING GROUND TRANSFER OF FUEL, THE NR 1 VALVE INDICATOR LIGHT SPARKED AND CAUGHT ON FIRE. DE-POWERED SWITCH AND FIRE EXTINGUISHED. MAINTENANCE FOUND LIGHT ASSY FULL OF FUEL. CHECKED FOR FUEL LEAKS, NONE FOUND. REPLACED LIGHT ASSY, OPN NOW NORMAL.
- [SDR DL72S992082](https://openairdocs.org/sdr/DL72S992082.md): Batteries · discharged · Sep 16, 1999 · N518DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPERATION NOW NML.
- [SDR DL72S991946](https://openairdocs.org/sdr/DL72S991946.md): Web · cracked · Sep 1, 1999 · N518DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C2 LETTER CK,.0625 INCH CRACK IN LT TORQUE BOX WEB LT SIDE STA 1266. REPAIRED PER MM 53-11-0.
- [SDR DL72S990403](https://openairdocs.org/sdr/DL72S990403.md): Skin · cracked · Feb 25, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 7 CRACK LOCATIONS ALONG THE PANEL. THE ENTIRE LAP SPLICE WAS CUTOUT ALONG THE PAN
- [SDR DL72S990402](https://openairdocs.org/sdr/DL72S990402.md): Skin · cracked · Feb 25, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 4 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AL
- [SDR DL72S990394](https://openairdocs.org/sdr/DL72S990394.md): Battery Pack · discharged · Feb 25, 1999 · N518DA · Boeing 727232 · Emergency Lighting
  > BATTERY DEAD ON EMERGENCY FLASHLIGHT AT 1L DOOR. REPLACED BATTERY AND BULB.
- [SDR DL72S990393](https://openairdocs.org/sdr/DL72S990393.md): Light · inop · Feb 25, 1999 · N518DA · Boeing 727232 · Emergency Lighting
  > MID CEILING EMER LIGHT WOULD NOT ELIMINATE WHEN CHECKING EMERGENCY LIGHTS. REPLACED LIGHT ASSY.
- [SDR DL72S990363](https://openairdocs.org/sdr/DL72S990363.md): Skin · cracked · Feb 23, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 12 CRACKS ALONG THE LENGTH OF THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LE
- [SDR DL72S990372](https://openairdocs.org/sdr/DL72S990372.md): Skin · cracked · Feb 22, 1999 · N518DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACK INDICATIONS AT APPROX FS 1100 WITH NO OTHER CRACK INDICATIONS FOR THE ENTIRE PANEL LENGTH. TH
- [SDR DL72S972364](https://openairdocs.org/sdr/DL72S972364.md): Tee · corroded · Nov 10, 1997 · N518DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > AT HMV, FOUND RT DOOR ATTACH TEE CORRODED. SECTION REMOVED FOR MTC ACCESS AT APPROX FUSELAGE STA 865. CUT OUT SECTION OF DOOR ATTACH TEE. FABRICATED REPAIR PARTS PER MM 53-30-1 AND SRM 51-40-3. INSTALLED REPAIR PER M/M 53-30-1.
- [SDR DL72S972284](https://openairdocs.org/sdr/DL72S972284.md): Skin · dented · Nov 7, 1997 · N518DA · Boeing 727232 · Ailerons
  > UPPER SKIN HAS A SMALL DENT AT AFT INBD CORNER. REPAIRED PER SRM 57-50-5 FIG 3.
- [SDR DL72S972283](https://openairdocs.org/sdr/DL72S972283.md): Skin · damaged · Nov 7, 1997 · N518DA · Boeing 727232 · Ailerons
  > IMPROPER SPLICE REPAIR ON LOWER SKIN. REPAIRED PER M/M 57-51-0.
- [SDR DL72S972350](https://openairdocs.org/sdr/DL72S972350.md): Web · cracked · Nov 6, 1997 · N518DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > WEB CRACKED.5 INCH ON LT VENTRAL STAIR TORQUE BOX AT STA 1213. REMOVED FASTENER, DYE CHECKED AREA, STOP DRILLED ENDS OF CRACK, FABRICATED REPAIR DOUBLER PER M/M 53-11-0 NR 19. INSTALLED REPAIR AS PER MM 53-11-0 NR 19.
- [SDR DL72S972531](https://openairdocs.org/sdr/DL72S972531.md): Doudler · cracked · Oct 29, 1997 · N518DA · Boeing 727232 · Trailing Edge Flaps
  > REPAIR DOUBLER CRACKED ON LOWER AFT CHORD ANGLE 37 FROM I/B END OF FLAP. DAMAGE REPAIRED PER M/M 57-52-0 PAGE 807, ON SHOP ORDER 331063.
- [SDR DL72S972516](https://openairdocs.org/sdr/DL72S972516.md): Flap · damaged · Oct 29, 1997 · N518DA · Boeing 727232 · Trailing Edge Flaps
  > AFT LWR CHORD IS CRACKED AT I/B AFT FLAP TRACK CUT OUT, TWO PLACES. ALSO, AFT LOWER CHORD ANGLE IS CRACKED 57 FROM I/B END. BOTH REPAIRS PER M/M 57-52-0 FIG 807.
- [SDR DL72S972349](https://openairdocs.org/sdr/DL72S972349.md): Floorbeam · worn · Oct 28, 1997 · N518DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM UPPER CAP IS WORN THIN AT FLOOR PNL SCREW HOLE FS 344 RBL 12 TO LBL 45. BLENDED AREAS FOR FURTHER EVALUATION. FOUND BEAM OUT OF LIMITS PER 53-10-1 FIG 4. REMOVED T-CAP FROM RBL 60 TO LBL 60. STARTED DRILLING NEW T-CAP PER SRM 53-10-8. INS
- [SDR DL72S972348](https://openairdocs.org/sdr/DL72S972348.md): Frame · cracked · Oct 28, 1997 · N518DA · Boeing 727232 · Nacelle/Pylon, Frame/Spar/Rib
  > FRAME CRACKED NR 2 INLET S-DUCT HOUSING FRAME CRACKED ON LT SIDE FS 1233 AT INTERSECTION WITH HORSE COLLAR. REMOVED DAMAGE AND FABRICATED DOUBLERS PER SRM 51-400-3, INSTALLED DOUBLERS PER SRM 51-40-3.
- [SDR DL72S972483](https://openairdocs.org/sdr/DL72S972483.md): Skin · cracked · Oct 27, 1997 · N518DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB SKIN CRACKED. DRILLED REPAIR DOUBLER PER SRM 55-30-3, CUTOUT DAMAGE PER SRM 55-30-3. VERIFIED CRACK REMOVAL AND INSTALLED REPAIR DOUBLER PER SRM 55-30-3.
- [SDR DL72S972482](https://openairdocs.org/sdr/DL72S972482.md): Skin · cracked · Oct 27, 1997 · N518DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB SKIN CRACKED. CUT OUT CRACK PER SRM 55-30-3 AND VERIFIED CRACK REMOVAL. FABRICATED REPAIR AND INSTALLED DOUBLER/REPAIR.
- [SDR DL72S972262](https://openairdocs.org/sdr/DL72S972262.md): Web · cracked · Oct 27, 1997 · N518DA · Boeing 727232 · Vertical Stabilizer
  > WEB - CRACKED VETICAL STAB INTERIOR FS 1303 WEB CRACKED AT STRINGER CUTOUT, RH SIDE FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17BEGAN INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.STOP DRILLEDCRACK AND DYE CHECKED PER SRM 53-10-4. COMPLETED INSTA
- [SDR DL72S972261](https://openairdocs.org/sdr/DL72S972261.md): Web · cracked · Oct 27, 1997 · N518DA · Boeing 727232 · Vertical Stabilizer
  > WEB - CRACKED VERT STAB INTERIOR FS1303 WEB CRACKED A T LOWER LH CORNER FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17DYE CHECKED AND STOP DRILLED CRACK PER SRM 53-10-4. OK TO INSTALL REPAIR. INSTALLED REPAIR PER SRM 53-10-4 FIG 17
- [SDR DL72S972206](https://openairdocs.org/sdr/DL72S972206.md): Bulkhead Beam · cracked · Oct 27, 1997 · N518DA · Boeing 727232 · Fuselage Main, Bulkhead
  > A CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX 1 LONG AND IS LOCATED AT APPROX WL237 IN THE INBD RADIUS OF THE AFT CHORD. REPAIRED PER ERA 330932-14.

Next page: https://openairdocs.org/deregistered/N518DA-2013-10-23/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 = 'N518DA' AND deregistration_id = 'N518DA-2013-10-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N518DA-2013-10-23/reports

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