# Service difficulty reports: N529DA, cancelled Oct 27, 2014

A list on [N529DA, cancelled Oct 27, 2014](https://openairdocs.org/deregistered/N529DA-2014-10-27.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 · 63 reports

- [SDR DL72S011897](https://openairdocs.org/sdr/DL72S011897.md): Battery · discharged · Dec 4, 2001 · N529DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES IN LIGHT ASSY
- [SDR DL72S011871](https://openairdocs.org/sdr/DL72S011871.md): Angle · cracked · Nov 27, 2001 · N529DA · Boeing 727232 · Wing Structure
  > 1.5 INCH CRACK UNDER STOP PAD NBR 6 SLAT OUTBOARD STOP PAD. COVE SKIN ANGLE REPAIRED PER M/M 57-54-000-8
- [SDR DL72S011870](https://openairdocs.org/sdr/DL72S011870.md): Beam · chafed · Nov 27, 2001 · N529DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > MLG SUPPORT BEAM CHAFED I/B FWD END OF T/E PANEL I/B END. REPAIR PER MM 57-43-000-8 FIG 801.
- [SDR DL72S011869](https://openairdocs.org/sdr/DL72S011869.md): Angle · cracked · Nov 27, 2001 · N529DA · Boeing 727232 · Wing, Control Surfaces
  > NBR 3 SLAT AFT ANGLE CRACKED AT ACTUATOR ROD END ATTACH REPAIR PER MM 57-54-000-8 FIG 807
- [SDR DL72S011803](https://openairdocs.org/sdr/DL72S011803.md): Battery · discharged · Nov 13, 2001 · N529DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY.
- [SDR DL72S011086](https://openairdocs.org/sdr/DL72S011086.md): Skin · cracked · Jun 21, 2001 · N529DA · Boeing 727232 · Leading Edge Devices
  > LOWER LEADING EDGE SKIN SPAR CRACKED AT ACTUATOR ARM CUTOUT. REPAIRED PER 727 AMM 57-54-000-8.
- [SDR DL72S010897](https://openairdocs.org/sdr/DL72S010897.md): Valve · overheated · Jun 3, 2001 · N529DA · Boeing 727232 · Cabin Pressure Control System
  > RT PACK OVERHEAT. CREW OBSERVED LIGHT HAZE IN CABIN. REPLACED RT PACK VALVE AND COALESCER BAGS.
- [SDR DL72S010784](https://openairdocs.org/sdr/DL72S010784.md): Light · inoperative · May 16, 2001 · N529DA · Boeing 727232 · Emergency Lighting
  > AIRSTAIR LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S010609](https://openairdocs.org/sdr/DL72S010609.md): Switch · failed · Apr 13, 2001 · N529DA · Boeing 727232 · Fire Detection
  > ABORTED T/O AT 100 KTS DUE TO APU FIRE WARN BELL/LIGHT. FOUND APU FIRE PUSH/PULL SWITCH BAD. REMOVED AND REPLACED SWITCH. OPS CHECKS GOOD.
- [SDR DL72K001391](https://openairdocs.org/sdr/DL72K001391.md): Battery · discharged · Jul 23, 2000 · N529DA · Boeing 727232 · Emergency Equipment
  > AFT FLT ATTENDANT FLASHLIGHT BLINKS EVERY 12 SECONDS. REPLACED BATTERIES.
- [SDR DL72K000956](https://openairdocs.org/sdr/DL72K000956.md): Skin · cracked · May 15, 2000 · N529DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > A CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN AT FS 1210 AND STRINGER 3A ON THE LEFT HAND SIDE. THE CRACK WAS REMOVED WITH A 1.4 X 2.7 CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER ERA 334389-14 AT HMV.
- [SDR DL72K000936](https://openairdocs.org/sdr/DL72K000936.md): Hinge Fitting · corroded · May 8, 2000 · N529DA · Boeing 727232 · Horizontal Stabilizer Structure
  > THE HORIZONTAL STABILIZER REAR SPAR HINGE FITTING LUGS WERE FOUND WORN ON THE LT AND RT I/B LUG FACES. THE LT I/B LUG FACE WAS SPOTFACED 0.010 AND THE RT I/B LUG FACE WAS SPOTFACED 0.015 TO REMOVE THE WEAR. THE LT I/B LUG BORE WAS REAMED TO 2.2345 DIA AND TH
- [SDR DL72K000901](https://openairdocs.org/sdr/DL72K000901.md): Skin · cracked · May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STR 4L LAP JOINT BETWEEN FS 360 AND FS 481. THE LAP JOINT WAS REMOVED AND REPLACED PER ERA 334350-14AD AT HMV.
- [SDR DL72K000900](https://openairdocs.org/sdr/DL72K000900.md): Skin · cracked · May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STR 4R LAP JOINT BETWEEN FS 400 AND FS 420. ERA 334362-14AD AUTHORIZES THE REMOVAL OF THE DAMAGE AND REPAIRS THE DAMAGE PER SRM 53-30-3 FIGURE 5. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000899](https://openairdocs.org/sdr/DL72K000899.md): Skin · cracked · May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND IN THE STR 4R LAP JOINT BETWEEN FS 480 AND FS 500. ERA 334363-14 AUTHORIZES THE DAMAGE TO BE CUT OUT AND REPAIRED PER SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000925](https://openairdocs.org/sdr/DL72K000925.md): Spar · cracked · Apr 29, 2000 · N529DA · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > AT HMV2 FROM N/R 794 - FABBED PER PRI 334389-14 4-27-00/1900, INSTALLED, FABBED ACCESS DOUBLER AND PANEL PER OPN 7951, R/C 994. REMOVED FASTENERS ON STRINGER 6 BELOW ACCESS HOLE TO FOM, FABBED ACCESS PANEL/DOUBLER PER OPN 7951/R/C994.
- [SDR DL72K000829](https://openairdocs.org/sdr/DL72K000829.md): Web · cracked · Apr 28, 2000 · N529DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > VERTICAL WEB----CRACKED RIB CUTOUT-FS 1303 VERT WEB CRACKED AT RT RIB CUTOUT. LT RIB CUTOUT SAME CONDITION. REMOVED SUPPORT BRACKET ABOVE S-DUCT AND BEGAN REMOVING FASTENERS FROM REPAIR AREA. DYE PENNED AREA AND STOP DRILLED CRACKS. CHEMICAL TREATED PER PS
- [SDR DL72K000818](https://openairdocs.org/sdr/DL72K000818.md): Mount · corroded · Apr 27, 2000 · N529DA · Boeing 727232 · Horizontal Stabilizer Structure
  > FACE-CORRODED CENTER AFT MOUNT PAD FOR TENSION TIE PLATE CORRODED ON TOP SURFACE. REMOVED DAMAGE WITHIN LIMITS AS PER SRM 55-30-50 FIG 801D. ROTO PEENED PER PS 900-4- NR 5. OK TO TREAT. REPAIRED PER SRM 55-30-50 FIG 801D.
- [SDR DL72K001988](https://openairdocs.org/sdr/DL72K001988.md): Skin · cracked · Apr 25, 2000 · N529DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, THE COVE SKIN WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT. THE DAMAGE WAS REPAIRED PER 727 M/M 57-52-0, FIG 809 BY REMOVING THE CRACK AND INSTALLING A DOUBLER AND SKIN FILLER.
- [SDR DL72K001984](https://openairdocs.org/sdr/DL72K001984.md): Angle · cracked · Apr 24, 2000 · N529DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, THE AFT SPAR LOWER ANGLE WAS FOUND CRACKED 20, 37, AND 55 INCHES FROM I/B END OF FLAP. A SECTION OF ANGLE WAS REPLACED AND SPLICED IN PER 727 M/M 57-52-0, FIG 802.
- [SDR DL72K000980](https://openairdocs.org/sdr/DL72K000980.md): Skin · damaged · Apr 24, 2000 · N529DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END OF THE MIDFLAP. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.
- [SDR DL72K000979](https://openairdocs.org/sdr/DL72K000979.md): Skin · damaged · Apr 24, 2000 · N529DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.
- [SDR DL72K000763](https://openairdocs.org/sdr/DL72K000763.md): Flap Track · corroded · Apr 20, 2000 · N529DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL OF THE I/B FLAP, I/B TRACK, SEVERAL AREAS EXCEEDED APPROVED LIMITS FOR WEAR. AREAS INCLUDED MLG BEAM ATTACH BOLT HOLES, NOTCHES, AND SPOTFACES, THE SPOILER BEAM ATTACH BOLT HOLES, THE MLG DOOR FWD AND AFT HINGE FITTING HOLES, THE SPLICE PLATE
- [SDR DL72K000760](https://openairdocs.org/sdr/DL72K000760.md): Skin · cracked · Apr 20, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THREE CRACKS WERE FOUND IN THE STR 4L LAP JOINT IN THE LOWER SKIN BETWEEN FS 380 AND FS 480. THE LAP JOINT WAS REPLACED FROM FS 360 TO FS 480 PER ERA 334350-14AD AT HMV.
- [SDR DL72K000761](https://openairdocs.org/sdr/DL72K000761.md): Flap Track · corroded · Apr 19, 2000 · N529DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY AT BF GOODRICH, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS, AND TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. DIME
- [SDR DL72K000924](https://openairdocs.org/sdr/DL72K000924.md): Skin · cracked · Apr 18, 2000 · N529DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > AT HMV2 FOUND SKIN CRACKED, LT SIDE VERT STAB AT FRONT SPAR. SKIN HAS TWO CRACKS ABOVE FS 1210, W/W N/R 1080. REMOVED DAMAGE PER DRD 55-30-3D, HFEC INSP PER DRD 55-30-3D NO DISCREPANCIES FOUND IN THIS AREA, REMOVED DAMAGE PER PRI 334389-14 DATED 4-27-00/190
- [SDR DL72K000857](https://openairdocs.org/sdr/DL72K000857.md): Rib · cracked · Apr 18, 2000 · N529DA · Boeing 727232 · Leading Edge Devices
  > AT HMV, THE RIB OF THE NR 2 SLAT WAS FOUND CRACKED JUST O/B OF ANTI-ICE DUCT. REMOVED DAMAGE AND MADE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER PER MM 57-54-0 FIG 814.
- [SDR DL72K000827](https://openairdocs.org/sdr/DL72K000827.md): Angle · bent · Apr 18, 2000 · N529DA · Boeing 727232 · Engine Cowling System
  > AT HMV THE NBR 2 ENG FWD RT COWL CONTACT ANGLE WAS BENT AT THE 5 O''CLOCK POS AT STA 1351. TRIMMED WORN CAP FLANGE, FABRICATED REPAIR ANGLE PER 53-11-0, VERIFIED 2024-T4 HARDNESS TEST, INSTALLED REPAIR PER 53-11-0.
- [SDR DL72K000926](https://openairdocs.org/sdr/DL72K000926.md): Splice · corroded · Apr 17, 2000 · N529DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > AT HMV2, FOUND SPLICE STRAP CORRODED FS 970 - 990 STR 29R. REMOVED CORR PER SRM 51-10-6 & COMMON FASTENERS THRU SKIN FOR FURTHER EVAL, REMOVED RT SIDE OF REPAIR ANGLE, CLEANED/REMOVED ALL CORROSION PER SRM 51-10-6, WITHIN LIMITS PER 53-10-110, ROTO PEENED ARE
- [SDR DL72K000351](https://openairdocs.org/sdr/DL72K000351.md): Battery · discharged · Feb 21, 2000 · N529DA · Boeing 727232 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT FLASHING. REPLACED BATTERY PACK.
- [SDR DL72K000332](https://openairdocs.org/sdr/DL72K000332.md): Latch Roller · out of adjust · Feb 17, 2000 · N529DA · Boeing 727232 · Passenger/Crew Doors
  > ON TAKEOFF ROLL, L-1 DOOR LIGHT ILLUMINATED AND F/A NOTICED DOOR HANDLE MOVED AND GAP WAS SEEN UNDER DOOR. REPLACED GUIDE ARMS, FOUND DOOR LATCH ROLLER OVER CENTER RIGGING OUT OF ADJUSTMENT. ADJUSTED SAME AND RIGGED DOOR. OP CHECKS GOOD.
- [SDR DL72K982304](https://openairdocs.org/sdr/DL72K982304.md): Skin · dented · Nov 5, 1998 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED JUST ABOVE STRINGER 21R BETWEEN FS 1166 AND 1183. THE DENT WAS CUT OUT 2 X 7.25, REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366004-14, REV B.
- [SDR DL72K982236](https://openairdocs.org/sdr/DL72K982236.md): Fitting · cracked · Oct 29, 1998 · N529DA · Boeing 727232 · Leading Edge Slat Actuator
  > O/B SUPPORT FOR ACTUATOR FITTING LOBE CRACKED AT NR 7 SLAT. REPAIRED PER MM 57-42-0.
- [SDR DL72S982193](https://openairdocs.org/sdr/DL72S982193.md): Skin · cracked · Oct 21, 1998 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A 1 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT. AN EXISTING EXTERNAL DOUBLER REPAIR WAS LOCATED MIDWAY BETWEEN THE UPPER HINGE CUTOUT ANDTHE LOWER HINGE CUTOUT. THE UPPER HINGE CRACK WAS REPAIRED PER SRM 53-30-3,
- [SDR DL72S982180](https://openairdocs.org/sdr/DL72S982180.md): Skin · corroded · Oct 21, 1998 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 1070-109, STRG 28R, SKIN CORROSION CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND CORRODED IN TWO AREAS NEAR S-28R BETWEEN FS 1070 AND 1091. THE CORRODED AREAS WERE CUTOUT WITH A 14.25 BY 3.25 CUTUOUT AND A.75 BY 1.5 CUTOUT. BOTH CUTOUTS WERE
- [SDR DL72S982153](https://openairdocs.org/sdr/DL72S982153.md): Blkhd Stiffener · cracked · Oct 16, 1998 · N529DA · Boeing 727232 · Fuselage Main, Bulkhead
  > THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 36.83 WAS FOUND WITH TYPICAL CRACKING AT WL 240. THE CRACKED STIFFENER WAS REPAIRED PER BAC S/B 727-53-0192 AND DOCUMENTED PER ER/A 365894-14.
- [SDR DL72S982208](https://openairdocs.org/sdr/DL72S982208.md): Panel · cracked · Oct 14, 1998 · N529DA · Boeing 727232 · Elevator, Plate/Skin
  > A 1.25 INCH CRACK AT NR 1 RT BALANCE BOARD ACCESS PANEL O/B EDGE (MARKED).
- [SDR DL72S982207](https://openairdocs.org/sdr/DL72S982207.md): Access Panel · cracked · Oct 14, 1998 · N529DA · Boeing 727232 · Elevator, Plate/Skin
  > TWO INCH CRACK IN NR 2 LT BALANCE BOARD ACCESS PANEL AT O/B EDGE (MARKED). INSTALLED REPAIR DOUBLER PER SRM 55-20-3 FIG 5.
- [SDR DL72S982174](https://openairdocs.org/sdr/DL72S982174.md): Skin · cracked · Oct 11, 1998 · N529DA · Boeing 727232 · Elevator, Plate/Skin
  > 1 INCH HOLE WITH CRACKS AT LT ELEVATOR UPPER SKIN AT INBD END. REPAIRED PER 727 SRM 55-20-3 FIG 4.
- [SDR DL72S981616](https://openairdocs.org/sdr/DL72S981616.md): Battery Pack · discharged · Aug 6, 1998 · N529DA · Boeing 727232 · Emergency Lighting
  > ALL 1ST CABIN SEAT MOUNTED EMERGENCY EXIT LIGHT AND ROWS 10 AND 11 EMERGENCY EXIT PATH LIGHTS INOP DURING STBY POWER CHECK. REPLACED BATTERY PACK AND BATTERY RACK OPS CKS OK.
- [SDR DL72S980879](https://openairdocs.org/sdr/DL72S980879.md): Rib · cracked · Apr 24, 1998 · N529DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON E2 LETTER CK, 2 CRACKS IN NR 7 SLAT NOSE RIB AT THE OUTBD SIDE OF THE ACTUATOR. REPAIRED PER MM 57-54-0.
- [SDR DL72S972594](https://openairdocs.org/sdr/DL72S972594.md): Light · inoperative · Dec 10, 1997 · N529DA · Boeing 727232 · Emergency Lighting
  > AFT OUTBOARD EMERGENCY FLASHLIGHT IS NOT FLASHING. REPLACED FLASHLIGHT ASSY AND BREAKAWAY BAND.
- [SDR DL72S972396](https://openairdocs.org/sdr/DL72S972396.md): Skin · cracked · Nov 17, 1997 · N529DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND.25 INCH CRACK IN A/C SKIN LEFT FWD OF A/C JUST AFT OF THE DOOR. REPAIRED PER SRM 53-30-03.
- [SDR DL72S972299](https://openairdocs.org/sdr/DL72S972299.md): Battery Pack · discharged · Nov 9, 1997 · N529DA · Boeing 727232 · Emergency Lighting
  > AFT TWO EXTERNAL EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.
- [SDR DL72S971857](https://openairdocs.org/sdr/DL72S971857.md): Rib · cracked · Sep 23, 1997 · N529DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING E 1 LETTER CHECK.0625 INCH CRACK PAST STOP DRILL AT NR 4 SLAT O/B ACTUATOR MOUNT RIB. REPAIR PER MM 57-54-0.
- [SDR DL72S971475](https://openairdocs.org/sdr/DL72S971475.md): Fire Loop · malfunctioned · Jul 28, 1997 · N529DA · Boeing 727232 · Fire Detection
  > ON CLIMBOUT, NR 3 ENGINE FIRE LIGHT ILLUMINATED. FIRE DETECTOR SWITCH IN A-MODE AS PER MCO. ALL OTHER ENGINE INDICATIONS NORMAL. SHUTDOWN ENGINE AS PER POM, FIRED BOTH BOTTLES AS PER POM AND FIRE LIGHT REMAINED ON UNTIL LANDING. TESTED FIRE LIGHT AFTER I
- [SDR DL72S971110](https://openairdocs.org/sdr/DL72S971110.md): Fan · shorted · Jun 8, 1997 · N529DA · Boeing 727232 · Air Distribution Fan
  > STRONG ELECTRICAL FUMES IN ACFT, COINCIDING WITH GASPER FAN C/B POPPED. REPLACED GASPER FAN, CKS OK.
- [SDR DL72S970824](https://openairdocs.org/sdr/DL72S970824.md): Wire Harness · chafed · May 2, 1997 · N529DA · Boeing 727232 · Hydraulic System, Auxiliary
  > DURING PREFLIGHT CK, STANDBY HYD PUMP WAS INOPERATIVE WITH THE ASSOCIATED CIRCUIT BREAKER POPPED. FOUND THE WIRE HARNESS TO THE PUMP HAD CHAFED ON A STRINGER IN THE LT 48 SECT BEHIND THE PUMP, ALSO CAUSING DAMAGE TO THE STRINGER. THE PUMP WAS REPLACED, THE W
- [SDR DL72S970402](https://openairdocs.org/sdr/DL72S970402.md): Skin · cracked · Mar 4, 1997 · N529DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > FOUND A 1 INCH CRACK ON THE VERTICAL STAB SKIN LT SIDE BELOW LOWER VORTEX GENERATOR. REPAIRED PER MM 55-30-0.
- [SDR DL72S970401](https://openairdocs.org/sdr/DL72S970401.md): Web · cracked · Mar 4, 1997 · N529DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND LOWER TORQUE BOX VERTICAL WEB CRACKED IN TWO PLACES STA 1236 AND STA 1226 RIGHT SIDE. REPAIRED PER M/M 53-11-0.

Next page: https://openairdocs.org/deregistered/N529DA-2014-10-27/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 = 'N529DA' AND deregistration_id = 'N529DA-2014-10-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N529DA-2014-10-27/reports

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