# Service difficulty reports: N532DA, cancelled Aug 25, 2004

A list on [N532DA, cancelled Aug 25, 2004](https://openairdocs.org/deregistered/N532DA-2004-08-25.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 DL72S021049](https://openairdocs.org/sdr/DL72S021049.md): Battery · weak · Sep 8, 2002 · N532DA · Boeing 727232 · Emergency Lighting
  > R1 OVERHEAD EMERGENCY LIGHT BARELY ILLUMINATES REPLACED BATTERIES OPS CK OK
- [SDR DL72S021034](https://openairdocs.org/sdr/DL72S021034.md): Web · cracked · Sep 3, 2002 · N532DA · Boeing 727232 · Wing Structure
  > CRACK ON O/B WEB OF #1 SLAT ACT. MOUNT BRACKET REPAIR PER M/M 57-20-021-8
- [SDR DL72S020200](https://openairdocs.org/sdr/DL72S020200.md): Battery Pack · discharged · Feb 18, 2002 · N532DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND EMERGENCY CEILING LIGHTS AT ROW 26 INOP. REPLACED BATTERY PACK, CHECKS GOOD.
- [SDR DL72S011765](https://openairdocs.org/sdr/DL72S011765.md): Battery · discharged · Nov 5, 2001 · N532DA · Boeing 727232 · Landing Gear Steering System
  > AFT AIRSTAIR EMERGENCY LIGHT VERY DIM. REPLACED BATTERIES.
- [SDR DL72S011441](https://openairdocs.org/sdr/DL72S011441.md): Reservoir · low · Aug 31, 2001 · N532DA · Boeing 727232 · Hydraulic Reservoir, Main
  > RETURNED TO DFW FOR LOW HYDRAULICS FLUID IN SYSTEM A. SERVICED A SYSTEM TO 4.4 GALLONS. INSPECTED ACFT FOR LEAKS, NONE FOUND.
- [SDR DL72S011098](https://openairdocs.org/sdr/DL72S011098.md): Fitting · cracked · Jul 1, 2001 · N532DA · Boeing 727232 · Nacelle/Pylon, Main Frame
  > DURING INSPECTIONS PER AD 97-05-08, CRACKS WERE FOUND IN THE#1 FORWARD ENGINE MOUNT AT HOLES C AND D. THE HOLES WERE OVERSIZED, INSPECTED AND NEW FASTENERS INSTALLED PER ERA 397735-14AD AT HMV.
- [SDR DL72S011090](https://openairdocs.org/sdr/DL72S011090.md): Frame · cracked · Jun 29, 2001 · N532DA · Boeing 727232 · Fuselage Main, Frame
  > DURING HMV A CRACK WAS FOUND IN THE FS 344 FRAME DIRECTLY ABOVE THE L1 DOOR. THE CRACK WAS.5". THE CRACK WAS CUT OUT AND A DOUBLER WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S011089](https://openairdocs.org/sdr/DL72S011089.md): Skin · cracked · Jun 29, 2001 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING AN INSPECTION REQUIRED BY AD 99-04-22 CRACKS WERE FOUND IN THE STR 4R LAP JOINT BETWEEN FS 660 AND 680. THE CRACKS WERE CUT OUT AND AN EXTERNAL REPAIR INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S011087](https://openairdocs.org/sdr/DL72S011087.md): Skin · cracked · Jun 29, 2001 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING THE ACCOMPLISHMENT OF THE INSPECTIONS REQUIRED BY AD 99-04-22, TWO CRACKS WERE FOUND IN THE STR 4L LAP JOINT BETWEEN FS 380 AND 400. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3, FIGURE 5. THE CRACKS WERE FOUND AT HMV.
- [SDR DL72S011036](https://openairdocs.org/sdr/DL72S011036.md): Skin · corroded · Jun 22, 2001 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FS1009 BETWEENSTR 29L AND 28R. THE SKIN WAS REPAIRED SIMILIAR TO THAT OF SRM 53-30-3, FIGURE 3A. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S011035](https://openairdocs.org/sdr/DL72S011035.md): Skin · corroded · Jun 22, 2001 · N532DA · Boeing 727232 · Fuselage Main, Keel
  > THE FUSELAGE SKIN AND STRINGER WERE FOUND CORRODED AT FS 950E AND STR 29R. THE STRINGER WAS CUT AT FS 950D +10 AND REMOVED TO THE AFT END OF THE PART. A NEW SECTION WAS SPLICED IN. AN EXTERNAL DOUBLER AND TRIPLE WERE USED TO REPAIR THE SKIN. TH
- [SDR DL72S010948](https://openairdocs.org/sdr/DL72S010948.md): Skin · cracked · Jun 12, 2001 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE STR 26L LAP JOINT BETWEEN FS 620 AND 640. THE CRACK WAS REMOVED AND REPIARED PER SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S010924](https://openairdocs.org/sdr/DL72S010924.md): Fastener · loose · May 31, 2001 · N532DA · Boeing 727232 · Leading Edge Devices
  > NR 2 SLAT I/B ACTUATOR RIB FASTENERS LOOSE. REQUIRING A SKIN SPLICE PER 727 SRM CH 57-54-000-8 FIG 801. ACTUAL DAMAGE NOT RELATED TO METHOD USED TO GAIN ACCESS. REASON FOR MAJOR REPAIR CLASSIFICATION UNKNOWN.
- [SDR DL72S010875](https://openairdocs.org/sdr/DL72S010875.md): Flap Track · corroded · May 31, 2001 · N532DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL THE INBD FLAP, INBD TRACK WAS FOUND WITH CORROSION AND WEAR EXCEEDING THE ALLOWABLE LIMITS. REPAIRED PER ER/A 401900-14AD AND BF GOODRICH DOCUMENT 23-0682.
- [SDR DL72S010874](https://openairdocs.org/sdr/DL72S010874.md): Flap Track · corroded · May 31, 2001 · N532DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL THE INBD FLAP, INBD TRACK ASSY WAS FOUND WITH CORROSION AND WEAR. DAMAGE EXCEEDED ALLOWABLE LIMITS AT THE MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, SPOILER BEAM ATTACH HOLES, MLG DOOR FWD AND AFT HINGE FITTING ATTACH HOLES, HINGE SUPPORT
- [SDR DL72S020894](https://openairdocs.org/sdr/DL72S020894.md): Angle · cracked · May 30, 2001 · N532DA · Boeing 727232 · Trailing Edge Flaps
  > AFT CHORD ANGLE CRACKED 22 INCHES AND 37 INCHES FROM THE I/B END. REPAIRED NR 3 FLAP CHORD ANGLE.
- [SDR DL72S011017](https://openairdocs.org/sdr/DL72S011017.md): Frame · worn · May 30, 2001 · N532DA · Boeing 727232 · Fuselage Main, Frame
  > AT HMV FOUND FRAME WORN STA.1342 6,O-CLOCK POSITION FRAME FOR FWD END OF #2 ENG COWL'S. CORR: REMVD DAMAGE PER MM 53-11-000-8,FABD REPAIR ANGLE PER MM 53-11-000-8,2054-0-.071,DRILLED DOUBLER PER MM 53-11-000-8,FABD FILLER,OK INS
- [SDR DL72S010908](https://openairdocs.org/sdr/DL72S010908.md): Spar · cracked · May 29, 2001 · N532DA · Boeing 727232 · Wing Spar
  > AT HMV FOUND FAST SPAR LWR CHORD - CRACK, REPAIR LOOSE LOC AT LWR END OF NR 7 SPOILER ACT FITTING. REMOVED NR 6/7 SPOILER MOUNT ARM, REMOVED DAMAGED SECTION OF BEAM PER MM 57-55-00-08 FIG 805, FABD AND DRILLED UP PARTS PER MM 57-55-00-08 FIG 805, OK TO INSTAL
- [SDR DL72S010648](https://openairdocs.org/sdr/DL72S010648.md): Light · inoperative · Apr 19, 2001 · N532DA · Boeing 727232 · Emergency Lighting
  > 1R DOOR EMERGENCY LIGHT WOULD NOT COME ON WITH TEST. REPLACED EMER LIGHT ASSY.
- [SDR DL72S002030](https://openairdocs.org/sdr/DL72S002030.md): Battery · inoperative · Oct 16, 2000 · N532DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT NOT HOLDING CHARGE. REPLACED BATTERY.
- [SDR DL72S001165](https://openairdocs.org/sdr/DL72S001165.md): Beam · cracked · Jun 15, 2000 · N532DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > HFEC BOLT HOLE INSPECTION OF TWO FASTENERS COMMON TO AN INTERCOSTAL AND THE FWD CAP OF THE FS 1183 BULKHEAD VERTICAL BEAM AT RBL 17.8 AND WL 273.25 REVEALED CRACK INDICATIONS. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK INDICATIONS WITH AN ADDITIONAL INSURAN
- [SDR DL72S001107](https://openairdocs.org/sdr/DL72S001107.md): Actuator · leaking · Jun 7, 2000 · N532DA · Boeing 727232 · Leading Edge Slat Actuator
  > ON T/O ROLL IN MSO, BOTH SYS A HYDRAULIC LOW PRESSURE LIGHTS CAME ON AT APROX 100 KIAS, SYS A QTY RAPIDLY WENT TO ZERO. T/O CONTINUED CHECKLIST C/W, UNEVENTFUL LANDING IN MSO. MTC FOUND NR 7 SLAT ACTUATOR LEAKING. REPLACED SAME.
- [SDR DL72S000672](https://openairdocs.org/sdr/DL72S000672.md): Acm · malfunctioned · Apr 7, 2000 · N532DA · Boeing 727232 · Cabin Cooling System
  > LEFT PACK ON DESCENT INCREASED TO 90 DEGREES AND SMOKE WAS EXHAUSTING BRIEFLY INTO THE CABIN WITH A SMELL. REDUCING MANUALLY TO 50 DEGREES STOPPED SMOKE. MTC ATL NOTIFIED IN FLIGHT. REMAINDER OF FLIGHT NORMAL. RAN LEFT PACK IN AUTO AND MANUAL THROUGH FULL
- [SDR DL72S992255](https://openairdocs.org/sdr/DL72S992255.md): Brake · failed · Oct 11, 1999 · N532DA · Boeing 727232 · Landing Gear Brake System
  > ON LANDING, NR2 BRAKE LOCKED AND BLEW NR 2 MAIN TIRE. REPLACED NR 2 BRAKE, NR 1 AND NR 2 WHEEL ASSY. T/S NR 2 WHEEL ANTI-SKID SYSTEM. OPERATION NORMAL.
- [SDR DL72S991976](https://openairdocs.org/sdr/DL72S991976.md): Battery · discharged · Sep 6, 1999 · N532DA · Boeing 727232 · Emergency Lighting
  > L-2 DOOR OVERHEAD EMERGENCY LT WOULD NOT TEST REPLACED BATTERY PACK.
- [SDR DL72S990803](https://openairdocs.org/sdr/DL72S990803.md): Skin · cracked · Apr 12, 1999 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-481 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. 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. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN 3 CONSE
- [SDR DL72S990705](https://openairdocs.org/sdr/DL72S990705.md): Frame · cracked · Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV2 CORROSION VISIT NRC 134,.375 INCH VISIBLE CRACK LT CUTOUT FRAME, AFT ENTRY DOORWAY AT SECOND FROM UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990631](https://openairdocs.org/sdr/DL72S990631.md): Web · cracked · Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON MV2 CK,.5 INCH CRACK IN STA 1303 WEB LT LOWER CORNER. REPAIRED PER SRM 53-10-4.
- [SDR DL72S990630](https://openairdocs.org/sdr/DL72S990630.md): Web · crack · Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON MV2 CK,.5 INCH CRACK STA 1303 WEB RT AT LOWER RT CORNER. REF NR 143. FOUND ON MV2 CK,.5 INCH CRACK STA 1303 WEB RT AT THE CUTOUT FOR THE STRINGER. REF NR 142. BOTH CRACKS REPAIRED WITH THE SAME DOUBLER PER SRM 53-10-4.
- [SDR DL72S990722](https://openairdocs.org/sdr/DL72S990722.md): Stringer · cracked · Mar 22, 1999 · N532DA · Boeing 727232 · Wing, Longeron/Stringer
  > REPAIRED CRACK AT UPPER STRINGER TO RIB FASTENER HOLE AT RT WING STA 656.50 STR 14 PER M/M 57-13-0.
- [SDR DL72S982614](https://openairdocs.org/sdr/DL72S982614.md): Doubler · cracked · Dec 21, 1998 · N532DA · Boeing 727232 · Leading Edge Slat Actuator
  > WING FIXED LEADING EDGE, NR 8 SLAT ACTUTOR SUPPORT BRACKET REPAIR FOR CRACKED DOUBLER. THE OUTBD SUPPORT BRACKET DOUBLER FOR THE NR 8 SLAT WAS FOUND CRACKED. THE INBD AND OUTBD ACTUATOR BRACKETS FOR THE NR 8 SLAT WERE REPAIRED/MODIFIED PER THE REQUIREMENTS O
- [SDR DL72S981648](https://openairdocs.org/sdr/DL72S981648.md): Wire · broken · Aug 10, 1998 · N532DA · Boeing 727232 · Light System Wiring
  > EMERGENCY TRACK LIGHTING SECTION IN FWD COACH AREA DOES NOT ILLUMINATE. REPAIRED SECTION OF WIRE.
- [SDR DL72S980596](https://openairdocs.org/sdr/DL72S980596.md): Cowl · cracked · Mar 17, 1998 · N532DA · Boeing 727232 · Engine Cowling System
  > FOUND.75 INCH CRACK NR 2 ENG NOSE COWL 10 INCH AFT OF NOSE RING 3.00 POS. REPAIRED PER MM 54-30-0 P 801.
- [SDR DL72S972702](https://openairdocs.org/sdr/DL72S972702.md): Indicator · failed · Dec 22, 1997 · N532DA · Boeing 727232 · Engine Oil Indicating System
  > SMOKE IN THE COCKPIT, FLT DIVERTED TO BHM. MTC FOUND NR 3 ENG OIL QTY IND TO BE SOURCE OF SMOKE. REPLACED INDICATOR.
- [SDR DL72S972520](https://openairdocs.org/sdr/DL72S972520.md): Torque Box · cracked · Dec 1, 1997 · N532DA · Boeing 727232 · Fuselage Main, Structure
  > THE TORQUE BOX WAS FOUND WITH A CRACKED UPPER CHORD AND A CRACKED FS 1263 UPPER BEAM ANGLE AND CHANNEL. THE CRACKED MEMBERS WERE REPLACED OR REPAIRED PER S/B 53-0129. ER/A 363340-14AD WAS ISSUED TO DOCUMENT THE DAMAGE AND CONTROL THE REPAIR METHOD.
- [SDR DL72S972514](https://openairdocs.org/sdr/DL72S972514.md): Skin · cracked · Dec 1, 1997 · N532DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON D1 LETTER CK, ONE 3 AND ONE 3.5 INCH CRACK IN SLAT LOWER SKIN OF NR 6 L/E SLAT AT O/B T/E. REPAIRED PER MM 57-54-0.
- [SDR DL72S972433](https://openairdocs.org/sdr/DL72S972433.md): Battery · discharged · Nov 21, 1997 · N532DA · Boeing 727232 · Emergency Lighting
  > AT LAYOVER, FOUND L2 DOOR EMERGENCY EXIT POWER PACK INOP. REPLACED BATTERIES.
- [SDR DL72S972080](https://openairdocs.org/sdr/DL72S972080.md): Oven · failed · Oct 17, 1997 · N532DA · Boeing 727232 · Buffet/Galleys
  > FWD GALLEY OVEN FIRE IN FLT AFTER DEPARTURE. PERFORMED SMOKE/ID, RMVAL AND CLEAN UP CHECKLIST. RETURNED TO LAND AT PHX. REMOVED OVEN, INSPECTED WIRING AND COMPARTMENT, ALL CKD OK. REPLACED OVEN AS PRECAUTIONARY.
- [SDR DL72S971868](https://openairdocs.org/sdr/DL72S971868.md): Skin · erosion · Sep 5, 1997 · N532DA · Boeing 727232 · Elevator, Plate/Skin
  > THE RT LOWER ELEVATOR SKIN HAS A 6 SPAN X 7 CHORD HOLE 12 O/B OF THE FUSELAGE. THE HOLE WAS CAUSED WHEN A DOUBLER PEELED BACK INTO THE AIRSTREAM. THE DEPARTING PIECE PUNTURED THE SKIN APPROXIMATELY 8 INCHES AFT OF THE HOLE. THE PUNCTURE IS 1.0 DIA, THE SKIN
- [SDR DL72S970037](https://openairdocs.org/sdr/DL72S970037.md): Skin · corroded · Dec 12, 1996 · N532DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND IN THREE AREAS AROUND THE RAM AIR ACTUATOR ACCESS DOOR. THE DAMAGED AREAS MEASURE 3.5 BY 4.375 IN THE AFT RT CORNER, 7.375 BY 3.625 ON THE FWD LT SIDE AND 3.5 BY 4.75 ON THE AFT LT SIDE. THE DAMAGE WAS REPAIRED WITH TITANIUM DOUBLERS AND
- [SDR DL72S960863](https://openairdocs.org/sdr/DL72S960863.md): Light Panel · smoking · Apr 15, 1996 · N532DA · Boeing 727232 · Flight Compartment Lighting
  > PRIOR TO DEPARTURE WITH PSGRS ON BOARD, B-SYS STBY HYD PANEL WAS SMOKING. PSGRS WERE DEPLANED IN A NORMAL MANNER. FOUND BACKGROUND LIGHTING PANEL DAMAGED. REPLACED PANEL ASSEMBLY.
- [SDR DL72S960659](https://openairdocs.org/sdr/DL72S960659.md): Overheat Sensor · out of position · Mar 26, 1996 · N532DA · Boeing 727232 · Overheat Detection
  > LOWER AFT BODY OVERHEAT LIGHT ILLUM. C/W PROM LIGHT WENT OUT WHEN LT PACK AND BLEED TURNED OFF. REPOS OVERHEAT SENSOR IN 48 SECTION. RAN ENGINE WITH NO OVERHEAT IND.
- [SDR DL72S960680](https://openairdocs.org/sdr/DL72S960680.md): Angle · cracked · Mar 13, 1996 · N532DA · Boeing 727232 · Leading Edge Devices
  > A CRACK WAS FOUND 32.5 FROM I/B END ON LOWER AFT COVE SKIN ATTACH ANGLE BELOW ANTI-ICE DUCT. REPAIRED AS PER MM 57-54-0 FIG 805A, FOR NR 8 L/E SLAT.
- [SDR DL72S960567](https://openairdocs.org/sdr/DL72S960567.md): Web · cracked · Mar 13, 1996 · N532DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON B2 LETTER CHECK, LOWER RT TORQUE BOX LIGHTENING HOLE WEB CRACKED FS 1243. REPAIRED PER MM 53-11-0.
- [SDR DL72S960436](https://openairdocs.org/sdr/DL72S960436.md): Light · inoperative · Feb 27, 1996 · N532DA · Boeing 727232 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT INOP AT AFT LT DOOR IN EMERGENCY. REPLACED LIGHT ASSY.
- [SDR DL72S954696](https://openairdocs.org/sdr/DL72S954696.md): Gearbox · failed · Dec 13, 1995 · N532DA · Boeing 727232 · Turbine Engine Accessory Drive
  > NR 2 ENG FAILED ON TAKEOFF. AFTER RETURNING TO YVR, CNTR MAINT FOUND THE NR 2 ENGINE GEARBOX HAD COME APART. REPLACED ENGINE AND ROUTED TO SHOP.
- [SDR DL72S953877](https://openairdocs.org/sdr/DL72S953877.md): Shim · misalignment · Sep 26, 1995 · N532DA · Boeing 727232 · Trailing Edge Flaps
  > DURING ROUTINE INSECTION, THE LAMINATED SHIM INSTALLED ON THE RIGHT WING I/B FLAP TRACK WAS FOUND TO HAVE MIGRATED FROM LEFT TO RIGHT. COMPLYING WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED, REINSTALLED AND THE ATTACHMENTS WILL BE RETORQUED. INSPECT
- [SDR DL72S953521](https://openairdocs.org/sdr/DL72S953521.md): Eel Sign · broken · Aug 27, 1995 · N532DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FOUND BROKEN AND HANGING ON SIDEWALL PANEL SEAT ROW 20ABC. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.
- [SDR DL72S953520](https://openairdocs.org/sdr/DL72S953520.md): Eel Battery Pack · discharged · Aug 27, 1995 · N532DA · Boeing 727232 · Emergency Lighting
  > DURING LAYOVER, FOUND THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. RELAMPED, CLEANED CONNECTIONS AND REPLACED BATTERY PACK. OPERATION NORMAL.
- [SDR DL72S953393](https://openairdocs.org/sdr/DL72S953393.md): Angle · cracked · Aug 14, 1995 · N532DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING B-1 LETTER CHECK,.5 INCH CRACK NR 3 SLAT COVE ANGLE BELOW ANTI-ICE DUCT. REPAIRED PER MM 57-54-0 PG 807A.

Next page: https://openairdocs.org/deregistered/N532DA-2004-08-25/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 = 'N532DA' AND deregistration_id = 'N532DA-2004-08-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N532DA-2004-08-25/reports

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