# Service difficulty reports: N528DA, cancelled Mar 3, 2003

A list on [N528DA, cancelled Mar 3, 2003](https://openairdocs.org/deregistered/N528DA-2003-03-03.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 · 98 reports

- [SDR DL72S011977](https://openairdocs.org/sdr/DL72S011977.md): Wire · damaged · Dec 25, 2001 · N528DA · Boeing 727232 · Light System Wiring
  > SEAT 31 DEF EMERGENCY LIGHT INOP. REPAIRED WIRING.
- [SDR DL72S011854](https://openairdocs.org/sdr/DL72S011854.md): Battery · discharged · Nov 24, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE 1L DOOR INOP.___BATTERIES DEAD. _REPLACED BATTERIES IN LIGHT ASSY. OP CKS NML.
- [SDR DL72S011849](https://openairdocs.org/sdr/DL72S011849.md): Light · inoperative · Nov 23, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER CENTER AISLE BETWEEN 2L AND 2R DOORS INOP. RELAMPED LIGHT ASSY AND OPERATION NORMAL.
- [SDR DL72S011242](https://openairdocs.org/sdr/DL72S011242.md): Skin · cracked · Jul 26, 2001 · N528DA · Boeing 727232 · Fuselage Structure (General)
  > .25 INCH CRACK IN EMPENAGE SKIN AT AFT I/B CORNER OF GROUND AIR CONNECTION ACCESS DOOR CUTOUT. REPAIRED PER M/M 53-30-000-8 PG 2.
- [SDR DL72S010800](https://openairdocs.org/sdr/DL72S010800.md): Rack · inoperative · May 19, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > AFT CTR AISLE EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERY, OPER NOW OK.
- [SDR DL72S010799](https://openairdocs.org/sdr/DL72S010799.md): Rack · inoperative · May 19, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > MID CABIN CTR AISLE EXIT LIGHT INOP. REPAIRED CONNECTOR. REPLACED BATTERY AND RACK.
- [SDR DL72S010546](https://openairdocs.org/sdr/DL72S010546.md): Door Frame · cracked · Apr 2, 2001 · N528DA · Boeing 727232 · Fuselage Main, Structure
  > INSPECTION OF THE C1 DOOR OPENING FWD FRAME AT FS 560 PER AD 99-23-13 REVEALED 3 CRACKS IN THE WEB (1 BELOW THE NR 4 STOP AND 2 BELOW THE NR 1 STOP). THE WEB WAS CUT AT THE NR 6 STOP AND THE UPPER SECTION WITH THE CRACKS REMOVED. WEB REMOVAL REVEALED SEVER
- [SDR DL72S010510](https://openairdocs.org/sdr/DL72S010510.md): Mount · damaged · Mar 27, 2001 · N528DA · Boeing 727232 · Engine Mount Section
  > INSPECTION OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT ATTACH FITTING HOLES PER AD 97-05-08 FOUND 2 HOLES OUT OF LIMITS. THE HOLES WERE HFEC INSPECTED TO ENSURE NO CRACKS AND OVERSIZED TO THE NEXT ALLOWABLE SIZE OF FED EX S/B 2000-5410A01. LARGER DIAMETER B
- [SDR DL72S010040](https://openairdocs.org/sdr/DL72S010040.md): Battery · discharged · Jan 8, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > OVERHEAD FWD EMERGENCY LIGHT AT ROW 13 INOP. REPLACED BATTERY PACK. CHECKS NORMAL.
- [SDR DL72S010017](https://openairdocs.org/sdr/DL72S010017.md): Battery Pack · inoperative · Jan 4, 2001 · N528DA · Boeing 727232 · Emergency Lighting
  > OVERWING EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK AND TRAY, CKS GOOD.
- [SDR DL72S001773](https://openairdocs.org/sdr/DL72S001773.md): Light · inoperative · Sep 14, 2000 · N528DA · Boeing 727232 · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT RACK ASSY.
- [SDR DL72S001693](https://openairdocs.org/sdr/DL72S001693.md): Compensator · leaking · Sep 1, 2000 · N528DA · Boeing 727232 · Crew Oxygen System
  > CREW O2 DEPLEATED IN FLIGHT GAUGE READS 150 PSI. REPLACED CREW O2 BOTTLE AND FOUND THERMAL COMPENSATOR LEAKING. REPLACED THERMAL COMPENSATOR, LEAK CKS OK.
- [SDR DL72S001382](https://openairdocs.org/sdr/DL72S001382.md): Transformer · shorted · Jul 21, 2000 · N528DA · Boeing 727232 · Exterior Lighting
  > NOSE WHEEL ILLUMINATION LIGHTS INOP ON WALKAROUND. FOUND TRANSFORMER BUS NR 1 C/B BAD TRANSFORMER T50 HIGH COIL/LOW COIL SHORTED AND WIRING DAMAGED BETWEEN TRANSFORMER AND C/B C354. REPLACED CIRCUT BREAKER, TRANSFORMER AND REPLACED WIRE 455-20.
- [SDR DL72S000982](https://openairdocs.org/sdr/DL72S000982.md): Light · inoperative · May 19, 2000 · N528DA · Boeing 727232 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS ARE OUT. REPLACED BATTERY PACK AND CHARGER.
- [SDR DL72S000648](https://openairdocs.org/sdr/DL72S000648.md): Battery · discharged · Apr 6, 2000 · N528DA · Boeing 727232 · Emergency Equipment
  > EMERGENCY FLASHLIGHT BATTERY WEAK. REPLACED BATTERY.
- [SDR DL72S992690](https://openairdocs.org/sdr/DL72S992690.md): Angle · cracked · Nov 17, 1999 · N528DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 55 FROM I/B END OF FLAP. THE CHORD ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72S992422](https://openairdocs.org/sdr/DL72S992422.md): Skin · dented · Nov 2, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED AT FS 354 AT STRINGER 3R. THE DAMAGE WAS REMOVED WITH A 1.0 CUTOUT AND REPAIRED PER ERA 333754-14.
- [SDR DL72S992361](https://openairdocs.org/sdr/DL72S992361.md): Skin · gouged · Oct 25, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS GOUGED AT FS 990 AT STRINGER 24R. REPAIRED PER ERA 333703-14 AT HMV.
- [SDR DL72S992360](https://openairdocs.org/sdr/DL72S992360.md): Skin · cracked · Oct 25, 1999 · N528DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > THE LT SKIN OF THE VERTICAL STABLIZER WAS DAMAGED RESULTING IN A 1.2 X 1.2 CUTOUT BETWEEN STRINGERS 7 AND 8 AT FIN STATION 204. REPAIRED PER ERA 333721-14 AT HMV.
- [SDR DL72S992379](https://openairdocs.org/sdr/DL72S992379.md): Apu · inop · Oct 24, 1999 · N528DA · Boeing 727232 · APU Core Engine
  > DURING HMV CK WORKING MCO 127703001, APU QUIT AT GATE BEFORE PUSHBACK. DURING T/S AND JIC OP 6009 FOUND APU FIRE TEST INOP. ALSO, FOUND FIRE LOOP BROKEN WITH APPARENT HIGH HEAT INDICATION AND SOOT INSIDE APU SHROUD AT INNER EXHAUST DUCT CLAMP. REPLACED APU
- [SDR DL72S992326](https://openairdocs.org/sdr/DL72S992326.md): Fitting · cracked · Oct 22, 1999 · N528DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 4 L/E SLAT I/B ACTUATOR ATTACH FITTING WAS CRACKED 3 EA LOCATION THROUGH AN EXISTING REPAIR. REPAIRED DOUBLER PER M/M 57-54-0 FIG 804. REMOVED CRACKED PLATE, REPLACED CLIP PER 51-00. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-54-0 FIG 804.
- [SDR DL72S992306](https://openairdocs.org/sdr/DL72S992306.md): Rib · cracked · Oct 18, 1999 · N528DA · Boeing 727232 · Leading Edge Devices
  > AT HMV FOUND NR 5 SLAT ACT MOUNT O/B RIB CRACKED. REF N/R 1140 - RIB NR 11 FROM O/B FWD. STOP DRILLED CRACK AND FABBED REPAIR PER MM 57-54-0 PG 805 AND INSTALLED PER SAME.
- [SDR DL72S992262](https://openairdocs.org/sdr/DL72S992262.md): Skin · worn · Oct 12, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WORN AT FS 1100 AND STRINGER 1. REPAIRED PER ERA 333691-14AD.
- [SDR DL72S992689](https://openairdocs.org/sdr/DL72S992689.md): Angle · cracked · Oct 11, 1999 · N528DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 20 FROM I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0, FIG 802.
- [SDR DL72S992388](https://openairdocs.org/sdr/DL72S992388.md): Rib · cracked · Oct 7, 1999 · N528DA · Boeing 727232 · Leading Edge Devices
  > AT HMV, FOUND O/B RIB CRACKED ON NR 7 L/E SLAT AT ACTUATOR FITTING. REMOVED FASTENER AND DOUBLER, FABBED NEW DOUBLER PER MM 57-54-0 FIG 804, AND INSTALLED.
- [SDR DL72S992285](https://openairdocs.org/sdr/DL72S992285.md): Rib · cracked · Oct 7, 1999 · N528DA · Boeing 727232 · Leading Edge Devices
  > RIB CRACKED NR 8 L/E SLAT O/B RIB. FABRICATED DOUBLER, REPAIRED PER M/M 57-54-0 FIG 814.
- [SDR DL72S992284](https://openairdocs.org/sdr/DL72S992284.md): Rib · cracked · Oct 7, 1999 · N528DA · Boeing 727232 · Leading Edge Devices
  > RIB CRACKED 2ND FROM I/B END ON NR 5 L/E SLAT. STOP DRILLED CRACK 2ND FROM I/B RIB ON NR 5 L/E SLAT. DRILLED VP DOUBLER FOR RIB 2ND FROM I/B NR 5 L/E SLAT. TREAT AND PAINT PER P/S 900-2-5. OK INSTALLED REPAIR. INSTALLED REPAIR DOUBLER PER M/M 57-40-0 FIG
- [SDR DL72S992258](https://openairdocs.org/sdr/DL72S992258.md): Bolt · loose · Oct 6, 1999 · N528DA · Boeing 727232 · Spoilers
  > AT HMV, FOUND NR 14 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804.
- [SDR DL72S992257](https://openairdocs.org/sdr/DL72S992257.md): Bolt · loose · Oct 6, 1999 · N528DA · Boeing 727232 · Spoilers
  > AT HMV, FOUND RW NR 12 SPOILER MOUNT BOX I/B LOWER ATTACH BOLT HAS PLAY. REPAIRED PER MM 57-42-0 PG 804.
- [SDR DL72S992256](https://openairdocs.org/sdr/DL72S992256.md): Mount · loose · Oct 6, 1999 · N528DA · Boeing 727232 · Spoilers
  > AT HMV, FOUND NR 13 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804.
- [SDR DL72S991641](https://openairdocs.org/sdr/DL72S991641.md): Bushing · worn · Jul 21, 1999 · N528DA · Boeing 727232 · Fuel Controlling System
  > ON DESCENT INTO BHM, NR 2 THROTTLE RETARDED TO IDLE NR 2 ENG WENT TO HIGH POWER SETTING AND DID NOT RESPOND TO THROTTLE MOVEMENT. ACCOM PRECAUTIONARY ENG SHUTDOWN. OPENED NR 2 ENG COWLING AT GATE AND FOUND THE BUSHING ON THE FUEL CONTROL ROD WORN OUT. REPLA
- [SDR DL72S991549](https://openairdocs.org/sdr/DL72S991549.md): Fitting · cracked · Jul 10, 1999 · N528DA · Boeing 727232 · Altimeter, Barometric/Encoder
  > AT 33,000 FT, THE CAPTAINS AND F/O ALTIMETERS DIFFER BY 200 FT AND F/O ALT STICKS AT 2999. REPLACED NR 2 ALT. FOUND CRACKED DISCONNECT FITTING ON NR 2 ALT. REPLACED FITTING AND PERFORMED LEAK CHECK.
- [SDR DL72S990828](https://openairdocs.org/sdr/DL72S990828.md): Spar · gouged · Apr 13, 1999 · N528DA · Boeing 727232 · Wing Spar
  > INBOARD FWD LWR SIDE OF AUX SPAR GOUGED LEFT SIDE. REPAIRED PER MM 57-43-0 P 801.
- [SDR DL72S990742](https://openairdocs.org/sdr/DL72S990742.md): Skin · cracked · Apr 4, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS IN 6 DIFFERENT FRAME BAYS. THE ENTIRE SKIN LAP WAS CUTOUT TO REMOVE ALL CRACKS AND REPAIRED WITH AN
- [SDR DL72S990711](https://openairdocs.org/sdr/DL72S990711.md): Skin · cracked · Mar 30, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN NEAR FS 486. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED A SINGLE CRACK AT FS 486. THE CRACK WAS ROUTED OUT AND REPAIRED PER B7
- [SDR DL72S990222](https://openairdocs.org/sdr/DL72S990222.md): Batteries · discharged · Feb 3, 1999 · N528DA · Boeing 727232 · Emergency Lighting
  > 2L EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR DL72S981896](https://openairdocs.org/sdr/DL72S981896.md): Rib · cracked · Sep 13, 1998 · N528DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON L/O CK, NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED AT FWD END. REPAIRED PER MM 57-54-0.
- [SDR DL72S981876](https://openairdocs.org/sdr/DL72S981876.md): Door · departed · Sep 10, 1998 · N528DA · Boeing 727232 · Landing Gear Doors
  > NOSE GEAR DOORS TORN FROM ACFT ON GEAR RETRACTION. REPLACED DOORS. REPAIRED NR 2 AND NR 3 SLATS. REPAIRED HOLE IN FUSELAGE. REPLACED CUT TIRE.
- [SDR DL72S981868](https://openairdocs.org/sdr/DL72S981868.md): Stiffener · cracked · Sep 9, 1998 · N528DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON F1 LETTER CK, NR 6 SLAT O/B TRACK O/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72S981699](https://openairdocs.org/sdr/DL72S981699.md): Spar Web · cracked · Aug 14, 1998 · N528DA · Boeing 727232 · Wing Spar
  > THE CENTER WING REAR SPAR WEB WAS FOUND WITH 5 CRACKS NEAR UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF THOSE IN BAC S/B 727-57A0182. THE SPAR WEB WAS MODIFIED PER THE S/B WITH A CHANGE TO THE REPAIR AT RBL 20 WHERE A PREVIOUS LOCAL REPAIR WAS INSTALLED. THE
- [SDR DL72S980349](https://openairdocs.org/sdr/DL72S980349.md): Rib · cracked · Feb 9, 1998 · N528DA · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB RIB CHORD CRACKED AT FASTENER HOLE, FIN STA 157.2 AND STR 9 RT, FOUND ON E-2 LETTER CHECK. INSTALLED DOUBLER PER M/M 55-30-3 NR 2.
- [SDR DL72S980348](https://openairdocs.org/sdr/DL72S980348.md): Beam · chafed · Feb 9, 1998 · N528DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > FOUND ON E2 LETTER CK, AFT SIDE OF MLG STRUT CHAFING FWD SIDE OF WALKING BEAM. REPAIRED PER MM 57-43-0.
- [SDR DL72S972517](https://openairdocs.org/sdr/DL72S972517.md): Skin · damaged · Nov 7, 1997 · N528DA · Boeing 727232 · Trailing Edge Flaps
  > COVE SKIN PANEL CUTOUT CRACKED 37 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 809.
- [SDR DL72S972209](https://openairdocs.org/sdr/DL72S972209.md): Battery Pack · discharged · Oct 30, 1997 · N528DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK POWER SUPPLY WILL NOT CHARGE. REPLACED BATTERY PACK.
- [SDR DL72S971929](https://openairdocs.org/sdr/DL72S971929.md): Stringer · cracked · Sep 25, 1997 · N528DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L WAS FOUND CRACKED AND CORRODED AT APPROXIMATELY STA 970. THERE WAS AN EXISTING SPLICE AT STATION 980 WHICH HAD BEEN ACCOMPLISHED BY ER/A 258938-14.
- [SDR DL72S971928](https://openairdocs.org/sdr/DL72S971928.md): Skin · corrosion · Sep 25, 1997 · N528DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE AFT CARGO BELLY SKIN WAS FOUND CORRODED FWD OF STA 970 AND JUST O/B OF STR 28-R. THE CUTOUT REMOVING THE SKIN MEASURED 3.5(F/A) BY 3.25 (CIRC). REPAIRED PER ERA 330753-14 REV. A.
- [SDR DL72S971880](https://openairdocs.org/sdr/DL72S971880.md): Blkhd Stiffener · cracked · Sep 12, 1997 · N528DA · Boeing 727232 · Fuselage Main, Bulkhead
  > TWO CRACKS WERE FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACKS ARE APPROX 1.75 AND 1 LONG AND ARE LOCATED AT APPROX WL 237 IN THE IB AND OB RADIUS, RESPECTIVELY, OF THE AFT CHORD. THIS AREA IS ADDRESSED I
- [SDR DL72S971827](https://openairdocs.org/sdr/DL72S971827.md): Fitting · corroded · Sep 12, 1997 · N528DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > RT MLG FWD TRUNNION FITTING IS CORRODED. REPAIRED PER M/M 57-42-0 PG 806-814.
- [SDR DL72S971826](https://openairdocs.org/sdr/DL72S971826.md): Fitting · corroded · Sep 12, 1997 · N528DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > LT MLG FWD TRUNNION PORK CHOP FITTING IS CORRODED. REPAIRED PER M/M 57-42-0 PG 806-814.
- [SDR DL72S971824](https://openairdocs.org/sdr/DL72S971824.md): Rib · cracked · Sep 12, 1997 · N528DA · Boeing 727232 · Elevator, Spar/Rib
  > AT MV2, FOUND RIB CRACKED. THE LOWER SKIN AT ELEV STA 99.79 TO 136.50 HAS A BUBBLE RIB CRACKED ON O/B END. REPAIRED PER SRM 55-20-3 FIG 3.

Next page: https://openairdocs.org/deregistered/N528DA-2003-03-03/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 = 'N528DA' AND deregistration_id = 'N528DA-2003-03-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N528DA-2003-03-03/reports

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