# Service difficulty reports: N534DA, cancelled Aug 7, 2003

A list on [N534DA, cancelled Aug 7, 2003](https://openairdocs.org/deregistered/N534DA-2003-08-07.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DL72S010928](https://openairdocs.org/sdr/DL72S010928.md): Battery Pack · discharged · Jun 7, 2001 · N534DA · Boeing 727232 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND FWD EMERGENCY LIGHT AT 3AB INOP. REPLACED BATTERY PACK.
- [SDR DL72S010429](https://openairdocs.org/sdr/DL72S010429.md): Oven · inoperative · Mar 15, 2001 · N534DA · Boeing 727232 · Buffet/Galleys
  > AIR-TURN-BACK DUE TO ELECTRICAL BURNING SMELL IN FWD GALLEY AREA. SLC MECHANIC FOUND FWD GALLEY OVEN TO BE THE CAUSE. REPLACED GALLEY OVEN.
- [SDR DL72S010104](https://openairdocs.org/sdr/DL72S010104.md): Battery · discharged · Jan 20, 2001 · N534DA · Boeing 727232 · Emergency Lighting
  > UNPON ARRIVAL AT AIRCRAFT EMERGENCY EXIT LIGHTS WOULD NOT COME ON BATTERIES OUT OF CHARGE. REPLACED BATTERY PACKS THROUGH OUT CABIN, ALL CHECKS NORMAL.
- [SDR DL72S002305](https://openairdocs.org/sdr/DL72S002305.md): Skin · punctured · Nov 24, 2000 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 670-710 / STRG. 21L-23L: PUNCTURE REPAIR. THE FUSELAGE SKIN WAS DENTED AND PUNCTURED BETWEEN FS 670 & 710 AND BETWEEN STRINGERS 21L & 23L. THE DAMAGE WAS REMOVED WITH A SKIN CUTOUT FWD OF THE FS 680 SKIN BUTT SPLICE AND CUTOUT AFT OF T
- [SDR DL72S002044](https://openairdocs.org/sdr/DL72S002044.md): Bolt · broken · Oct 18, 2000 · N534DA · Boeing 727232 · Engine Mount Section
  > FOUND ON CREW WALKAROUND, NR 3 ENGINE AFT MOUNT BOLT BROKEN. REMOVED ENGINE, REPAIRED DAMAGE, REPLACED CONE BOLT, REINSTALLED ENGINE.
- [SDR DL72S001335](https://openairdocs.org/sdr/DL72S001335.md): Battery Pack · inoperative · Jul 16, 2000 · N534DA · Boeing 727232 · Emergency Lighting
  > OVERWING EXIT LIGHTS MID AND CARGO INOP. REPLACED BATTERY PACK.
- [SDR DL72S001246](https://openairdocs.org/sdr/DL72S001246.md): Battery Pack · discharged · Jul 1, 2000 · N534DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. MOST FWD CENTER AISLE EXIT LIGHT WILL NOT ILLUMINATE. - REPLACED BATTERY PACK.
- [SDR DL72S001175](https://openairdocs.org/sdr/DL72S001175.md): Battery · inoperative · Jun 18, 2000 · N534DA · Boeing 727232 · Emergency Lighting
  > RIGHT AFT CARGO DOOR EMERGENCY LIGHT INOP. FOUND BATTERY UNIT INOP. REPLACED BATTERY FOR EMERGENCY LIGHTS, NOW OK.
- [SDR DL72S001004](https://openairdocs.org/sdr/DL72S001004.md): Oil Cap · leaking · May 22, 2000 · N534DA · Boeing 727232 · Engine Oil Storage (Airframe Furnished)
  > EN ROUTE NR 2 ENG SHUTDOWN DUE OIL QTY WENT DOWN TO ZERO WITH DECREASING OIL QTY. LOW OIL PRESS LIGHT ILLUM. SHUTDOWN PER POM. FOUND LEAK AT OIL CAP. REPLACED SAME.
- [SDR DL72S000931](https://openairdocs.org/sdr/DL72S000931.md): Angle · cracked · May 10, 2000 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT F-1 LTR CHECK, AIRSTAIR ACTUATOR ATTACH FITTING LOWER FWD SUPPORT ANGLE CRACKED 2.5 INCH AT STA 1263. REPLACED ANGLE PER SRM 53-10-10D.
- [SDR DL72S992840](https://openairdocs.org/sdr/DL72S992840.md): Beam · cracked · Dec 27, 1999 · N534DA · Boeing 727232 · Cargo/Baggage Doors
  > B727 AFT CARGO DOOR, NR 5 PRESSURE STOP BEAM WAS FOUND DAMAGED. THE OUTER T-CHORD OF THE STOP BEAM WAS FOUND CRACKED AT ATA 1095. REPAIRED PER ER/A 372942-14AD.
- [SDR DL72S992550](https://openairdocs.org/sdr/DL72S992550.md): Light · inop · Nov 18, 1999 · N534DA · Boeing 727232 · Emergency Lighting
  > R-1 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NOW OK.
- [SDR DL72S992226](https://openairdocs.org/sdr/DL72S992226.md): Skin · cracked · Oct 6, 1999 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > 1.75 CRACK FUSELAGE SKIN SAT 1045 STRINGER 28L. REPAIRED PER MM 53-30-3 FIG 25.
- [SDR DL72S991185](https://openairdocs.org/sdr/DL72S991185.md): Frame · worn · May 22, 1999 · N534DA · Boeing 727232 · Fuselage Main, Frame
  > FOUND DURING MV2 CORROSION VISIT NR 266, T-ANGLE WORN THROUGH THREE PLACES FROM.75 TO 4.25 INCHES LONG AT FWD FLANGE OF T-ANGLE, NR 2 ENG CUTOUT 4 O'CLOCK POS TO 6 O'CLOCK POS STA 1453. NRC 267 NR 2 ENG CUTOUT FWD COWL STRIKER T-ANGLE WORN THROUGH/THIN 3 O'
- [SDR DL72S991175](https://openairdocs.org/sdr/DL72S991175.md): Web · cracked · May 7, 1999 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV2 CORROSION VISIT NRC 208, 2 CRACKS AT RT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. REPAIRED PER SRM 53-10-4 FIG 17.
- [SDR DL72S991174](https://openairdocs.org/sdr/DL72S991174.md): Web · cracked · May 7, 1999 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV2 MID VISIT NRC 209, 2 CRACKS AT LT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. REPAIRED PER SRM 53-10-4 FIG 17.
- [SDR DL72S991123](https://openairdocs.org/sdr/DL72S991123.md): Stringer · cracked · May 7, 1999 · N534DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING MV2 CORROSION VISIT NRC 210, STR 9 CRACKED AT FIN STA 157.2 INSIDE VERT STAB CRAWLWAY (3RD STR FROM BOTTOM, 3RD BAY UP FROM DOOR). REPAIRED PER M/M 55-30-0 FIG 803.
- [SDR DL72S991008](https://openairdocs.org/sdr/DL72S991008.md): Web · cracked · May 7, 1999 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LEFT I/B TORQUE BOX VERT WEB CRACKED.5 INCH AT UPPER FASTENER STA 1214. REPAIRED PER MM 53-11-0 FIG 819.
- [SDR DL72S990933](https://openairdocs.org/sdr/DL72S990933.md): Power Supply · malfunctioned · Apr 28, 1999 · N534DA · Boeing 727232 · Fuel Flow Indicating
  > WHEN TAKEOFF POWER WAS APPLIED FUEL FLOW INDICATORS, INCREASED IN UNISION AND THEN FLUCTUATED IN UNISION BETWEEN BETWEEN 1000-5000 PPH. WITH T/O EPR ESTABLISHED ALL 3 FUEL FLOW GAUGES INDICATED 1000 PPH STEADY. ALL OTHER ENGINE INDICATIONS NORMAL. TAKEOFF A
- [SDR DL72S990789](https://openairdocs.org/sdr/DL72S990789.md): Power Supply · inoperative · Apr 12, 1999 · N534DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING IN F/C WOULD NOT WORK. REPLACED POWER SUPPLY.
- [SDR DL72S990479](https://openairdocs.org/sdr/DL72S990479.md): Mount · cracked · Mar 8, 1999 · N534DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON E1 LETTER CK, 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR O/B MOUNT WEB ABOVE TRUNNION FITTING. REPAIRED PER MM 57-20-21.
- [SDR DL72S990478](https://openairdocs.org/sdr/DL72S990478.md): Frame · cracked · Mar 8, 1999 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT E-1 LETTER CK, AFT ENTRY DOOR FRAME CUTOUT HAS.5 INCH VISIBLE CRACK LT SIDE. REPAIRED PER SRM 53-10-9.
- [SDR DL72S981204](https://openairdocs.org/sdr/DL72S981204.md): Power Supply · inoperative · Jun 7, 1998 · N534DA · Boeing 727232 · Emergency Lighting
  > DURING LAYOVER INSP, FOUND LEFT FWD OVERWING EMERG LIGHTS INOP. REPLACED ASSOCIATED POWER SUPPLY BASE-DAL (P/N 334701744), (S/N VA-6227).
- [SDR DL72S980495](https://openairdocs.org/sdr/DL72S980495.md): Light · inoperative · Feb 28, 1998 · N534DA · Boeing 727232 · Emergency Lighting
  > PORTABLE EMERGENCY LIGHT ABOVE R1 GALLEY DOOR IS INOP. REPLACED LIGHT ASSY.
- [SDR DL72S980436](https://openairdocs.org/sdr/DL72S980436.md): Radio Alt · malfunctioned · Feb 22, 1998 · N534DA · Boeing 727232 · Ground Proximity System
  > RADIO ALT (CAPTS) SHOWED 2000 AGL WHILE 10000 MSL. THIS WAS FOLLOWED BY A GPWAS PULL UP WARNING AND THEN ELECTRICAL SMOKE IN THE COCKPIT. PULLED CAPTS R/A CB SMOKE DISSIPATED AFTER RUNNING CK LIST LANDED NORMALLY. REPLACED CAPTS R/A IND AND NR 1 R/A TRANSCV
- [SDR DL72S971551](https://openairdocs.org/sdr/DL72S971551.md): Battery Pack · discharged · Aug 7, 1997 · N534DA · Boeing 727232 · Emergency Lighting
  > LT FWD AND AFT OVERWING EXIT UPPER EXIT LIGHTS INOP. REPLACED BATTERY PACK.
- [SDR DL72S970983](https://openairdocs.org/sdr/DL72S970983.md): Web · cracked · May 22, 1997 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING C-2 LETTER CHECK,.75 INCH CRACK LWR TORQUE BOX WEB STA 1218 RT. 1/4 IN CRACK LWR TORQUE BOX WEB STA 1228 RT. REPAIRED PER M/M 53-11-0.
- [SDR DL72S970921](https://openairdocs.org/sdr/DL72S970921.md): Light · inoperative · May 13, 1997 · N534DA · Boeing 727232 · Emergency Lighting
  > LT AFT EMERGENCY EXIT EXT SLIDE LIGHT INOP. REPLACED REFLECTOR ASSY, NOW OPS NORMAL.
- [SDR DL72S970503](https://openairdocs.org/sdr/DL72S970503.md): Power Supply · inoperative · Mar 18, 1997 · N534DA · Boeing 727232 · Emergency Lighting
  > DISC: LT AND RT AFT SERVICE DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, CHECKS GOOD.
- [SDR DL72S970631](https://openairdocs.org/sdr/DL72S970631.md): Skin · corroded · Jan 28, 1997 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON THE SKIN AT STA 1009, STR28R. REPAIRED PER SRM 53-30-3, FIG 3A.
- [SDR DL72S970189](https://openairdocs.org/sdr/DL72S970189.md): Skin · corrosion · Jan 27, 1997 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND ON THE SKIN JUST OUTBOARD OF STR 29L NEAR THE F.S. 1010 BUTT SPLICE WHICH RESULTED IN A 12.5 INCH BY 4.125 INCH CUT-OUT. AN EXISTING EXTERNAL SKIN REPAIR WAS REMOVED AS WELL AND INCORPORATED INTO ONE REPAIR ACCOMPLISHED BY B727 SRM 53-30-3
- [SDR DL72S970182](https://openairdocs.org/sdr/DL72S970182.md): Rib · cracked · Jan 27, 1997 · N534DA · Boeing 727232 · Leading Edge Devices
  > ONE INCH CRACK IN NOSE RIB NR 5 SLAT ACT ATTACH OUTBOARD SIDE. CORRECTION - DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER PER M/M 57-54-0.
- [SDR DL72S970206](https://openairdocs.org/sdr/DL72S970206.md): Floorbeam · corroded · Jan 21, 1997 · N534DA · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT STA 344 FROM LBL 35 TO LBL 53. REMOVED DAMAGED SECTION OF FLOORBEAM AND DRILLED UP NEW SECTION AND SPLICES PER SRM 53-10-8.
- [SDR DL72S960657](https://openairdocs.org/sdr/DL72S960657.md): Stringer · cracked · Mar 25, 1996 · N534DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE TAIL CRAWLWAY ONE AND ONE HALF BAYS DOWN. REPAIRED PER M/M 55-30-0.
- [SDR DL72S960656](https://openairdocs.org/sdr/DL72S960656.md): Stringer · cracked · Mar 25, 1996 · N534DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED IN TAIL CRAWLWAY BETWEEN 2ND AND 3RD BAY RT SIDE. REPAIRED PER M/M 55-30-0.
- [SDR DL72S960655](https://openairdocs.org/sdr/DL72S960655.md): Torque Box Web · cracked · Mar 25, 1996 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING B-2 LETTER CHECK, LWR LT TORQUE BOX CRACKED AT LIGHTNING HOLE AFT OF STA 1223 ADJACENT TO PREVIOUS REPAIRS. LOWER TORQUE BOX LIGHTNING HOLE ROUTED BEYOND LIP RT SIDE STA 1243 BOTH ITEMS REPAIRED PER M/M 53-11-0.
- [SDR DL72S953436](https://openairdocs.org/sdr/DL72S953436.md): Skin · cracked · Aug 18, 1995 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND DURING B-1 LETTER CHECK,.5 CRACK AT LWR AFT CORNER OF L3 WINDOW OPENING. REPAIRED PER SRM 53-30-3 FIG 8.
- [SDR DL72S953435](https://openairdocs.org/sdr/DL72S953435.md): Angle · cracked · Aug 18, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING B-1 LETTER CHECK, NR 2 SLAT ACTUATOR O/B UPPER MOUNT BROKEN. REPAIRED PER MM 57-42-0 PG 812 TO 813.
- [SDR DL72S953434](https://openairdocs.org/sdr/DL72S953434.md): Angle · cracked · Aug 18, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING B-1 LETTER CHECK, NR 2 SLAT COVE SKIN ANGLE CRACKED AT INBOARD END. REPAIRED PER MM 57-54-0 PG 807A.
- [SDR DL72S953433](https://openairdocs.org/sdr/DL72S953433.md): Angle · cracked · Aug 18, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING B-1 LETTER CHECK, NR 2 SLAT COVE SKIN ANGLE CRACKED UNDER THERMAL ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.
- [SDR DL72S951182](https://openairdocs.org/sdr/DL72S951182.md): Slat · cracked · Feb 22, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > UPON INITIAL INSPECTION FOUND NR 6, NR 11, AND NR 18 RIBS CRACKED. RIBS REPAIRED PER 727 M/M CH 57-54-0 BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS ON LEFT WING NR 4 L/E SLAT.
- [SDR DL72S951215](https://openairdocs.org/sdr/DL72S951215.md): Rib · cracked · Feb 21, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH RIB NR 6 CRACKED. REPAIRED PER MM 57-54-0 PG 807.
- [SDR DL72S951214](https://openairdocs.org/sdr/DL72S951214.md): Skin · cracked · Feb 21, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP INSPECTION, FOUND NR 4 L/E SLAT WITH CRACKED SKIN AT MOUNT AREA FOR WING FENCE. REPAIRED PER SRM 57-54-0 PG 817.
- [SDR DL72S951124](https://openairdocs.org/sdr/DL72S951124.md): Slat · cracked · Feb 21, 1995 · N534DA · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND NUMEROUS CRACKS AROUND MOUNT HOLES FOR FENCE IN THE NR 4 LE ADING EDGE SLAT. REPAIRED HOLES PER MM 57-54-0.
- [SDR DL72S950814](https://openairdocs.org/sdr/DL72S950814.md): Stiffener · cracked · Feb 11, 1995 · N534DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT UPPER TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS LOCATED AT F61273. THE STIFFENERS WILL BE REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4.
- [SDR DL72S950584](https://openairdocs.org/sdr/DL72S950584.md): Skin · cracked · Feb 10, 1995 · N534DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND DURING A-2 LETTER CHECK, 2 INCH VISIBLE CRACK AT LWR HINGE CUTOUT OF MAIN ENTRY DOOR ON FUSELAGE. REPAIRED PER MM 53-30-0 PG 820-836 PART 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 = 'N534DA' AND deregistration_id = 'N534DA-2003-08-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N534DA-2003-08-07/reports

---
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