# Service difficulty reports: N410DA, cancelled Jul 20, 2010

A list on [N410DA, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N410DA-2010-07-20.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 DL72S030143](https://openairdocs.org/sdr/DL72S030143.md): Skin · damaged · Feb 11, 2003 · N410DA · Boeing 727232 · Elevator, Plate/Skin
  > UPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD.
- [SDR DL72S011025](https://openairdocs.org/sdr/DL72S011025.md): Warning Light · false indication · Jun 21, 2001 · N410DA · Boeing 727232 · Door Warning System
  > R-2 DOOR IND ILLUM ON T/O ROLL. ABORTED T/O BELOW 100 KTS. INSPECTED DOOR, NO PROBLEM NOTED. DOOR OPS NORM. CYCLED NUMEROUS TIMES, UNABLE TO DUPLICATE.
- [SDR DL72S010516](https://openairdocs.org/sdr/DL72S010516.md): Angle · cracked · Mar 29, 2001 · N410DA · Boeing 727232 · Leading Edge Devices
  > 1/2 INCH CRACK IN NR 8 L/E SLAT COVE SKIN ANGLE AT ANTI-ICE DUCT CUTOUT REPAIRED PER MM 57-54-000-8
- [SDR DL72K001734](https://openairdocs.org/sdr/DL72K001734.md): Sign · inoperative · Sep 8, 2000 · N410DA · Boeing 727232 · Emergency Lighting
  > FOUND AFT SERVICE DOORS OVERHEAD EXIT SIGN IN AFT GALLEY. REINSTALLED EXIT SIGN. LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY PACK AND BASE, NO HELP. FOUND WIRE BROKEN ON EXIT SIGN. REPAIRED WIRE. SIGN OPS NORMAL NOW.
- [SDR DL72K001291](https://openairdocs.org/sdr/DL72K001291.md): Relay · failed · Jul 7, 2000 · N410DA · Boeing 727232 · Cabin Pressure Controller
  > AFTER TAKEOFF PRESSURIZATION AUTO FAILED TO STBY. ATTEMPTED OPERATION IN STBY AND MANUAL. CABIN DIDN''T PRESSURIZE. FOUND PACK VALVE C/B POPPED. LEVELED AT 8,000 FT, CABIN ALT 8,000. PSI DIF. ISOLATED POPPING C/B TO R23 RELAY. REPLACED BOTH R23 AND R22 R
- [SDR DL72K000920](https://openairdocs.org/sdr/DL72K000920.md): Pump · damaged · May 8, 2000 · N410DA · Boeing 727232 · Engine Fuel Pump
  > AS ENG POWER WAS ADVANCED FOR TAKEOFF NR 1 ENG FLAMED OUT. EPR ON NR 1 ENG REACHED 1.3 BEFORE ENGINE INST. ROLLED BACK, NO TAKEOFF WAS INITIATED. FOUND ENG FUEL PUMP SHEARED. REPLACED SAME AND ENG FUEL CONTROL.
- [SDR DL72K000769](https://openairdocs.org/sdr/DL72K000769.md): Sign · inoperative · Apr 20, 2000 · N410DA · Boeing 727232 · Emergency Lighting
  > AFT EMERGENCY EXIT SIGN INOP AT CENTER AISLE STA 1046. REPLACED BATTERY RACK, CKS NORMAL.
- [SDR DL72K000728](https://openairdocs.org/sdr/DL72K000728.md): Frame · cracked · Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, Frame
  > A PREVIOUS REPAIR WAS FOUND ON THE FS 910 FRAME AT STR 18A ON THE RIGHT SIDE OF THE AIRCRAFT. THE REPAIR WAS REMOVED, INSPECTED AND A NEW REPAIR INSTALLED PER ERA 334253-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000727](https://openairdocs.org/sdr/DL72K000727.md): Frame · corroded · Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON THE FS 1142.7 CARGO DOOR OPENING FRAME ON THE FORWARD SIDE OF THE WEB. THE CORROSION WAS BLENDED AND A DOUBLER INSTALLED PER ERA 334273-14 AT HMV.
- [SDR DL72K000723](https://openairdocs.org/sdr/DL72K000723.md): Skin · gouged · Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-2 DOOR AT FS 990. THE DAMAGE WAS LOCATED APPROX 1 INCH ABOVE STRINGER 24R. THE SKIN, DOUBLER AND TRIPLER WERE TRIMMED, INSPECTED AND TREATED PER ERA 334268-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000668](https://openairdocs.org/sdr/DL72K000668.md): Door Frame · cracked · Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE RT FRAME OF THE AFT ENTRY DOOR WAS FOUND CRACKED IN THE FORWARD FLANGE AT WL 276. THE BEAM WAS CUT AND A NEW SECTION SPLICED IN PER ERA 334236-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000667](https://openairdocs.org/sdr/DL72K000667.md): Frame · worn · Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, Frame
  > THE FS 1148 FRAME INNER CHORD WAS WORN AT STRINGER 5R. THE DAMAGE WAS BLENDED SMOOTH AND A REPAIR WAS INSTALLED PER ERA334258-14. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72K000656](https://openairdocs.org/sdr/DL72K000656.md): Stiffener · cracked · Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CRACKS WERE FOUND ON BOTH THE LBL 8 AND RBL 8 STIFFENERS OF THE 1183 BULKHEAD AT WL 182. THE CRACKS ARE IN THE TYPICAL LOCATIONS AS THOSE DESCRIBED IN S/B 727-53-0175. THE S/B REPAIR WAS INSTALLED PER ERA 334276-14AD AT HMV.
- [SDR DL72K000655](https://openairdocs.org/sdr/DL72K000655.md): Skin · cracked · Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK IS THROUGH THE SKIN, DOUBLER AND BEARSTRAP AND IS APPROXIMATELY 2 INCHES LONG. THE CRACK WAS CUT OUT AND REPAIRED PER ERA 334242-14 WITH AND EXTERNAL REPAIR DOUBLER AND TRIPLER. THE
- [SDR DL72K000654](https://openairdocs.org/sdr/DL72K000654.md): Skin · gouged · Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT FS 360 BETWEEN STRINGER 17L AND 18L JUST BELOW AND AFT OF THE L1 DOOR CUTOUT. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED AT HMV PER ERA 334256-14.
- [SDR DL72K000589](https://openairdocs.org/sdr/DL72K000589.md): Skin · cracked · Mar 28, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > SEVERAL CRACKS WERE FOUND IN THE LAP JOINT OF THE FUSELAGE SKIN AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE LAP JOINT WAS REPLACED PER ERA 334230-14AD AT HMV.
- [SDR DL72K000568](https://openairdocs.org/sdr/DL72K000568.md): Beam · corroded · Mar 24, 2000 · N410DA · Boeing 727232 · Wing, Attach Fittings
  > DURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS AND WEAR AT THE FWD ATTACH LUGS AND TOGGLE DETENT HOLE. REPAIR PER ER/A 387256-14AD AND BF GOODRICH REPAIR NR 23-0592.
- [SDR DL72K000753](https://openairdocs.org/sdr/DL72K000753.md): Angle · cracked · Mar 23, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 3 PLACES. A SECTION OF THE ANGLE WAS REPLACED AND NEW SECTION SPLICED IN PER MM 5752-01, FIG 802.
- [SDR DL72K000638](https://openairdocs.org/sdr/DL72K000638.md): Skin · worn · Mar 23, 2000 · N410DA · Boeing 727232 · Leading Edge Devices
  > AT HMV THE 5 SLAT LEADING EDGE WAS FOUND WORN AT FENCE. DRILLED REPAIR DOUBLER PER MM 57-54-0. DYE PEN INSP AREA UNDER FENCE FOUND 2 CRACKS STOP DRILLED. INSTALLED DOUBLER PER MM 57-54-0 FIG 817.
- [SDR DL72K000585](https://openairdocs.org/sdr/DL72K000585.md): Rib · cracked · Mar 23, 2000 · N410DA · Boeing 727232 · Leading Edge Devices
  > NR 5 SLAT I/B RIB CRACKED. INSTALLED REPAIR DOUBLER PER B727 MM 57-54-0, FIG 814.
- [SDR DL72K001976](https://openairdocs.org/sdr/DL72K001976.md): Skin · damaged · Mar 22, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B LOWER CORNER. THE SKIN WAS REPAIRED PER 727 M/M 57-52-0 FIG 803, BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND SKIN FILLER.
- [SDR DL72K000641](https://openairdocs.org/sdr/DL72K000641.md): Skin · worn · Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge Devices
  > AT HMV THE SKIN ON 4 L/E SLAT WAS WORN ON UPPER AND LWR SURFACES I/B TRACK. AREA BURNISHED REPAIR DOUBLER MANUF INSTALLED DOUBLER PER MM 57-54-0 FIG 813.
- [SDR DL72K000640](https://openairdocs.org/sdr/DL72K000640.md): Rib · cracked · Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge Devices
  > AT HMV A RIB WAS FOUND CRACKED ON 4 L/E SLAT I/B END. REPAIRED PER 57-54-0 FIG 814.
- [SDR DL72K000639](https://openairdocs.org/sdr/DL72K000639.md): Rib · cracked · Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge Devices
  > AT HMV 4 L/E SLAT RIB WAS FOUND CRACKED ON O/B END. REPLACED PER MM 57-54-0 FIG 814. DYE CHECKED, FOUND NO CRACKS.
- [SDR DL72K000756](https://openairdocs.org/sdr/DL72K000756.md): Angle · cracked · Mar 21, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. A SECTION OF THE ANGLE WAS REPLACED AND SPLICED TO OLD SECTION PER MM 57-52-0, FIG 802.
- [SDR DL72K000755](https://openairdocs.org/sdr/DL72K000755.md): Angle · cracked · Mar 21, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. THE CHORD WAS REPAIRED PER MM 57-52-0, FIG 802.
- [SDR DL72K000744](https://openairdocs.org/sdr/DL72K000744.md): Rib · cracked · Mar 20, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE I/B AFT RIB WAS FOUND CRACKED IN THE LOWER RADIUS AT THE AFT END. THE CRACK WAS STOP DRILLED AND A DOUBLER INSTALLED PER 727 MM 57-52-0, FIG 808.
- [SDR DL72K000624](https://openairdocs.org/sdr/DL72K000624.md): Skin · cracked · Mar 20, 2000 · N410DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > AT HMV THE VERT SKIN WAS CRACKED AT PANEL 9523 LT FWD SIDE OF VERT STAB. REPAIR WAS FABRICATED PER MM 54-30-0 FIG 903 AND REPAIR WAS INSTALLED.
- [SDR DL72K000621](https://openairdocs.org/sdr/DL72K000621.md): Panel · damaged · Mar 20, 2000 · N410DA · Boeing 727232 · Vertical Stabilizer
  > AT HMV A TEMP REPAIR WAS INSTALLED ON LT SIDE OF VERT STAB AT L/E STA 1298 JUST FWD OF L/E PNL 9525. TEMP REPAIR WAS REMOVED AND DAMAGE CUT OUT AND PERM REPAIR INSTALLED PER MM 54-30-0 FIG 802.
- [SDR DL72K000580](https://openairdocs.org/sdr/DL72K000580.md): Flap Track · corroded · Mar 20, 2000 · N410DA · Boeing 727232 · Trailing Edge Flaps
  > HMV- ATTACH LUG HOLE FORWARD FITTING MLG WING DOOR CORRODED. REPAIRED PER MM 57-43-01.
- [SDR DL72K991576](https://openairdocs.org/sdr/DL72K991576.md): Skin · cracked · Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 29 CRACKS ALONG
- [SDR DL72K991575](https://openairdocs.org/sdr/DL72K991575.md): Skin · cracked · Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 480-500, STRG 4L, SKIN LAP SPLICE, CRACK REPAIR. HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A SINGLE CRACK BETWEEN FS 480 AND 500. THE CRACK WAS CUTOUT OF THE SK
- [SDR DL72K991574](https://openairdocs.org/sdr/DL72K991574.md): Skin · cracked · Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 700-720, STRG 4R, SKIN LAP SPLICE: CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWE
- [SDR DL72K991573](https://openairdocs.org/sdr/DL72K991573.md): Skin · cracked · Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 720A-720B, STRG 4R SKIN LAP SPLICE CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 7
- [SDR DL72K991111](https://openairdocs.org/sdr/DL72K991111.md): Light · inoperative · May 19, 1999 · N410DA · Boeing 727232 · Emergency Lighting
  > L2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.
- [SDR DL72K990966](https://openairdocs.org/sdr/DL72K990966.md): Angle · corroded · Apr 30, 1999 · N410DA · Boeing 727232 · Engine Mount Section
  > WHILE PERFORMING HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLES CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLES WITH ANGLES OF NEW MFG.
- [SDR DL72K990740](https://openairdocs.org/sdr/DL72K990740.md): Angle · cracked · Apr 5, 1999 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.25 INCH CRACK ON ANGLE FWD SIDE OF FS 910 RT ABOVE AND FWD OF H BRACKET. REPAIRED PER MM 53-11-0, TIME LIMITED REPAIR.
- [SDR DL72K990512](https://openairdocs.org/sdr/DL72K990512.md): Actuator · leaking · Mar 11, 1999 · N410DA · Boeing 727232 · Drag Control Actuator
  > ON WALKAROUND INSPECTION, FOUND NR 14 SPOILER ACTUATOR LEAKING.
- [SDR DL72K981031](https://openairdocs.org/sdr/DL72K981031.md): Skin · damaged · May 12, 1998 · N410DA · Boeing 727232 · Elevator, Plate/Skin
  > DURING BUYBACK OF N/R 218, FOUND NUT PLATE EMBEDDED AT RT ELEVATOR LOWER SKIN. SKIN HAS.3125 INCH IN HOLE REPAIRED PER SRM 55-20-3.
- [SDR DL72K980992](https://openairdocs.org/sdr/DL72K980992.md): Stringer · cracked · May 8, 1998 · N410DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > THE OUTER CHORD OF THE STRINGER 17L CREASE BEAM WAS FOUND WITH A.5 CRACK AT STA 848.95. THE CRACK WAS IN THE HORIZONTAL FLANGE OF THE TEE WHERE THE FLANGE WAS MILLED AWAY TO PASS UNDER THE FRAME. THE CRACK WAS ROUTED OUT OF THE HORIZONTAL FLANGE AND STOP
- [SDR DL72K981030](https://openairdocs.org/sdr/DL72K981030.md): Rear Spar · cracked · May 4, 1998 · N410DA · Boeing 727232 · Elevator, Spar/Rib
  > AN.375 INCH CRACK RT ELEVATOR REAR SPAR AT 2ND FROM O/B TAB, HINGE. REPLACED REAR SPAR UNDER EO 4-70183-3AD ME 02 AND ME 03.
- [SDR DL72K980894](https://openairdocs.org/sdr/DL72K980894.md): Bear Strap · cracked · Apr 26, 1998 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FUSELAGE/SKIN ASSY, R1 DOOR SURROUND DOUBLER, UPPER HINGE CUTOU. REPAIR FOR CRACK IN REINFORCING DOUBLER. THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN THE UPPER HINGE CUTOUT. THE CRACK WAS IDENTIFIED AS BEING IN R
- [SDR DL72K980950](https://openairdocs.org/sdr/DL72K980950.md): Skin · cracked · Apr 22, 1998 · N410DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > THREE EACH.125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER MM 54-30-0.
- [SDR DL72K980937](https://openairdocs.org/sdr/DL72K980937.md): Floorbeam · corrosion · Apr 21, 1998 · N410DA · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM STA 1030 BL 0. REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-20-11.
- [SDR DL72K980914](https://openairdocs.org/sdr/DL72K980914.md): Bear Strap · cracked · Apr 21, 1998 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON MV2 CORROSION VISIT, CRACK IN EDGE OF BEARSTRAP AT RT FWD SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REFERENCE SUPPLEMENTAL CARD FOR SI 4-72762-12 ME-02. REPAIRED PER ERA 364614-14 REV A.
- [SDR DL72K981029](https://openairdocs.org/sdr/DL72K981029.md): Bracket · cracked · Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Devices
  > NR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812.
- [SDR DL72K980902](https://openairdocs.org/sdr/DL72K980902.md): Stringer · cracked · Apr 20, 1998 · N410DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON MV2 CORROSION VISIT, 1 VISABLE CRACK STR 18A RT, AFT OF STA 940 FITTING UPPER AFT ATTACH BOLT. REPAIRED PER M/M 53-12-0.
- [SDR DL72K980900](https://openairdocs.org/sdr/DL72K980900.md): Bracket · cracked · Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21.
- [SDR DL72K980899](https://openairdocs.org/sdr/DL72K980899.md): Bracket · cracked · Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.
- [SDR DL72K980898](https://openairdocs.org/sdr/DL72K980898.md): Bracket · cracked · Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21.

Next page: https://openairdocs.org/deregistered/N410DA-2010-07-20/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 = 'N410DA' AND deregistration_id = 'N410DA-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N410DA-2010-07-20/reports

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