# Service difficulty reports: N510DA, cancelled Jun 7, 2013

A list on [N510DA, cancelled Jun 7, 2013](https://openairdocs.org/deregistered/N510DA-2013-06-07.md).

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

- [SDR DL72L011206](https://openairdocs.org/sdr/DL72L011206.md): Splice · cracked · Jul 19, 2001 · N510DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 500 & 520 AND ANOTHER BETWEEN FS 560 & 580.
- [SDR DL72L011128](https://openairdocs.org/sdr/DL72L011128.md): Battery · discharged · Jul 7, 2001 · N510DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT OVERWING EMERGENCY EXIT LIGHT ON MCO. REPLACED M955 BATTERY CHARGER AND BATTERY.
- [SDR DL72L011097](https://openairdocs.org/sdr/DL72L011097.md): Battery · discharged · Jul 1, 2001 · N510DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND INTERIOR OVERWING EXIT LIGHTS ON RIGHT SIDE FLICKERING. T/S, REPLACED BATTERY CARTRIDGE ASSY. OPS CHECK NORMAL.
- [SDR DL72L010634](https://openairdocs.org/sdr/DL72L010634.md): Seal · worn · Apr 17, 2001 · N510DA · Boeing 727232 · Passenger/Crew Doors
  > LT FWD ENTRY DOOR SEAL MADE ALOUD SQUEAL UPON A/C PRESSURIZING AFTER TAKEOFF SQUEALED UNTIL 4.0 PSI DIFF.AND CEASED AT.5 PSI DIFF. REPAIRED SEAL AREA PRESSURIZED ACFT CKS GOOD
- [SDR DL72L010530](https://openairdocs.org/sdr/DL72L010530.md): Seat Belt · worn · Apr 1, 2001 · N510DA · Boeing 727232 · Emergency Lighting
  > EXIT PATH LITE AT SEAT ROW 11 DEF INOPERATIVE. REPLACED SEAT HARNESS. CKS NML.
- [SDR DL72L010324](https://openairdocs.org/sdr/DL72L010324.md): Flap Track · corroded · Feb 23, 2001 · N510DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL AT BF GOODRICH THE INBOARD FLAP, NR 4 INBOARD TRACK WAS FOUND WITH WEAR AND CORROSION AT THE MLG AND SPOILER BEAM ATTACH PADS, THE MLG DOOR FWD HINGE FITTING AND FWD BRACKET LOWER ATTACH HOLES, FWD LUG BORES, AND IN THE TOGGLE DETENT HOLE
- [SDR DL72L010130](https://openairdocs.org/sdr/DL72L010130.md): Light · inoperative · Jan 23, 2001 · N510DA · Boeing 727232 · Exterior Lighting
  > BOTH AFT CABIN DOORS OUTSIDE LIGHTS ARE INOP. RELAMPED BOTH DOORS. OPERATION NORMAL.
- [SDR DL72L002461](https://openairdocs.org/sdr/DL72L002461.md): Sensor · faulty · Dec 15, 2000 · N510DA · Boeing 727* · Fuel Storage
  > ON LIFT OFF A/C ROLLED TO THE RT - REQUIRED LEFT YOKE TO LEVEL WINGS - SUSPECT FUEL IMBALANCE - FOUND NR 1 FUEL QTY SYSTEM IN ERROR - REPLACED COMPENSATOR
- [SDR DL72L001925](https://openairdocs.org/sdr/DL72L001925.md): Oxygen Mask · disconnected · Oct 2, 2000 · N510DA · Boeing 727232 · Crew Oxygen System
  > S/O OXYGEN MASK HEAD PIECE DISCONNECTED FROM HOSE. REPLACED O2 MASK ASSY, OPS CHECK OK.
- [SDR DL72L001201](https://openairdocs.org/sdr/DL72L001201.md): Battery Pack · inoperative · Jun 23, 2000 · N510DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS NORMAL
- [SDR DL72L001090](https://openairdocs.org/sdr/DL72L001090.md): Battery Pack · inoperative · Jun 3, 2000 · N510DA · Boeing 727232 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK PER MM.
- [SDR DL72L000725](https://openairdocs.org/sdr/DL72L000725.md): Frame · corroded · Apr 16, 2000 · N510DA · Boeing 727232 · Fuselage Main, Frame
  > THE 1166 FRAME AND BONDED DOUBLER WERE FOUND WITH CORROSION DAMAGE BETWEEN STRINGER 30 AND STRINGER 29R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 334245-14AD AT MV-2.
- [SDR DL72L000663](https://openairdocs.org/sdr/DL72L000663.md): Skin · corroded · Apr 7, 2000 · N510DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > AN UNIDENTIFIED REPAIR WAS FOUND AT FS 1010 BETWEEN STR 29L AND 29R. THE DOUBLER WAS REMOVED AND ADDITIONAL CORROSION WAS FOUND. THE DAMAGE WAS REMOVED RESULTING IN A 4.5 X 17.75 CUTOUT. ERA 334227-14 INSTALLS AN EXTERNAL DOUBLER. THE DAMAGE WAS FOUND AT M
- [SDR DL72L000653](https://openairdocs.org/sdr/DL72L000653.md): Frame · cracked · Apr 7, 2000 · N510DA · Boeing 727232 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON THE FS 700 FRAME BETWEEN STRINGER 22L AND 23L. THE FRAME WAS CUT AT STRINGER 22L AND A NEW SECTION WAS SPLICED. THE DAMAGE WAS REPAIRED PER ERA 334272-14 AT A MID-VISIT.
- [SDR DL72L000651](https://openairdocs.org/sdr/DL72L000651.md): Frame · corroded · Apr 7, 2000 · N510DA · Boeing 727232 · Fuselage Main, Frame
  > THE C2 DOOR SILL WAS FOUND WITH CORROSION JUST FORWARD OF THE FS 990 FRAME. CORROSION WAS FOUND ON THE OUTBAORD HOR. FLANGE AND BLENDED AWAY TO A MAXIMUM DEPTH OF.160. THE DAMAGE WAS REPAIRED PER ERA 334217-14 BY REMOVING THE DAMAGED FLANGE AND INSTALLI
- [SDR DL72L000588](https://openairdocs.org/sdr/DL72L000588.md): Skin · damaged · Mar 28, 2000 · N510DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > AN OPEN PILOT HOLE WAS FOUND IN THE FUSELAGE SKIN AT FS 826 JUST ABOVE STRINGER 18A, UNDER THE WING TO BODY FAIRING. THE HOLE WAS.125 IN DIAMETER. ERA 334223-14 PERFORMS A HIGH FREQUENCE EDDY CURRENT INSPECTION AND LEAVES THE HOLE AS IS. THE HOLE WAS FOUN
- [SDR DL72L000620](https://openairdocs.org/sdr/DL72L000620.md): Web · cracked · Mar 16, 2000 · N510DA · Boeing 727232 · Vertical Stabilizer
  > WEB CRACKED LT LOWER CORNER INSIDE OF VERT, MARKED. STOP DRILLED CRACK AND MADE REPAIR PARTS PER SRM 53-10-4D. CHEMICAL TREAT PER PS 900-2-4-1 NR 2. OK TO IST DOUBLER. REPAIRED PER SRM 53-10-4D.
- [SDR DL72L000214](https://openairdocs.org/sdr/DL72L000214.md): Fcu · failed · Jan 29, 2000 · N510DA · Boeing 727232 · Fuel Control/Turbine Engines
  > NR 3 THROTTLE BINDING IN FLT. NO THROTTLE/ENG RESPONSE IN UPPER ONE-THIRD OF TRAVEL. BINDING THEN RELOCATED TO LWR ONE-THIRD OF THROTTLE MOVEMENT. WHEN THROTTLE WAS ADVANCED THE LEVER WOULD TRAVEL AFT APPROX 1 TO 2 INCHES ON ITS OWN WITH NO ENG RESPONSE. R
- [SDR DL72L992357](https://openairdocs.org/sdr/DL72L992357.md): Insulation · damaged · Sep 20, 1999 · N510DA · Boeing 727232 · Electrical Power System Wiring
  > ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL
- [SDR DL72L992356](https://openairdocs.org/sdr/DL72L992356.md): Insulation · damaged · Sep 20, 1999 · N510DA · Boeing 727232 · Electrical Power System Wiring
  > ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FOR SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL
- [SDR DL72L991887](https://openairdocs.org/sdr/DL72L991887.md): Battery Pack · discharged · Aug 24, 1999 · N510DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND RIGHT EXTERIOR OVERWING EMERGENCY LIGHT FLASHING DURING TEST. REPLACED BATTERY PACK.
- [SDR DL72L990034](https://openairdocs.org/sdr/DL72L990034.md): Bracket · cracked · Jan 7, 1999 · N510DA · Boeing 727232 · Leading Edge Slat Actuator
  > THE ACTUATOR SUPPORT BRACKET DOUBLERS WERE FOUND CRACKED FOR THE NR 7 SLAT. THE CRACKS ARE TYPICAL OF BAC S/B 727-57- 0130. THE BRACKETS WERE MODIFIED PER THE INSTRUCTIONS OF THE S/B AND DOCUMENTED PER ER/A 366431-14.
- [SDR DL72L990013](https://openairdocs.org/sdr/DL72L990013.md): Frame · cracked · Jan 4, 1999 · N510DA · Boeing 72723 · Leading Edge Devices
  > A.25 INCH VISIBLE CRACK LOWER FWD CORNER NR 5 FLAP ACT MOUNT BOX I/B FRAME. REPAIRED PER MM 57-20-21.
- [SDR DL72L990011](https://openairdocs.org/sdr/DL72L990011.md): Bracket · cracked · Jan 4, 1999 · N510DA · Boeing 727232 · Trailing Edge Flaps
  > FOUND ON D1 LETTER CK,.25 INCH CRACK NR 5 L/E FLAP ACTUATOR OUTBOARD ATTACH BRACKET. REPAIRED PER MM 57-20-21.
- [SDR DL72L982644](https://openairdocs.org/sdr/DL72L982644.md): Duct · failed · Dec 24, 1998 · N510DA · Boeing 727232 · Pneumatic Distribution System
  > ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. ALL CK LIST WERE RUN AND LIGHT DID NOT GO OUT. SHUT DOWN NR 1 ENG AND DUMP FUEL. RETURNED TO SEA. REPLACED LEAKING HP TAI DUCT, LEAK CK NORMAL.
- [SDR DL72L982358](https://openairdocs.org/sdr/DL72L982358.md): Battery · discharged · Nov 14, 1998 · N510DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHTS FAILED TO TEST. REPLACED BATTERY.
- [SDR DL72L981963](https://openairdocs.org/sdr/DL72L981963.md): Wire · broken · Sep 21, 1998 · N510DA · Boeing 727232 · Landing Gear System Wiring
  > WHEN LANDING GEAR WAS LOWERED THE RLG GREEN DOWN AND LOCKED DIDN'T ILUMINATE. LIGHT DIDN'T PRESS TO TEST. CHANGED BULBS, NO HELP. WENT TO BRIGHT ON BRIGHT/DIM SWITCH AND INDICATION WERE NORMAL. SECURED WIRE ON BACK OF BRIGHT/DIM SWITCH, OPS CHECK NORMAL.
- [SDR DL72L981147](https://openairdocs.org/sdr/DL72L981147.md): Web · cracked · May 29, 1998 · N510DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > RT VERT TORQUE BOX WEB CRACKED.875 INCH AT UPPER LIGHTENING HOLE STA 1300 RT. REPAIRED PER MM 53+11+0 P 828.
- [SDR DL72L972666](https://openairdocs.org/sdr/DL72L972666.md): Rib · cracked · Dec 17, 1997 · N510DA · Boeing 727232 · Leading Edge Devices
  > O/B ACTUATOR RIB CRACKED. REPAIRED RIB PER SRM 57-54-0.
- [SDR DL72L972678](https://openairdocs.org/sdr/DL72L972678.md): Rib · cracked · Dec 13, 1997 · N510DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 18 CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72L972164](https://openairdocs.org/sdr/DL72L972164.md): Megaphone · inop · Oct 27, 1997 · N510DA · Boeing 727232 · Emergency Equipment
  > ON PREDEPARTURE CK, FOUND F/C MEGAPHONE INOP. REPLACED F/C MEGAPHONE.
- [SDR DL72L972153](https://openairdocs.org/sdr/DL72L972153.md): Angle · cracked · Oct 25, 1997 · N510DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FROM MV1C1,.25 INCH VISIBLE CRACK KEEL BEAM VERTICAL ANGLE INBD OF APU LOAD CONTROL VALVE. REPAIRED PER SRM 53-10-9.
- [SDR DL72L972151](https://openairdocs.org/sdr/DL72L972151.md): Support · cracked · Oct 25, 1997 · N510DA · Boeing 727232 · Leading Edge Devices
  > FROM MV1C, NR 7 SLAT ACTUATOR O/B SUPPORT STRUCTURE CRACKED. REPAIR PER M/M 57-42-0.
- [SDR DL72L972189](https://openairdocs.org/sdr/DL72L972189.md): Frame · corroded · Oct 24, 1997 · N510DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE C3 DOOR SURROUND FS 1142.7 FRAME STRG 28R. REPAIR FOR CORRODED SKIN ATTACH FLANGE. C3 AFT DOOR JAMB FRAME (FS 1142.7) WAS FOUND CORRODED AT STRG 28R. THE LOWER FLANGE OF THE FRAME SKIN ATTACH ANGLE WAS TRIMMED OFF. ANGLE REPAIR INSTALLED PER ER/A
- [SDR DL72L972152](https://openairdocs.org/sdr/DL72L972152.md): Skin · cracked · Oct 24, 1997 · N510DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FROM MV1C1,.5 INCH CRACK IN VERTICAL SKIN AT UPPER RIVET ROW OF LT TORQUE BOX AT STA 1223. REPAIR PER M/M 53-11-0.
- [SDR DL72L972180](https://openairdocs.org/sdr/DL72L972180.md): Skin · corroded · Oct 23, 1997 · N510DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 480-500, STRG 28L, SKIN CUT OUT DUE TO CORROSION. REPAIRED PER ER/A 362981-14.
- [SDR DL72L972075](https://openairdocs.org/sdr/DL72L972075.md): Chord · corroded · Oct 16, 1997 · N510DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON O/B FLANGE OF NOSE WHEEL WELL SIDE PANEL T-CHORD RT WALKWAY BEAM AFT OF STA 312 AND 344. CLEANED CORROSION WITHIN LIMITS PER SRM 53-10-4 FIG 7. TREATED AND PAINTED REWORKED AREAS.
- [SDR DL72L972076](https://openairdocs.org/sdr/DL72L972076.md): Rib · cracked · Oct 14, 1997 · N510DA · Boeing 727232 · Leading Edge Devices
  > A.25 INCH CRACK IN NR 4 SLAT I/B ACTUATOR ATTACH NOSE RIB. REPAIRED PER MM 57-40-0.
- [SDR DL72L970260](https://openairdocs.org/sdr/DL72L970260.md): Battery · discharged · Feb 12, 1997 · N510DA · Boeing 727232 · Emergency Lighting
  > DOOR EXIT LIGHT ABOVE COCKPIT DOOR DOES NOT ILLUMINATE WITH STANDBY POWER. REPLACED BATTERIES.
- [SDR DL72L960257](https://openairdocs.org/sdr/DL72L960257.md): Stringer · cracked · Feb 1, 1996 · N510DA · Boeing 727232 · Vertical Stabilizer
  > STRINGERS CRACKED 3RD BAY UP IN VERT STAB ON LT AND RT SIDE UPPER END AND 3RD BAY UP RT LOWER. FOUND DURING A-2 LTR CK TPAMM AND REPAIRED PER SRM 55-30-0.
- [SDR DL72L954440](https://openairdocs.org/sdr/DL72L954440.md): Battery Pack · discharged · Nov 19, 1995 · N510DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS INOP 2R AND AFT AISLE. REPLACED BATTERY PACK, OPERATION NORMAL.
- [SDR DL72L952919](https://openairdocs.org/sdr/DL72L952919.md): Angle · cracked · Jul 1, 1995 · N510DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING LETTER CHECK, A 1 INCH CRACK WAS FOUND IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. REPLACED DAMAGED PART IN ACCORDANCE WITH S/B 727-53-0129, REV. 4.
- [SDR DL72L950756](https://openairdocs.org/sdr/DL72L950756.md): Actuator · cracked · Feb 20, 1995 · N510DA · Boeing 727232 · Landing Gear Actuator
  > ON LANDING GEAR EXTENSION, LOST ALL A SYSTEM HYDRAULIC FLUID, LANDED SAN WITHOUT INCIDENT, FOUND NOSE LANDING GEAR DOWN LOCK ACTUATOR CRACKED. REPLACED ACTUATOR OPERATION NORMAL.
- [SDR DL72L950605](https://openairdocs.org/sdr/DL72L950605.md): Anti-Ice Valve · leaking · Feb 11, 1995 · N510DA · Boeing 727232 · Air Intake Anti/De-Ice System
  > DURING CLIMB, HAD NR 3 STRUT OVERHEAT LIGHT ON, LIGHT WENT OUT WITH REDUCTION OF POWER. RETURNED ATL. REPLACED NR 3 ENGINE ANTI-ICE VALVE AND UPPER ANTI-ICE DUCT ASSEMBLY AT VALVE, LEAK CHECK OK.

## 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 = 'N510DA' AND deregistration_id = 'N510DA-2013-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N510DA-2013-06-07/reports

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