# Service difficulty reports: N513DA, cancelled Jul 20, 2010

A list on [N513DA, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N513DA-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.

- [SDR DL72L011111](https://openairdocs.org/sdr/DL72L011111.md): Rib · cracked · Mar 3, 2001 · N513DA · Boeing 727232 · Trailing Edge Flaps
  > INBOARD AFT RIB CRACKED ON THE NR 1 MID FLAP. REPAIRED PER M/M 57-52-0 FIG 808.
- [SDR DL72L002251](https://openairdocs.org/sdr/DL72L002251.md): Connector · shorted · Nov 19, 2000 · N513DA · Boeing 727232 · Fuel Indicating System
  > WORKING MCO - REFUEL PANEL QTY INDICATORS INOP. FOUND CANNON PLUG TIED BACK AND CAPPED D1756 SHORTED AND BURNED. REMOVED CONNECTOR AND TERMINATED WIRES AND TIED BACK HARNESS.
- [SDR DL72L002111](https://openairdocs.org/sdr/DL72L002111.md): Frame · cracked · Oct 25, 2000 · N513DA · Boeing 727232 · Cargo/Baggage Doors
  > AFT DEACTIVATED CARGO DOOR HAD 7 INCH CRACK IN FWD LOWER CORNER FORMER. REPLACED AFT CARGO DOOR, PRESS CKS GOOD.
- [SDR DL72L002092](https://openairdocs.org/sdr/DL72L002092.md): Fire Loop · false activation · Oct 23, 2000 · N513DA · Boeing 727233 · Fire Detection
  > ENG NR 1 DETECTOR FAULT LIGHT ILLUMINATED AT T/O POWER. LIGHT EXTINGUISHED ON POWER REDUCTION. RTO AT 25 KTS. FOUND 1 LOOP IN CONTACT WITH METAL SHROUD. MOVED SHROUD TO PROVIDE CLEARANCE FOR FIRE LOOP. RAN ENGINE AT T/O POWER FOR SEVERAL MINUTES. NO DETE
- [SDR DL72L001197](https://openairdocs.org/sdr/DL72L001197.md): Battery Pack · discharged · Jun 21, 2000 · N513DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT EXTERIOR EMERGENCY LIGHT BEHIND LEFT WING INOPERATIVE. REPLACED BATTERY PACK. LIGHT OP NORMAL
- [SDR DL72L000858](https://openairdocs.org/sdr/DL72L000858.md): Light · inoperative · Apr 30, 2000 · N513DA · Boeing 727232 · Emergency Lighting
  > RIGHT CENTER OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY RACK, OPS NORMAL.
- [SDR DL72L992584](https://openairdocs.org/sdr/DL72L992584.md): Skin · corroded · Nov 23, 1999 · N513DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND IN THE STR 26R LAP JOINT BETWEEN FS 500 AND 520. THE DAMAGE WAS REPAIRED PER ERA 333773-14AD AT HMV.
- [SDR DL72L992536](https://openairdocs.org/sdr/DL72L992536.md): Bearstrap · gouged · Nov 17, 1999 · N513DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FORWARD EDGE OF THE BEARSTRAP OF THE C-1 CARGO DOOR WAS FOUND DAMAGED. THE DAMAGE WAS CLEANED UP WITH A.5 BY.3 AND REPAIRED PER ERA 333761-14 AT MV.
- [SDR DL72L992479](https://openairdocs.org/sdr/DL72L992479.md): Blkhd Stiffener · cracked · Nov 10, 1999 · N513DA · Boeing 727232 · Fuselage Main, Bulkhead
  > THE VERTICAL STIFFENERS AT LBL AND RBL 36.83 ON THE FORWARD SIDE OF THE FS 1183 BULKHEAD WERE FOUND CRACKED BETWEEN WL 230 AND WL 270. THE DAMAGE WAS REPIARED PER ERA 333759-14 AT MV.
- [SDR DL72L992480](https://openairdocs.org/sdr/DL72L992480.md): Skin · dented · Nov 4, 1999 · N513DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT STA 380 AND STR 17L AND STA 387 BETWEEN S 17L AND 18L. DAMAGE TRIMMED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER. ERA 333767-14 REV B.
- [SDR DL72L992026](https://openairdocs.org/sdr/DL72L992026.md): Battery · discharged · Sep 12, 1999 · N513DA · Boeing 727232 · Emergency Lighting
  > 32 OVERHEAD EXIT LIGHT INOP. REPLACED BATTERY OPS NOW OK.
- [SDR DL72L992025](https://openairdocs.org/sdr/DL72L992025.md): Battery Pack · discharged · Sep 12, 1999 · N513DA · Boeing 727232 · Emergency Lighting
  > RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK OPS CK OK.
- [SDR DL72L991116](https://openairdocs.org/sdr/DL72L991116.md): Switch · out of adjust · May 20, 1999 · N513DA · Boeing 727232 · Leading Edge Slat Position Indicating System
  > UNSAFE (AMBER LIGHT) INDICATION EXT AT FLAPS 5 POSITION. AFTER EXAMINATION IT WAS DETERMINED THAT L/E FLAP NR 1 FAILED TO EXTEND PROPERLY. AFTER TOUCHDOWN, L/E FLAPS LIGHT TURNED GREEN AND POS IND APPEARED NORMAL. ADJUSTED NR 1 L/E FLAP SWITCH PER MM, CHECK
- [SDR DL72L990605](https://openairdocs.org/sdr/DL72L990605.md): Battery Pack · discharged · Mar 22, 1999 · N513DA · Boeing 727232 · Emergency Lighting
  > FWD AND REAR OVER AISLE EMERG EXIT LIGHTS FLICKER WHEN STANDBY PWR SELECTED. REPLACED 2 BATTERY PACKS, OPS NORMAL.
- [SDR DL72L990355](https://openairdocs.org/sdr/DL72L990355.md): Beacon · loose · Feb 23, 1999 · N513DA · Boeing 727232 · Exterior Lighting
  > UPPER ROTATING BEACON CAME OUT OF ITS RETAINER AND FELL AND ROLLED BETWEEN CEILING PANEL AND OVERHEAD COMPARTMENT IN CABIN CAUSING A PASSENGERS BAG TO BE SCORCHED. NO OTHER DAMAGE. REINSTALLED BEACON, ALL CHECKED OK.
- [SDR DL72L982108](https://openairdocs.org/sdr/DL72L982108.md): Skin · cracked · Oct 9, 1998 · N513DA · Boeing 727232 · Wing, Plate/Skin
  > CRACK AT NR 4 SLAT IB GUIDE CUTOUT AFT END. REPAIRED PER MM 57-20-21.
- [SDR DL72L982107](https://openairdocs.org/sdr/DL72L982107.md): Stiffener · cracked · Oct 9, 1998 · N513DA · Boeing 727232 · Wing Miscellaneous Structure
  > SPAR STIFFENER CRACKED NR 3 SLAT IB TRACK. REPAIRED PER MM 57-20-21.
- [SDR DL72L982106](https://openairdocs.org/sdr/DL72L982106.md): Skin · cracked · Oct 9, 1998 · N513DA · Boeing 727232 · Wing, Plate/Skin
  > CRACK AT NR 3 SLAT OB GUIDE CUT OUT AFT END. REPAIRED PER MM 57-20-21.
- [SDR DL72L980552](https://openairdocs.org/sdr/DL72L980552.md): Sringer · cracked · Mar 10, 1998 · N513DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STRINGER 18A LT CRACKED 1 INCH THROUGH HORIZ FLANGE AT STA 945. REPAIRED PER M/M 53-12-0 LEVEL 1 TIME LIMITED REPAIR.
- [SDR DL72L980043](https://openairdocs.org/sdr/DL72L980043.md): Light · inoperative · Jan 7, 1998 · N513DA · Boeing 727232 · Emergency Lighting
  > RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED OVERWING EMERGENCY EXIT LIGHT BASE.
- [SDR DL72L972025](https://openairdocs.org/sdr/DL72L972025.md): Power Supply · inoperative · Oct 9, 1997 · N513DA · Boeing 727232 · Emergency Lighting
  > FOUND REAR CEILING EMER EXIT LIGHT OUT DURING L/O CHECK. REPLACED POWER SUPPLY, OPS CKS GOOD.
- [SDR DL72L971934](https://openairdocs.org/sdr/DL72L971934.md): Hose · leaking · Sep 30, 1997 · N513DA · Boeing 727232 · Hydraulic System, Main
  > SYS -A- HYD QTY DROPPED TO 0 ON T/O NR 1 ENG SYS -A- PUMP LO PRESS LT ILLUM AND PRESS DROPPED TO 2000 PSI. AFTER RETRACTION, FLUID RETURNED TO.75 GAL AND INCREASED WITH GEAR EXR AND FLAPS EXT 10 1.5 GAL ON LDG FLUID QTY INDICATED 3.0. REPLACED HYDRAULIC PRE
- [SDR DL72L970480](https://openairdocs.org/sdr/DL72L970480.md): Control Valve · inoperative · Mar 13, 1997 · N513DA · Boeing 727232 · Cabin Cooling System
  > AFTER TAKEOFF APPROXIMATELY 5,000 MSL, THE CARGO VALVE CLOSED. IT ILLUMINATED AT LEVEL OFF FL 280. THE CABIN CONTINUED TO CLB REACHING A MAX OF 9,000 FEET. CABIN ALT DIFF OF 6 PSID. ATB CVG. REPLACED RT PACK FLOW CONT VALVE. FOUND RT ACM INOPERATIVE.
- [SDR DL72L962781](https://openairdocs.org/sdr/DL72L962781.md): Control Module · leaking · Dec 29, 1996 · N513DA · Boeing 727232 · Aileron Control System
  > SHORTLY AFTER T/O, AILERON SYS-A LIGHT ACCOMPANIED BY A LOSS OF SY-A HYD FLUID, APPROX 2 MIN AFTER. FOUND AILERON FLIGHT CONTROL MODULE LEAKING. REPLACED SAME, CHECKS NORMAL.
- [SDR DL72L962613](https://openairdocs.org/sdr/DL72L962613.md): Wire Harness · burned · Dec 1, 1996 · N513DA · Boeing 727232 · Light System Wiring
  > DURING TAXI OUT, THE LEFT AFT CEILING PASSENGER CABIN LIGHTING CIRCUIT BREAKER POPPED. UNABLE TO RESET. FLIGHT ATTENDANT REPORTED A SMOKE SMELL. RETURNED TO GATE. REPAIRED BURNED WIRE BUNDLE ABOVE CEILING PANEL AT SEAT 10ABC PER BOEING WIRING PRACTICES MAN
- [SDR DL72L962516](https://openairdocs.org/sdr/DL72L962516.md): Light · inoperative · Nov 13, 1996 · N513DA · Boeing 727232 · Emergency Lighting
  > LT CENTER OVERWING EMERGENCY LIGHT AND AFT BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT PACK M955 AND AFT BULLNOSE LIGHT, ASSY OPS CHKS GOOD.
- [SDR DL72L961705](https://openairdocs.org/sdr/DL72L961705.md): Rib · cracked · Jul 17, 1996 · N513DA · Boeing 727232 · Leading Edge Devices
  > RIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00.
- [SDR DL72L961704](https://openairdocs.org/sdr/DL72L961704.md): Rib · cracked · Jul 17, 1996 · N513DA · Boeing 727232 · Leading Edge Devices
  > RIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00 PG 813.
- [SDR DL72L961281](https://openairdocs.org/sdr/DL72L961281.md): Door Frame · cracked · May 24, 1996 · N513DA · Boeing 727232 · Service Doors
  > THE L-2 DOOR FORWARD FRAME HAS A.5 CRACK EMANATING FROM THE LOWER INBOARD CORNER OF THE UPPER HINGE CUTOUT. THIS DAMAGE IS ADDRESSED BY B727 SRM 52-40-2, FIGURE 4. THERE IS AN EXISTING REPAIR LOCATED APPROXIMATELY 2 INCHES ABOVE THE UPPER HINGE CUTOUT. THE
- [SDR DL72L961267](https://openairdocs.org/sdr/DL72L961267.md): Fitting · cracked · May 23, 1996 · N513DA · Boeing 727232 · Leading Edge Devices
  > A.6875 INCH CRACK IN NR 5 SLAT AT ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-0.
- [SDR DL72L961266](https://openairdocs.org/sdr/DL72L961266.md): Beam · chafed · May 23, 1996 · N513DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > AFT SIDE OF MLG LOWER SIDE STRUT CHAFING INTO FWD SIDE OF WALKING BEAM RT WING. REPAIRED PER M/M 57-43-0.
- [SDR DL72L960681](https://openairdocs.org/sdr/DL72L960681.md): Pump · failed · Mar 15, 1996 · N513DA · Boeing 727232 · Engine Fuel Pump
  > NUMBER 2 ENGINE FLAMED OUT AT FL 310 NO INDICATIONS OF STALLS OR OTHER ENGINE DAMAGE. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL.
- [SDR DL72L960344](https://openairdocs.org/sdr/DL72L960344.md): Skin · gouged · Feb 13, 1996 · N513DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DAMAGE WAS FOUND ON THE UPPER TORQUE BOX SKIN DUE TO AN UNCONTAINED ENGINE FAILURE. THE DAMAGED SKIN SECTIONS WERE REMANUFACTURED AND REPLACED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 12 FEB 96.
- [SDR DL72L960246](https://openairdocs.org/sdr/DL72L960246.md): Comb Chamber · failed · Jan 30, 1996 · N513DA · Boeing 727232 · Turbine Engine Combustion Section
  > ON TAKEOFF, THE NR 1 ENGINE SHUTDOWN WITH FIRE WARNING IND FOLLOWING. AFTER A/C RETURNED, MAINTENANCE FOUND THE NR 1 ENGINE HAD A UNCONTAINED FAILURE. ALSO, AFTER FURTHER INSPECTION A/C SUBSTAINED MORE DAMAGE TO THE TAIL, FUSELAGE AND S-DUCT DUE TO PARTS COM
- [SDR DL72L954329](https://openairdocs.org/sdr/DL72L954329.md): Angle · cracked · Oct 26, 1995 · N513DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE LOWER ANGLE CRACKED AT THE I/B SIDE BEHIND UPSTOP. REPAIRED PER MM 57-54-0 FIG 812.
- [SDR DL72L954230](https://openairdocs.org/sdr/DL72L954230.md): Rib · cracked · Oct 26, 1995 · N513DA · Boeing 727232 · Leading Edge Devices
  > DURING THE SHOP INITIAL INSPECTION, THE INBOARD ACTUATOR RIB WAS FOUND TO HAVE CRACKED AT THE FORWARD LOWER CORNER WHERE THE RIB ATTACHES TO THE SLAT SPAR. THE RIB WAS REPAIRED PER SRM 57-54-0 FIG 804.
- [SDR DL72L954084](https://openairdocs.org/sdr/DL72L954084.md): Web · cracked · Oct 23, 1995 · N513DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND.125 INCH CRACK AT RT TORQUE BOX VERT WEB UPPER LIGHTENING HOLE, STA 1243. FOUND AT A-2 LTR CK, REPAIRED PER MM 53-11-0.
- [SDR DL72L954126](https://openairdocs.org/sdr/DL72L954126.md): Skin · cracked · Jun 21, 1995 · N513DA · Boeing 727232 · Ailerons
  > DURING SHOP INSPECTION, RIGHT WING OUTBOARD AILERON WAS FOUND WITH DENTED UPPER SKIN AT 37 INCHES FROM I/B END AND OVERSIDE HOLE SKIN TO RIB FASTENER HOLE AT 2ND FROM I/B RIB. REPAIRED PER SRM 57-50-5, FIG 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 = 'N513DA' AND deregistration_id = 'N513DA-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N513DA-2010-07-20/reports

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