# Service difficulty reports: N519DA, cancelled Apr 1, 2013

A list on [N519DA, cancelled Apr 1, 2013](https://openairdocs.org/deregistered/N519DA-2013-04-01.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 · 70 reports

- [SDR DL72S021251](https://openairdocs.org/sdr/DL72S021251.md): Light · inoperative · Oct 27, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT ROW 16 INOP AND LENS MISSING. RELAMPED AND REPLACED LENS-OPS NORMAL.
- [SDR DL72S021072](https://openairdocs.org/sdr/DL72S021072.md): Battery Pack · discharged · Sep 12, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > AFT EMERGENCY EXIT IDENTIFIER INOP. REPLACED BATTERY PACK.
- [SDR DL72S020917](https://openairdocs.org/sdr/DL72S020917.md): Valve · worn · Aug 6, 2002 · N519DA · Boeing 727232 · Engine Anti-Icing System
  > AIR RETURN TO CVG FOR HIGH OIL TEMP NUMBER 1 ENG. REPLACED FUEL HEAT VALVE, OP CHECKS NORMAL.
- [SDR DL72S020464](https://openairdocs.org/sdr/DL72S020464.md): Charger · inoperative · Apr 21, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > FOUND AFT OVERHEAD EMERGENCY LIGHT INOP FWD OF AIRSTAIR DOOR. REMOVED AND REPLACED BATTERY PACK CHARGING RACK. CHECKS GOOD.
- [SDR DL72S020258](https://openairdocs.org/sdr/DL72S020258.md): Battery Pack · discharged · Mar 5, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > FORWARD AISLE EMERGENCY SIGN INOPERATIVE. REPLACED BATTERY PACK AND RACK ASSEMBLY PER MM, OPS GOOD.
- [SDR DL72S020202](https://openairdocs.org/sdr/DL72S020202.md): Stiffener · cracked · Feb 16, 2002 · N519DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION OF THE WL 283 FASTENER HOLES ON THE RBL & LBL 17.8 BEAMS OF THE FS 1183 BULKHEAD REVEALED TOOLING DAMAGE IN THE TWO RT HOLES AND A CRACK INDICATION IN THE LOWER LT HOLE. THE INSPECTION WAS ACCOMPLISHED PER AD 99-18-05 AND BAC S/B 727-53-0210. THE
- [SDR DL72S020164](https://openairdocs.org/sdr/DL72S020164.md): Battery Pack · discharged · Feb 9, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER FOUND EMERGENCY LIGHT IN AFT STAIRWAY INOP. REPLACED BATTERY PACK.
- [SDR DL72S020163](https://openairdocs.org/sdr/DL72S020163.md): Battery Pack · discharged · Feb 9, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER FOUND EXTERIOR LIGHT FLASHING LEFT AFT FUSELAGE EMERGENCY LIGHT. REPLACED BATTERY PACK.
- [SDR DL72S020133](https://openairdocs.org/sdr/DL72S020133.md): Apu · malfunctioned · Feb 2, 2002 · N519DA · Boeing 727232 · APU Core Engine
  > ON APU SHUTDOWN FOUND APU EXHAUST FIRE OVER RIGHT WING COULD NOT PUT OUT HAD TO CALL FIRE DEPT TO PUT OUT FIRE. ALSO, FIRE BLISTERED WING TO FUSELAGE PANEL ABOVE APU EXHAUST ON FUSELAGE. FOUND APU BAD, REPLACED SAME.
- [SDR DL72S020097](https://openairdocs.org/sdr/DL72S020097.md): Battery Pack · discharged · Jan 26, 2002 · N519DA · Boeing 727232 · Emergency Lighting
  > FIRST CLASS EXIT LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S010821](https://openairdocs.org/sdr/DL72S010821.md): Door · missing · May 22, 2001 · N519DA · Boeing 727232 · Engine Cowling System
  > PANEL NR 3 ENGINE OIL SERVICE DOOR MISSING. REPLACED NR 3 OIL SERVICE DOOR.
- [SDR DL72S010738](https://openairdocs.org/sdr/DL72S010738.md): Attach Angle · cracked · May 9, 2001 · N519DA · Boeing 727232 · Leading Edge Devices
  > A 1 INCH CRACK COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIR PER M/M 57-54-000-8.
- [SDR DL72S010737](https://openairdocs.org/sdr/DL72S010737.md): Stiffener · cracked · May 9, 2001 · N519DA · Boeing 727232 · Wing Miscellaneous Structure
  > A 2 INCH CRACK WING L/E SPAR STIFFENER I/B TRACK NR 2 SLAT I/B STIFFENER. REPLACED ANGLE PER M/M 57-200021-8.
- [SDR DL72S001626](https://openairdocs.org/sdr/DL72S001626.md): Actuator · failed · Aug 21, 2000 · N519DA · Boeing 727232 · Landing Gear Actuator
  > WITH GEAR HANDLE DOWN AND MAIN GEAR LOCKED DOWN (GREEN LIGHTS) - EXCESSIVE TIME DELAY BEFORE NOSE GEAR SHOWED LOCKED DOWN AND GREEN LIGHT. NOTE: RED DOOR LIGHT STAYED ILLUM UNTIL NOSE GEAR GREEN LIGHT ILLUMINATED. THROTTLES WERE NOT AT IDLE AND FLAPS WERE
- [SDR DL72S001568](https://openairdocs.org/sdr/DL72S001568.md): Strap · corroded · Aug 3, 2000 · N519DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE BEAR STRAP AT THE C-3 DOORWAY WAS FOUND CORRODED ON THE INTERIOR SURFACE AT THE LOWER FWD CORNER OF THE DOORWAY CUTOUT. ER/A 334752-14AD REV A.
- [SDR DL72S001514](https://openairdocs.org/sdr/DL72S001514.md): Strap · tool damage · Aug 3, 2000 · N519DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TOOLING DAMAGE FOUND ON THE STA 784 LT FRAME REINFORCING STRAP. THE DAMAGE IS AT THE FOURTH FASTENER HOLE ABOVE THE FLOOR LINE. NO DAMAGE TO THE FRAME ITSELF. ER/A 334717-14AD REV A.
- [SDR DL72S001513](https://openairdocs.org/sdr/DL72S001513.md): Frame · tool damage · Aug 3, 2000 · N519DA · Boeing 727232 · Fuselage Main, Frame
  > TOOLING DAMAGE IN THE LT AND RT OVERWING EXIT FRAMES AT FS 761, DAMAGE FOUND IN BOTH THE I/B AND O/B CHORDS. THE LT FRAME DAMAGE AT THE 4TH FASTENER ABOVE THE FLOOR LINE. THE RT FRAME DAMAGE AT THE THIRD FASTENER ABOVE THE FLOOR LINE. ER/A 334726-14AD REV A
- [SDR DL72S001512](https://openairdocs.org/sdr/DL72S001512.md): Beam · misinstalled · Aug 3, 2000 · N519DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LBL AND RBL 17.8 VERTICAL BEAMS OF THE STA 1183 BULKHEAD HAVE SEVERAL FASTENERS INSTALLED FLUSH IN LIEU OF THE DRAWING REQUIRED BUTTON HEAD. ER/A 334720-14AD.
- [SDR DL72S001511](https://openairdocs.org/sdr/DL72S001511.md): Frame · cracked · Aug 2, 2000 · N519DA · Boeing 727232 · Fuselage Main, Frame
  > STA 1142.7 RT FRAME CRACKED/CORRODED JUST ABOVE C3 DOOR LOWER SILL. ER/A 334693-14AD REV A.
- [SDR DL72S001374](https://openairdocs.org/sdr/DL72S001374.md): Flap Track · corroded · Jul 20, 2000 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > NUMBER 1 FLAP TRACK LT WING WAS CORRODED IN THE BARREL NUT HOLE. TRACK CLEANED UP AND REPAIRED PER MM 57-52-0.
- [SDR DL72S001372](https://openairdocs.org/sdr/DL72S001372.md): Flap Track · corroded · Jul 20, 2000 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > NUMBER 2 FLAP TRACK LT WING WAS CORRODED IN THE BARREL NUT HOLE. TRACK CLEANED UP AND REPAIRED PER MM 57-52-0.
- [SDR DL72S001366](https://openairdocs.org/sdr/DL72S001366.md): Channel · worn · Jul 20, 2000 · N519DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FIREWALL CHANNEL WORN AT 5:30 POSITION FS 1343 AT MATING SURFACE FOR NR 2 ENG COWLING. REPAIRED PER 53-11-0.
- [SDR DL72S001478](https://openairdocs.org/sdr/DL72S001478.md): Flap Track · corroded · Jul 12, 2000 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > NR 3 FLAP TRACK CORRODED NR 116. REPAIRED PER M/M.
- [SDR DL72S001476](https://openairdocs.org/sdr/DL72S001476.md): Flap Track · corroded · Jul 12, 2000 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 FLAP TRACK CORRODED CARD NR 115. REPAIRED PER M/M.
- [SDR DL72S000881](https://openairdocs.org/sdr/DL72S000881.md): Switch · failed · May 4, 2000 · N519DA · Boeing 727232 · Engine Oil Indicating System
  > INFLIGHT SHUTDOWN DUE TO NR 2 ENG FILTER BYPASS LIGHT ON. REMOVED AND INSPECTED MAIN OIL FILTER. NO CONTAMINENTS FOUND. CHIP DET CHECKS CLEAN. REPLACED FILTER BYPASS SWITCH.
- [SDR DL72S000676](https://openairdocs.org/sdr/DL72S000676.md): Pcu · malfunctioned · Apr 8, 2000 · N519DA · Boeing 727232 · Rudder Control System
  > RUDDER LOAD LIMITER FOLLOWING MEL PROCEDURES WHEN REENGAGED SYSTEM A RUDDER BEFORE FLAP EXTENSION RECEIVED UNCOMMANDED LOWER RUDDER YAW 1 INDICE RT SYS A RUDDER THEN TURNED OFF AGAIN. STBY ON AND LOWER RUDDER RETURNED TO NORMAL. CENTERED POSITION. LANDING M
- [SDR DL72S000797](https://openairdocs.org/sdr/DL72S000797.md): Skin · cracked · Mar 20, 2000 · N519DA · Boeing 727232 · Leading Edge Devices
  > NR 5 SLAT LOWER SKIN WORN O/B OF O/B ALIGNMENT SPADE. CUT INNER SKIN MADE NEW SKIN DOUBLERS. REPAIRED PER MM 57-54-0 FIG 801.
- [SDR DL72S000551](https://openairdocs.org/sdr/DL72S000551.md): Skin · cracked · Mar 20, 2000 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > A.5 INCH CRACK ON NR 2 MIDFLAP LOWER COVE SKIN AT THE I/B ROD CUTOUT.
- [SDR DL72S000305](https://openairdocs.org/sdr/DL72S000305.md): Battery · discharged · Feb 13, 2000 · N519DA · Boeing 727232 · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK.
- [SDR DL72S992514](https://openairdocs.org/sdr/DL72S992514.md): Battery Pack · discharged · Nov 14, 1999 · N519DA · Boeing 727232 · Emergency Lighting
  > FOUND ON LAYOVER AFT EMERGENCY CEILING LIGHT STROBING. REPLACED BATTERY CHARGER AND BATTERY.
- [SDR DL72S991594](https://openairdocs.org/sdr/DL72S991594.md): Brake · failed · Jul 15, 1999 · N519DA · Boeing 727232 · Brake
  > AFTER TAXI TO RUNWAY, A/C REQUIRED APPROX 1.4 EPR TO INITIATE TAXI. WHEN A/C MOVED A VERY LOUD SHUDDER WAS FELT ON LT SIDE OF A/C. MAINT TOW BACK TO GATE. REPLACED NR 1 BRAKE AND TIRE ASSY DUE NR 1 BRAKE FAILUR.
- [SDR DL72S991512](https://openairdocs.org/sdr/DL72S991512.md): Bulb · failed · Jul 4, 1999 · N519DA · Boeing 727232 · Emergency Lighting
  > ON L/O 2 CK, FOUND NO SMOKING LIGHTS INOP AT 4CD, 14DEF, 19DEF, 23DEF. ALSO, FOUND FASTEN SEAT BELT LIGHTS AT 4CD, 2AB, 20DEF INOP. RELAMPED, ALL CHECK GOOD.
- [SDR DL72S990595](https://openairdocs.org/sdr/DL72S990595.md): Power Supply · inoperative · Mar 19, 1999 · N519DA · Boeing 727232 · Emergency Lighting
  > ON S/C FOUND E PATH LIGHTING AT SECTION 20 TO 26 INOP. FOUND BAD FUSE ON AFT PWR SUPPLY. REPLACED AFT PWR SUPPLY, OPS NORMAL NOW.
- [SDR DL72S990294](https://openairdocs.org/sdr/DL72S990294.md): Light · inop · Feb 14, 1999 · N519DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED RACK, NOW CKS NORMAL.
- [SDR DL72S990293](https://openairdocs.org/sdr/DL72S990293.md): Battery Pack · discharged · Feb 14, 1999 · N519DA · Boeing 727232 · Emergency Lighting
  > MID CABIN SEAT EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK AND BATTERY PACK, ALL OPS NORMAL.
- [SDR DL72S990273](https://openairdocs.org/sdr/DL72S990273.md): Skin · cracked · Feb 9, 1999 · N519DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-481, STRG 4L, SKIN LAP SPLICE, REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 360-481. INTERNAL HFEC INSPECTION CONFIRMED 10 CRACKS ALONG THE LOWER ROW OF
- [SDR DL72S990272](https://openairdocs.org/sdr/DL72S990272.md): Skin · cracked · Feb 9, 1999 · N519DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-481, STRG 4R, SKIN LAP SPLICE REPAIR FOR CRACKED FASTENER HOLES. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360-481 REVEALED CRACK INDICATIONS. HFEC INTERNAL INSPECTION CONFIRMED A TOTAL OF 4 CRACKS IN TWO SEPERATE FRA
- [SDR DL72S990258](https://openairdocs.org/sdr/DL72S990258.md): Skin · cracked · Feb 6, 1999 · N519DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FS 528, STRG 4, REPAIR FOR SKIN CRACK. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE GAVE A CRACK INDICATION. HFEC INTERNAL INSPECTION WAS THEN ACCOMPLISHED ALONG THE ENTIRE LENGTH OF THE PANEL WITH ONLY ONE CRACK FINDING. THE CRACK WAS
- [SDR DL72S990065](https://openairdocs.org/sdr/DL72S990065.md): Skin · cracked · Jan 11, 1999 · N519DA · Boeing 727232 · Leading Edge Devices
  > 4.5 INCH CRACK IN NR 8 SLAT COVE SKIN ANGLE AT O/B UPSTOP PAD. REPAIR PER MM 57-54-0 PG 816.
- [SDR DL72S982341](https://openairdocs.org/sdr/DL72S982341.md): Stop · loose · Nov 12, 1998 · N519DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION PER REQUIREMENTS OF AD 94-07-08, LOOSE SLAT STOP ATTACH BOLTS WERE FOUND LOOSE FOR THE NR 6, 7 & 8 SLATS. EACH OF THESE SLAT LOCATIONS WERE MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-171. THE MODIFICATION WAS DOCUMENTED PER ER/A 366092
- [SDR DL72S981278](https://openairdocs.org/sdr/DL72S981278.md): Spar Web · cracked · Jun 14, 1998 · N519DA · Boeing 727232 · Wing Spar
  > WING CENTER SECTION REAR SPAR, WEB RBL 3 AND RBL 9: REPAIR FOR WEB CRACKS. THE WING CENTER SECTION SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER SPAR CAP. THE CRACKS WERE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCO
- [SDR DL72S981175](https://openairdocs.org/sdr/DL72S981175.md): Skin · cracked · Jun 2, 1998 · N519DA · Boeing 727232 · Leading Edge Devices
  > FOUND AT B2 LETTER CHECK, 2 CRACKS.75 INCH AND 2 INCH AT NR 4 L/E FLAP O/B HINGE CUTOUT. REPAIRED PER ERA 364950-14 AND M/M 57-53-0.
- [SDR DL72S972133](https://openairdocs.org/sdr/DL72S972133.md): Skin · hole · Oct 22, 1997 · N519DA · Boeing 727232 · Rudder, Plate/Skin
  > HOLE IN LT L/E SKIN, 34 INCH FROM BOTTOM. INSTALLED REPAIR DOUBLER PER SRM 55-40-3 FIG. 1.
- [SDR DL72S972132](https://openairdocs.org/sdr/DL72S972132.md): Skin · hole · Oct 22, 1997 · N519DA · Boeing 727232 · Rudder, Plate/Skin
  > HOLE IN LEFT L/E SKIN ON LOWER RUDDER. REPAIRED PER SRM 55-40-3.
- [SDR DL72S972131](https://openairdocs.org/sdr/DL72S972131.md): Skin · gouged · Oct 22, 1997 · N519DA · Boeing 727232 · Rudder, Plate/Skin
  > SKIN GOUGED AT LOWER END OF LOWER RUDDER. INSTALLED DOUBLER PER SRM 55-40-3, FIG 1.
- [SDR DL72S972245](https://openairdocs.org/sdr/DL72S972245.md): Angle · cracked · Oct 21, 1997 · N519DA · Boeing 727232 · Leading Edge Devices
  > THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION AT HMV VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY STOP DRILLING CRACK AND INSTALLING A DOUBLER.
- [SDR DL72S972186](https://openairdocs.org/sdr/DL72S972186.md): Stringer · cracked · Oct 14, 1997 · N519DA · Boeing 727232 · Wing, Longeron/Stringer
  > STRINGER TO RIB CRACK LEFT WING STA 686.5 AT STR 12. REPAIRED PER M/M57-13-0 FIG 804.
- [SDR DL72S972056](https://openairdocs.org/sdr/DL72S972056.md): Stringer · cracked · Oct 13, 1997 · N519DA · Boeing 727232 · Wing, Longeron/Stringer
  > HFEC INSPECTION PER OPN NO 8602 AS SHOWS CRACK ON STRINGER TO RIB AT STA 686.5 5-10. PERFORMED DYE CHECK TO IDENTIFY CRACK. NO STOP DRILL HOLE REQUIRED. DISCONNECTED FUEL DUMP LINE AT STA 686.5 - 700 FOR ACCESS TO REPAIR. DRILLED UP REPAIR DOUBLERS PER MM
- [SDR DL72S972119](https://openairdocs.org/sdr/DL72S972119.md): Bracket · cracked · Oct 10, 1997 · N519DA · Boeing 727232 · Leading Edge Slat Actuator
  > THE NR 2 L/E FLAP ACTUATOR SUPPORT BRACKETS I/B AND O/B ARE CRACKED. REMOVED SUPPORT BRACKETS AND BEGAN REPAIRS PER M/M 57-20-21 FIG 807, FINISHED REPAIR PER MM 57-20-21 FIG 807.
- [SDR DL72S972078](https://openairdocs.org/sdr/DL72S972078.md): Angle · cracked · Oct 9, 1997 · N519DA · Boeing 727232 · Trailing Edge Flaps
  > AFT LOWER CHORD ANGLE IS CRACKED AT I/B AFT FLAP TRACK CUTOUT I/B AND O/B CORNERS. INSTALLED DOUBLER PER M/M 57-52-0 FIG 802.

Next page: https://openairdocs.org/deregistered/N519DA-2013-04-01/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 = 'N519DA' AND deregistration_id = 'N519DA-2013-04-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N519DA-2013-04-01/reports

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