# Service difficulty reports: N402DA, cancelled Oct 3, 2012

A list on [N402DA, cancelled Oct 3, 2012](https://openairdocs.org/deregistered/N402DA-2012-10-03.md).

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

- [SDR DL72S001794](https://openairdocs.org/sdr/DL72S001794.md): Fuse · failed · Sep 17, 2000 · N402DA · Boeing 727232 · Emergency Lighting
  > WHILE TESTING EMERGENCY LIGHTS FOUND FIRST CLASS LIGHTS NOT WORKING. FOUND FUSE BAD IN F/C BATTERY PACK. REPLACED FUSE, CKS OK.
- [SDR DL72S001793](https://openairdocs.org/sdr/DL72S001793.md): Light · inoperative · Sep 17, 2000 · N402DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT AT 22D INOP. LIGHTS DISCONNECTED UNDER SEAT. RECONNECTED AFT MODULE PULLED AWAY FROM SEAT. INSTALLED NEW MODULE. CKS OK.
- [SDR DL72S001563](https://openairdocs.org/sdr/DL72S001563.md): Web · cracked · Aug 15, 2000 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.75 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB TOP OF WEB AT STA 1226. A.5 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB TOP OF WEB AT STA 1214. REPAIRED PER MM 53-11-0.
- [SDR DL72S001297](https://openairdocs.org/sdr/DL72S001297.md): Power Supply · inoperative · Jul 8, 2000 · N402DA · Boeing 727232 · Emergency Lighting
  > FORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED FORWARD POWER SUPPLY, CKS GOOD PER MM.
- [SDR DL72S000913](https://openairdocs.org/sdr/DL72S000913.md): Warning Light · false indication · May 7, 2000 · N402DA · Boeing 727232 · Auxiliary Gear (Tail Skid)
  > DURING CLIMBOUT EWR HAD A TAIL SKID LIGHT. AIRCRAFT WAS ON A MAINTENANCE FERRY TO ATL. NO OBVIOUS PROBLEM NOTICED ON INSPECTION. PROBLEM RELATED TO INDICATION ONLY. FLIGHT WAS AN AIR TURNBACK AFTER TAKEOFF. CLEANED PROX SWITCH.
- [SDR DL72S991372](https://openairdocs.org/sdr/DL72S991372.md): Skin · cracked · Jun 16, 1999 · N402DA · Boeing 727232 · Service Doors
  > REF NRC 52 - TPA LETTER CHECK C-1,.5 INCH CRACK IN DOOR SKIN, R-1 DOOR LOWER FWD CORNER. INSTALLED DOUBLER PER M/M 52-11-01, NR 8.
- [SDR DL72S991371](https://openairdocs.org/sdr/DL72S991371.md): Skin · cracked · Jun 16, 1999 · N402DA · Boeing 727232 · Passenger/Crew Doors
  > REF NRC 53 TPA LETTER CHECK C-1,.5 INCH CRACK IN R-1 DOOR SKIN AT LWR AFT CORNER. INSTALLED DOUBLER PER M/M 52-11-01, NR 8.
- [SDR DL72S990460](https://openairdocs.org/sdr/DL72S990460.md): Skin · cracked · Mar 3, 1999 · N402DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED SEVERAL CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH
- [SDR DL72S990459](https://openairdocs.org/sdr/DL72S990459.md): Skin · cracked · Mar 3, 1999 · N402DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 35 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPA
- [SDR DL72S982329](https://openairdocs.org/sdr/DL72S982329.md): Frame · cracked · Nov 11, 1998 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT LETTER CK B-2, AFT ENTRY DOOR CUTOUT LT FRAME HAS.3125 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-8.
- [SDR DL72S981468](https://openairdocs.org/sdr/DL72S981468.md): Wire · damaged · Jul 14, 1998 · N402DA · Boeing 727232 · Light System Wiring
  > FIRST CLASS EMER ESCAPE PATH LIGHTING INOP. FOUND BLOWN POWER SUPPLY FUSE AND MELTED WIRING AT C/P. REPLACED POWER SUPPLY AND BATTERY, REPAIRED DAMAGED WIRING. OPN TEST OK.
- [SDR DL72S980771](https://openairdocs.org/sdr/DL72S980771.md): Spar · misdrilled · Apr 2, 1998 · N402DA · Boeing 727232 · Trailing Edge Flaps
  > NR 3 MIDFLAP/ REAR SPAR/WBL 124/AD 94-07-08 - OS HOLE: OVERSIZED HOLE IN REAR SPAR UPR CHORD AND UPPER SKIN IN AD INSPECTION AREA. FOUND DURING ACCOMPLISHMENT OF EO, 4-58705-3AD MODIFICATION. FAA AMOC REC'D TO INSTALL OS HI-LOK IN HOLE.
- [SDR DL72S980660](https://openairdocs.org/sdr/DL72S980660.md): Blkhd Stiffener · cracked · Mar 25, 1998 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CRACKS WERE FOUND IN THE LBL AND RBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE FS 1183 BLKHD. THE CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIRED PER ERA 331543-14.
- [SDR DL72S980749](https://openairdocs.org/sdr/DL72S980749.md): Angle · cracked · Mar 20, 1998 · N402DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, A DOUBLER ON THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED ANGLE, 32 FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 FIG 802 BY INSTALLING/REPLACING THE REPAIR DOUBLER.
- [SDR DL72S980748](https://openairdocs.org/sdr/DL72S980748.md): Angle · cracked · Mar 20, 1998 · N402DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER CLOSEOUT ANGLE, 18 FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.
- [SDR DL72S980820](https://openairdocs.org/sdr/DL72S980820.md): Rib · cracked · Mar 19, 1998 · N402DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, THE NR 1 MIDFLAP WAS FOUND WITH IB AFT CLOSEOUT RIB CRACKED AT LOWER AFT CORNER. THE RIB WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER 727 MM 57-52-0,FIG. 808.
- [SDR DL72S980931](https://openairdocs.org/sdr/DL72S980931.md): Doubler · cracked · Mar 18, 1998 · N402DA · Boeing 727232 · Trailing Edge Flaps
  > REPAIR DOULBERS CRACKED IN THREE PLACES 19, 32 AND 37 FROM I/B END OF LOWER AFT CHORD ANGLE NR 2 MIDFLAP. REPAIRED BY REPLACING DOUBLERS PER BOEING M/M 57-52-0 FIG 802. ON NON-ROUTINE CARDS NR 005932 AND 005933.
- [SDR DL72S980662](https://openairdocs.org/sdr/DL72S980662.md): Skin · cracked · Mar 18, 1998 · N402DA · Boeing 727232 · Vertical Stabilizer
  > SKIN CRACKED, PREVIOUSLY STOP DRILLED CRACK AT BASE OF VERTICAL STAB FRONT SPAR, RT SIDE. REMOVED FASTENERS. CUT OUT DAMAGED SECTION OF SKIN. E/C INSP OK. FABRICATED FILLER AND BEGAN FABRICATION OF DOUBLER PER SRM 55-30-3. OK TO INSTALL DOUBLER. STARTED
- [SDR DL72S980640](https://openairdocs.org/sdr/DL72S980640.md): Web · cracked · Mar 18, 1998 · N402DA · Boeing 727232 · Vertical Stabilizer
  > WEB CRACKED VERT STAB INTERIOR, VERTICAL WEB OVER S-DUCT IS CRACKED AT BOTH LOWER CORNERS (2 PLACES). REMOVED FASTENERS DYE PEN'D STOP DRILL, NO CRACK NOTED AFTER STOP DRILL HOLES ON BOTH SIDES, FABRICATED NEW DOUBLERS AS PER SRM 53-10-4 FIG 17. INSTALLED DO
- [SDR DL72S980234](https://openairdocs.org/sdr/DL72S980234.md): Skin · corroded · Jan 27, 1998 · N402DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 680, STRINGER 26L-28L, REPAIR FOR CORROSION CUTOUTS. TWO AREAS OF CORROSION WERE CUTOUT OF THE FUSELAGE SKIN AT FS 680 BETWEEN STRINGERS 26L AND 28L. THE CUTOUTS WERE REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 363860-14, REV A.
- [SDR DL72S980229](https://openairdocs.org/sdr/DL72S980229.md): Pressure Deck · cracked · Jan 26, 1998 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON A2 LETTER CK, 1 INCH CRACK AT LEFT MLG W/W PRESSURE DECK BEAD STA 950 AT LBL 63. STOP DRILLED CRACK PER MM 53-14-0.
- [SDR DL72S980228](https://openairdocs.org/sdr/DL72S980228.md): Web · cracked · Jan 26, 1998 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON A2 LETTER CK, TORQUE BOX WEB CRACKED.5 INCH AT DOUBLER UPPER LIGHTNING HOLE STA 1223 AND.25 INCH CRACK AT LIGHTNING HOLE FWD STA 1243. REPAIR PER ERA 363858-14 AND M/M 53-11-0.
- [SDR DL72S980227](https://openairdocs.org/sdr/DL72S980227.md): Angle · cracked · Jan 26, 1998 · N402DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND 0N A2 LETTER CK, NR 3 L/E FLAP ACTUATOR BOX CRACKED AT OUTBOARD LOWER CORNER. REPAIRED PER MM 57-20-21 AND ERA.
- [SDR DL72S972120](https://openairdocs.org/sdr/DL72S972120.md): Bulb · failed · Oct 20, 1997 · N402DA · Boeing 727232 · Emergency Lighting
  > AFT MOST RED BULB INOP ON FLOOR PROX LIGHT STRIP. REPLACED BULB SOCKET.
- [SDR DL72S971167](https://openairdocs.org/sdr/DL72S971167.md): Rib · cracked · Jun 16, 1997 · N402DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A1 LETTER CK,.75 IN CRACK IN RADIUS OF NR 6 SLAT RIBS I/B AND O/B SIDES OF ACTUATOR AT COVE SKIN ATTACH. REPAIRED PER MM 57-54-0.
- [SDR DL72S970045](https://openairdocs.org/sdr/DL72S970045.md): Actuator · failed · Jan 10, 1997 · N402DA · Boeing 727232 · Leading Edge Slat Actuator
  > SYSTEM-A QTY WENT TO 0, SYS-A HYD PUMPS WERE TURNED OFF PRIOR TO LOSING PRESS. TOWED FROM TAXIWAY. NR 5 LE FLAP ACT FAILED. REPLACED LE ACT, CHECK CASE DRAIN FILTERS OK.
- [SDR DL72S962510](https://openairdocs.org/sdr/DL72S962510.md): Skin · cracked · Nov 12, 1996 · N402DA · Boeing 727232 · Elevator, Plate/Skin
  > FOUND A.5 INCH CRACK IN LT ELEVATOR TOP SKIN, FWD OF OUTBD END OF TAB CUTOUT. REPAIRED PER SRM 55-20-3.
- [SDR DL72S962119](https://openairdocs.org/sdr/DL72S962119.md): Post · cracked · Sep 12, 1996 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND CRACK AT THE INBOARD LOWER CORNER OF THE L4 COCKPIT WINDOW. REPAIRED IN ACCORDANCE WITH DER FORM 8110-3, DER DESIGNATIONSO-831, DATED 9/12/96.
- [SDR DL72S962053](https://openairdocs.org/sdr/DL72S962053.md): Door Frame · cracked · Sep 3, 1996 · N402DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND IN THE FOURTH FASTENER HOLE LOCATED ABOVE THE CABIN FLOOR LINE ON THE LT STA 761 OVERWING EXIT FRAME. THE HOLE WAS OVERSIZED TO 0.340 AND A HIGH FREQUENCY EDDY CURRENT INSPECTION SHOWED THAT THE CRACK NO LONGER EXISTED IN THE FASTENER HOLE.
- [SDR DL72S962044](https://openairdocs.org/sdr/DL72S962044.md): Stringer · cracked · Aug 28, 1996 · N402DA · Boeing 727232 · Vertical Stabilizer
  > THE VERTICAL STABILIZER STRINGER 9L WAS FOUND CRACKED AT FIN STA 157.2, DURING EXECUTION OF EO 4-59253-12AD. THIS EO CALLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9L CANNOT BE REPAIRED PER SRM PROCEDURE DUE TO SPACE LIMITATION ON INBOARD FLANGE. STRIN
- [SDR DL72S960986](https://openairdocs.org/sdr/DL72S960986.md): Skin · cracked · Apr 24, 1996 · N402DA · Boeing 727232 · Passenger/Crew Doors
  > FOUND ON LETTER CHECK, MAIN ENTRY DOOR UPPER AFT SKIN HAS A CRACK EXTENDING FROM FASTENER. REPAIR: REPAIRED PER M/M 52-12-0, NR 10, FIG 806 10P PER PS 900-5-1, NR 04.
- [SDR DL72S960985](https://openairdocs.org/sdr/DL72S960985.md): Actuator Bracket · cracked · Apr 24, 1996 · N402DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON F1 LETTER CHECK, NR 5 LE FLAP ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72S960984](https://openairdocs.org/sdr/DL72S960984.md): Stiffener · cracked · Apr 24, 1996 · N402DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON F1 LETTER CHECK, 1.25 INCH CRACK AT L/E EDGE SPAR VERTICAL STIFFENER AFT OF NR 6 SLAT OUTBOARD TRACK OUTBOARD SIDE. REPLACED STIFFENER PER MM 57-20-21.
- [SDR DL72S960983](https://openairdocs.org/sdr/DL72S960983.md): Actuator Bracket · cracked · Apr 24, 1996 · N402DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON F1 LETTER CHECK, NR 1 SLAT ACTUATOR INBOARD MOUNT BRACKET CRACKED AT UPPER MOUNT BOLT. REPAIRED PER MM57-20-21.
- [SDR DL72S960874](https://openairdocs.org/sdr/DL72S960874.md): Rib · cracked · Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge Devices
  > RIB MARKED NR 14 WAS FOUND CRACKED IN THE LOWER RADIUS NEAR ATTACH ANGLE. THE NOTED RIB WAS REPAIRED IN COMPLIANCE WITH MM 57-54-0 FIGURE 805, FOR NR 2 L/E SLAT.
- [SDR DL72S960873](https://openairdocs.org/sdr/DL72S960873.md): Slat · cracked · Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge Devices
  > THE INNR SKIN WAS FOUND CRACKED BY THE TELESCOPING ANTI-ICE DUCT. REPAIRED INNR SKIN PER SRM 57-50-3, FOR NR 2 L/E SLAT.
- [SDR DL72S960872](https://openairdocs.org/sdr/DL72S960872.md): Rib · cracked · Apr 16, 1996 · N402DA · Boeing 727232 · Leading Edge Devices
  > THE 3RD RIB WAS FOUND CRACKED. REPAIRED RIB PER MM 57-54-0, FOR NR 2 L/E SLAT.
- [SDR DL72S960340](https://openairdocs.org/sdr/DL72S960340.md): Cadc · failed · Feb 14, 1996 · N402DA · Boeing 727232 · Air Data Computer
  > AFTER TAKEOFF, TCAS DISPLAYED ALL FAILED AND MAIN TCAS SCREEN SHOWED NR 1 XPONDER DATA BUS AND ALT DATA. CENTER ADVISED THEY RECEIVED SQUAWK, BUT NO ALT READOUT. AT FL 310 LEVEL OFF AND CRUISE MACH.80, A/C BEGAN MILD DUTCH ROLL. ROLL CEASED WHEN SPEED SLOW
- [SDR DL72S951139](https://openairdocs.org/sdr/DL72S951139.md): Skin · crack · Mar 16, 1995 · N402DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING E-1 LETTER CHECK, SKIN CRACKED.5 INCH VERTICAL STAB LT SIDE BELOW ACCESS PNL 9501. REPAIRED PER SRM 55-30-3 FIG 1.
- [SDR DL72S951137](https://openairdocs.org/sdr/DL72S951137.md): Slat · crack · Mar 16, 1995 · N402DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING E-1 LETTER CHECK, 2 INCH BY.25 INCH CRACKS BELOW ANTI-ICE TUBE ON NBR 2 L/E SLAT. REPAIRED PER MM 57-54-0 PG 807A.
- [SDR DL72S950791](https://openairdocs.org/sdr/DL72S950791.md): Panel · shorted · Feb 21, 1995 · N402DA · Boeing 727232 · Central Display
  > DURING CRUISE, HAD ELECTRICAL BURNING SMELL AND SMOKE COMING FROM FLIGHT ENGINEERS PANEL THROUGH GASPER FAN SWITCH HOLE. DEACTIVATED CIRCUITS, ODOR CEASED. FOUND P4-22 PANEL SHORTED TO GROUND. REPLACED PANEL, OPERATION NORMAL.

## 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 = 'N402DA' AND deregistration_id = 'N402DA-2012-10-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N402DA-2012-10-03/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.