# Service difficulty reports: N494DA, cancelled Jun 22, 2000

A list on [N494DA, cancelled Jun 22, 2000](https://openairdocs.org/deregistered/N494DA-2000-06-22.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 · 88 reports

- [SDR DL72S992449](https://openairdocs.org/sdr/DL72S992449.md): Fire Detector · malfunctioned · Nov 6, 1999 · N494DA · Boeing 727232 · Fire Detection
  > APU FIRE WARNING WITH LIGHT AND BELL AT 100 KNOTS. REJECTEDTAKEOFF. STOPPED ACFT USING MODERATE, EVEN BRAKING. 16 DEG COAT 168,000 LBS. INSPECTED ACFT PER MM 05-52-121. NO DISCREPANCIES NOTED. FWD FIRE WARNING TO MCO PER MEL 26-00-01B. PULLED AND CO
- [SDR DL72S991901](https://openairdocs.org/sdr/DL72S991901.md): Battery Pack · discharged · Aug 25, 1999 · N494DA · Boeing 727232 · Emergency Lighting
  > DURING LAYOVER CHECK, FOUND LEFT OVERWING MID POSITION EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK OPS NORMAL.
- [SDR DL72S991636](https://openairdocs.org/sdr/DL72S991636.md): Strap · out of position · Jul 20, 1999 · N494DA · Boeing 727232 · Passenger/Crew Doors
  > DOOR 2L SAFETY WAS REPORTED BY F/A TO BE FLAPPING AGAINST OUTSIDE OF A/C AFTER T/O. INSPECTED AREA, NO APPRECIABLE DAMAGE NOTED. INSPECTED INTAKE NR 1 ENG, A-OK. REPLACED DAMAGED STRAP.
- [SDR DL72S991629](https://openairdocs.org/sdr/DL72S991629.md): Frame · damaged · Jul 20, 1999 · N494DA · Boeing 727232 · Cargo/Baggage Doors
  > C-3 CARGO DOOR / DOOR STOP FITTING MODIFICATION / OMIT FRAME DOUBLER REPAIR: AD 90-06-09. DURING CURRENT SHOP VISIT, MTC ACCOMPLISHING DOOR STOP FITTING REPLACEMENT PER EO 4-59432-3AD. DAMAGE WAS FOUND TO FWD EDGE FRAME REQUIRING REPLACEMENT. EO REQUIRES T
- [SDR DL72S991351](https://openairdocs.org/sdr/DL72S991351.md): Bracket · cracked · Jun 15, 1999 · N494DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72S991350](https://openairdocs.org/sdr/DL72S991350.md): Skin · cracked · Jun 15, 1999 · N494DA · Boeing 727232 · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN CRACKED DAMAGED APPROX.5 INCH, 24 INCHES OUTBD OF TAB. RIGHT ELEVATOR UPPER SKIN CRACKED.375 INCH APPROX 20 INCHES OUTBD OF TAB. REPAIRED PER ERA367622-14 CODE 4-55-21.
- [SDR DL72S991043](https://openairdocs.org/sdr/DL72S991043.md): Throttle Rod · loose · May 12, 1999 · N494DA · Boeing 727232 · Power Lever
  > AT 10,000 FEET ON DESCENT, THE NR 3 ENGINE WENT TO 95 PERCENT N1 AND EGT TO 610 ENGINE SHUTDOWN WITH THE PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST. FOUND THROTTLE ROD OFF OF THRU SHAFT AT GEARBOX. REINSTALLED SAME ENGINE CHECKS NORMAL ON RUN UP ALL PARAMETERS
- [SDR DL72S990231](https://openairdocs.org/sdr/DL72S990231.md): Engine · failed · Feb 4, 1999 · N494DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 1 ENG FAILED IN FLIGHT AT APPROX FL305. AIRCRAFT SHUTTERED FOR ABOUT 10 SEC THEN ENG FLAMED OUT, EGT ROSE TO ABOUT 780C, OIL TEMP ROSE TO 140C. RETURNED TO SLC. FOUND METAL IN TAILPIPE. REPLACED ENGINE.
- [SDR DL72S990180](https://openairdocs.org/sdr/DL72S990180.md): Skin · cracked · Jan 25, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE ALONG THE PANEL LENGTH FROM FS 681 TO 740 INDICATED POTENTIAL CRACKS IN THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 31 CRACKED FASTENER HOLES ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. THE
- [SDR DL72S990179](https://openairdocs.org/sdr/DL72S990179.md): Skin · cracked · Jan 25, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE ON THE PANEL BETWEEN FS 481 AND 680 INDICATED POSSIBLE CRACKS. INTERNAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS IN THE LOWER SKIN PANEL CONFIRMED A TOTAL OF 46 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE
- [SDR DL72S990178](https://openairdocs.org/sdr/DL72S990178.md): Skin · cracked · Jan 24, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF LFEC INSPECTIONS OF THE LOWER ROW OF FASTENERS IN THE STRINGER 4R LAP SPLICE OF THE FS 360 TO 481 PANEL, CRACK INDICATIONS WERE NOTED. INTERNAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS OF THE LOWER SKIN PANEL CONFIRMED 11
- [SDR DL72S982449](https://openairdocs.org/sdr/DL72S982449.md): Battery Pack · discharged · Nov 27, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > LEFT FWD AND MID OVERWING EMERG LIGHTS INOP. ALSO, AFT SERVICE DOOR EXIT SIGN INOP, FOUND ON L/O. REPAIRED WIRE AT AFT SERVICE DOOR EMERG EXIT SIGN. ALSO, REPLACED PACK. REPLACED PACK AT MID OVERWING EMERG RACK. REPLACED RACK AND PACK FOR FWD OVERWING EME
- [SDR DL72S982383](https://openairdocs.org/sdr/DL72S982383.md): Power Supply · inop · Nov 17, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > EMERG EXIT LIGHT SIGN OVERHEAD AISLE AT ROW 20 INOP ON TEST. REPLACED FUSES IN POWER SUPPLY, OPN CKS OK.
- [SDR DL72S982382](https://openairdocs.org/sdr/DL72S982382.md): Battery Pack · discharged · Nov 17, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > LEFT OVERWING EMERG LIGHT MID INOP. REPLACED BATTERY PACK AND SWITCHING CHARGING UNIT, OPS OK.
- [SDR DL72S982324](https://openairdocs.org/sdr/DL72S982324.md): Angle · cracked · Nov 10, 1998 · N494DA · Boeing 727232 · Wing Miscellaneous Structure
  > LWR CHORD ANGLE 1 INCH CRACK AT FWD END BELOW NR 8 SPOILER ACTUATOR. REPAIRED PER M/M 57-20-22 FIG 806.
- [SDR DL72S982323](https://openairdocs.org/sdr/DL72S982323.md): Bracket · cracked · Nov 10, 1998 · N494DA · Boeing 727232 · Leading Edge Devices
  > NR 6 L/E FLAP ACT ATTACH BRACKET CRACKED AT UPPER AND LWR ENDS. REPAIRED PER M/M 57-20-21 FIG 807.
- [SDR DL72S982322](https://openairdocs.org/sdr/DL72S982322.md): Skin · cracked · Nov 10, 1998 · N494DA · Boeing 727232 · Trailing Edge Flaps
  > A.375 INCH CRACK AT NR 2 MIDFLAP LOWER SURFACE AT CUTOUT I/B OF NR 4 MIDFLAP FAIRING. REPAIRED PER M/M 57-52-0.
- [SDR DL72S981511](https://openairdocs.org/sdr/DL72S981511.md): Battery Pack · discharged · Jul 21, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > LEFT WING OVERWING AFT EMERGENCY LIGHT ASSY BULB BLINKS INTERMITTENTLY. REPLACED BATTERY PACK. OPS CKS NORMAL.
- [SDR DL72S981273](https://openairdocs.org/sdr/DL72S981273.md): Battery Pack · discharged · Jun 17, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND L2 DOOR EMERGENCY LIGHT INOP. REPLACED M9027 CONTROLLER AND BATTERY PACK.
- [SDR DL72S980891](https://openairdocs.org/sdr/DL72S980891.md): Battery Pack · discharged · Apr 26, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > LEFT WING EMERGENCY LIGHT DID NOT ILLUMINATE ON TEST. REPLACED BATTERY PACK.
- [SDR DL72S980808](https://openairdocs.org/sdr/DL72S980808.md): Angle · corrosion · Apr 3, 1998 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING MV1 CHECK TASK C53-113-01, CORROSION FOUND ON SKIN SUPPORT ANGLE AT STA 740 STR 27R. REPLACED SUPPORT ANGLE PER M/M 53-11-0 PG 858.
- [SDR DL72S980755](https://openairdocs.org/sdr/DL72S980755.md): Bear Strap · cracked · Apr 2, 1998 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER THE DIRECTION OF BAC S/B 727-53-0136 AND ER/A 364433-14.
- [SDR DL72S980796](https://openairdocs.org/sdr/DL72S980796.md): Skin · cracked · Apr 1, 1998 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF FWD SVC DOOR UPPER HINGE CUTOUT REF SI 4-72762-12 ME 02,.25 INCH VISIBLE CRACK FOUND IN BEAR STRAP. REPAIRED PER ER/A 364433-14 CODE 4-53-31-20.
- [SDR DL72S980809](https://openairdocs.org/sdr/DL72S980809.md): Blkhd Angle · cracked · Mar 27, 1998 · N494DA · Boeing 727232 · Fuselage Main, Bulkhead
  > DURING MV1 CHECK, FOUND KEEL BEAM SUPPORT ANGLE CRACKED 3.5 INCHES, FWD SIDE OF STA 870 BULKHEAD, RT SIDE OF KEEL BEAM. REPLACED ANGLE PER SRM 53-10-9 FIG 13.
- [SDR DL72S980829](https://openairdocs.org/sdr/DL72S980829.md): Frame · cracked · Mar 26, 1998 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > .75 INCH CRACK BEYOND STOP DRILL AT MAIN ENTRY DOOR UPPER DOOR UPPER FRAME, AFT END PREVIOUS REPAIR. REMOVED UPPER LINER AND GATE. REMOVED UPPER FRAME. DRILLED REPLACEMENT FRAME. BEGAN INSTALLING FRAME. INST FRAME CLOSED UPPER LINER. PER M/M 52-11-01.
- [SDR DL72S980700](https://openairdocs.org/sdr/DL72S980700.md): Floorbeam · corrosion · Mar 26, 1998 · N494DA · Boeing 727232 · Fuselage Main, Floor Beam
  > ON UPPER SURFACE OF FLOORBEAM STA 344 FROM LT O/B SEAT TRACK TO DOOR SILL FOUND CORROSION. INSTALLED NEW FLOORBEAM PER SRM 53-10-8 FIG 11.
- [SDR DL72S980817](https://openairdocs.org/sdr/DL72S980817.md): Skin · cracked · Mar 23, 1998 · N494DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > .5 INCH CRACK IN FUSELAGE SKIN AT LOWER INBD CORNER L-4 WINDSHIELD, FROM ATTACH SCREW TO CUTOUT-MARKED. REPAIRED PER SRM 53-30-3 AND ER/A 364469-14.
- [SDR DL72S980564](https://openairdocs.org/sdr/DL72S980564.md): Light · inoperative · Mar 12, 1998 · N494DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING INOP IN AFT SECTION OF CABIN.
- [SDR DL72S972332](https://openairdocs.org/sdr/DL72S972332.md): Battery Pack · discharged · Nov 11, 1997 · N494DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND EMER EXIT SIGN LIGHTS OUT ABOVE R-2 DOOR AND ABOVE CTR AISLE SAME STATION. REPLACED BATTERY FOR AISLE SIGN AND FUSE FOR R-2 DOOR SIGN.
- [SDR DL72S972175](https://openairdocs.org/sdr/DL72S972175.md): Plate · worn · Oct 27, 1997 · N494DA · Boeing 727232 · Service Doors
  > LEFT FWD SVC DOOR GUST LOCK BROKEN. REPLACED UPPER DOOR ARM GUIDE PLATE. DOOR AND GUST LOCK OPERATION NOW NORMAL.
- [SDR DL72S971809](https://openairdocs.org/sdr/DL72S971809.md): Battery Pack · discharged · Sep 16, 1997 · N494DA · Boeing 727232 · Emergency Lighting
  > LEFTHAND FORWARD OVERWING AND R-2 INTERIOR EMERG LIGHTS INOP. REPLACED BATTERY PACK.
- [SDR DL72S971755](https://openairdocs.org/sdr/DL72S971755.md): Battery · discharged · Sep 8, 1997 · N494DA · Boeing 727232 · Emergency Lighting
  > AISLE EMERGENCY LIGHTS INOP AT NR 2 DOOR. REPLACED BATTERY.
- [SDR DL72S971707](https://openairdocs.org/sdr/DL72S971707.md): Battery · discharged · Aug 30, 1997 · N494DA · Boeing 727232 · Emergency Lighting
  > REAR INBOARD EMERGENCY FLASHLIGHT LED INDICATION INOP. REPLACED BATTERY IN FLASHLIGHT AND LED INDICATION RETURNED TO NORMAL. REPLACED BULB AS PRECAUTIONARY.
- [SDR DL72S971599](https://openairdocs.org/sdr/DL72S971599.md): Web · cracked · Aug 15, 1997 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.75 INCH CRACK IN UPPER LT TORQUE BOX WEB AT UPPER CHORD STA 1223. INSTALLED DOUBLER PER M/M 53-11-0.
- [SDR DL72S971004](https://openairdocs.org/sdr/DL72S971004.md): Brakes · damaged · May 24, 1997 · N494DA · Boeing 727232 · Brake
  > NUMBER 3 BRAKE OVERHEATED AND CAUGHT FIRE AFTER LANDING. REPLACED BRAKE AND WHEEL ASSY NO DAMAGE TO LANDING GEAR OR ANY OTHER PART OF AIRCRAFT.
- [SDR DL72S962728](https://openairdocs.org/sdr/DL72S962728.md): Ballast · melted · Dec 18, 1996 · N494DA · Boeing 727232 · Flight Compartment Lighting
  > JUST AFTER LEVEL OFF AT FL230, NOTED SMOKE IN THE COCKPIT COMING FROM BEHIND S/O PANEL. SMOKE STOPPED AFTER 2 TO 3 MINUTES. AT THE GATE NOTICED PANEL FLOOR C/B POPPED. FOUND PANEL FLOOR BALLAST M354 MELTED AND CONTROL PANEL FLOOR C/B POPPED. REPLACED B
- [SDR DL72S961485](https://openairdocs.org/sdr/DL72S961485.md): Channel · cracked · Jun 18, 1996 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND A.875 INCH CRACK IN THE CHANNEL AT FS 1263. REPAIRED PER DELTA ER/A 303744-14AD.
- [SDR DL72S961451](https://openairdocs.org/sdr/DL72S961451.md): Web · cracked · Jun 17, 1996 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.5 INCH CRACK IN TORQUE BOX WEB EXTENDING FROM RT FWD LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.
- [SDR DL72S961450](https://openairdocs.org/sdr/DL72S961450.md): Angle · cracked · Jun 17, 1996 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 2 INCH AND 1.5 INCH CRACK IN TORQUE BOX WEB AT UPPER CHORD RT END. REPAIRED PER M/M 53-11-0.
- [SDR DL72S954410](https://openairdocs.org/sdr/DL72S954410.md): Angle · cracked · Nov 16, 1995 · N494DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING A-1 LETTER CHECK, 4 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.
- [SDR DL72S953706](https://openairdocs.org/sdr/DL72S953706.md): Eel Battery · discharged · Sep 14, 1995 · N494DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS INOP AFT AISLE EXIT SIGN. REPLACED BATTERY, OPERATION NORMAL.
- [SDR DL72S953256](https://openairdocs.org/sdr/DL72S953256.md): Eel Connector · loose · Jul 31, 1995 · N494DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE DURING MTC CHECK. RELAMPED, NO HELP. RESEATED CANNON PLUG, OPERATION NORMAL.
- [SDR DL72S951871](https://openairdocs.org/sdr/DL72S951871.md): Web · cracked · May 1, 1995 · N494DA · Boeing 727232 · Fuselage Main, Bulkhead
  > DURING HMV, FOUND STA 870 WEB CRACKED AT APU BLEED VALVE CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S951873](https://openairdocs.org/sdr/DL72S951873.md): Stringer · cracked · Apr 22, 1995 · N494DA · Boeing 727232 · Vertical Stabilizer
  > DURING HMV, FOUND STRINGER 1 LEFT CRACKED AT RIB 3A INSIDE VERT STAB. REPAIRED PER M/M 53-30-0 PG 803.
- [SDR DL72S951762](https://openairdocs.org/sdr/DL72S951762.md): Stringer · cracked · Apr 22, 1995 · N494DA · Boeing 727232 · Vertical Stabilizer
  > DURING HMV, FOUND STRINGER CRACKED AT STR 3 LEFT RIB NR 4 INSIDE VERTICAL STAB. REPAIRED PER M/M 55-30-0 PG 803.
- [SDR DL72S951696](https://openairdocs.org/sdr/DL72S951696.md): Channel · corroded · Apr 21, 1995 · N494DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > AT HMV, FOUND J-CHANNEL CORRODED BEHIND T-CHORD AT HINGES FOR DOOR 3348. INSTALLED NEW DOUBLER AND NEW ANGLE PER SRM 51-40-3.
- [SDR DL72S951622](https://openairdocs.org/sdr/DL72S951622.md): Fitting · corrosion · Apr 20, 1995 · N494DA · Boeing 727232 · Trailing Edge Flaps
  > O/B CARRIAGE FITTING FOR ALL FOUR THRUST BEARING RETAINER BOLT HOLES HAVE CORROSION, NR 2 MID FLAP. FOUND AT SHOP INSPECTION, REAMED HOLES TO.312 TEATED AND INSTALLED BUSHING.
- [SDR DL72S951756](https://openairdocs.org/sdr/DL72S951756.md): Frame · cracked · Apr 18, 1995 · N494DA · Boeing 727232 · Fuselage Main, Frame
  > THE BS 970 FRAME IS CRACKED JUST O/B OF STR 27L. THE CRACK RUNS FROM THE AFT FREE FLANGE, ACROSS THE UPPER FLANGE AND DOWN TO A FASTENER HOLE COMMON TO THE FAILSAFE CHORD. DAMAGE FOUND AT HMV, AND REPAIRED PER DL ERA 301580-14AD.
- [SDR DL72S952106](https://openairdocs.org/sdr/DL72S952106.md): Doublers · cracked · Apr 17, 1995 · N494DA · Boeing 727232 · Trailing Edge Flaps
  > AFT LOWER CHORD HAS TWO CRACKED DOUBLERS 23 AND 32 FROM IB END OF NR 3 MID-FLAP PANEL. SPLICED IN NEW SECTION OF AFT CHORD PER MM 57-52-0. FOUND AT HMV, SHOP VISIT.
- [SDR DL72S951870](https://openairdocs.org/sdr/DL72S951870.md): Stringer · corroded · Apr 16, 1995 · N494DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING HMV, STR 25L CORRODED STA 1148. REPAIRED PER SRM 53-10-3.

Next page: https://openairdocs.org/deregistered/N494DA-2000-06-22/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 = 'N494DA' AND deregistration_id = 'N494DA-2000-06-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N494DA-2000-06-22/reports

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