# Service difficulty reports: N485DA, cancelled Feb 14, 2000

A list on [N485DA, cancelled Feb 14, 2000](https://openairdocs.org/deregistered/N485DA-2000-02-14.md).

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

- [SDR DL72S991979](https://openairdocs.org/sdr/DL72S991979.md): Pack Battery · discharged · Sep 6, 1999 · N485DA · Boeing 727232 · Emergency Lighting
  > FOUND MID LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CKS GOOD.
- [SDR DL72S991758](https://openairdocs.org/sdr/DL72S991758.md): Battery · discharged · Aug 6, 1999 · N485DA · Boeing 727232 · Emergency Lighting
  > LT MID OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT RACK M654. OPS CHKS GOO.
- [SDR DL72S991693](https://openairdocs.org/sdr/DL72S991693.md): Engine · failed · Jul 28, 1999 · N485DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 2 ENG OIL PRESS SLOWLY DECREASED TO ZERO WITH ASSOCIATED LOW OIL PRESS LIGHT ON. GOOD QTY AND TEMP. REPLACED ENGINE.
- [SDR DL72S991559](https://openairdocs.org/sdr/DL72S991559.md): Engine · malfunctioned · Jul 11, 1999 · N485DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > DURING THE ROTATION AND INITIAL CLIMBOUT OF THE TAKEOFF FROM FLL, (OAT 32 DEG CELSIUS USING NORMAL PWR/EPR 2.06). ENG NR 3 EGT EXCEEDED THE TAKEOFF LIMIT. A MAXIMUM TEMP OF 640 DEG CELSIUS ON ENG 3 EGT WAS REACHED FOR A PERIOD OF UP TO 1 MINUTE. THRUST WAS
- [SDR DL72S982298](https://openairdocs.org/sdr/DL72S982298.md): Battery · discharged · Nov 8, 1998 · N485DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS L2 DOOR DID NOT TEST ON LAYOVER. REPLACED BATTERIES, NOW TESTS NORMAL.
- [SDR DL72S982032](https://openairdocs.org/sdr/DL72S982032.md): Skin · misdrilled · Oct 2, 1998 · N485DA · Boeing 727232 · Elevator, Plate/Skin
  > RT ELEVATOR, REAR SPAR MOD, OS HOLES: AD 96-06-05. DURING REAR SPAR MOD PER EO 4-70183-3AD, SEVERAL HOLES IN THE UPPER SKIN WERE OVERSIZED. REPAIR BONDED AN INTERNAL DOUBLER AND INSTALL OVERSIZED FASTENERS.
- [SDR DL72S981553](https://openairdocs.org/sdr/DL72S981553.md): Bulb · failed · Jul 9, 1998 · N485DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOP OVERWING EXIT. REPLACED LIGHT BULBS.
- [SDR DL72S981376](https://openairdocs.org/sdr/DL72S981376.md): Skin · delaminated · Jun 30, 1998 · N485DA · Boeing 727232 · Elevator, Plate/Skin
  > T/E OF RT ELEVATOR WAS DELAMINATING. INSTALLED ADDITIONAL TACK RIVETS BETWEEN FACTORY RIVETS AS PER M/M 55-20-0.
- [SDR DL72S980088](https://openairdocs.org/sdr/DL72S980088.md): Skin · cracked · Jan 12, 1998 · N485DA · Boeing 727232 · Rudder, Plate/Skin
  > THE UPPER RUDDER WAS FOUND WITH MULTIPLE CRACKS ON THE RT SKIN PANEL BETWEEN RS 220 AND 242. THE PANEL WAS ORIGINALLY A BONDED ALUMINUM ASSEMBLY WITH BEADED STIFFENERS, BUT HAD BEEN PREVIOUSLY REPLACED WITH A REPAIR PANEL OF DIFFERENT CONSTRUCTION. THE PANEL
- [SDR DL72S980034](https://openairdocs.org/sdr/DL72S980034.md): Skin · cracked · Jan 6, 1998 · N485DA · Boeing 727232 · Engine Cowling System
  > .5 INCH CRACK EXTENDING FROM NR 2 ENG DUCT HOUSING ACCESS PANEL 9524R. REPAIRED PER MM 54-30-0 P 803.
- [SDR DL72S971740](https://openairdocs.org/sdr/DL72S971740.md): Switch · failed · Sep 6, 1997 · N485DA · Boeing 727232 · Landing Gear Position and Warning
  > DURING ROTATION JUST AFTER V1 THE NOSE GEAR INDICATED UNSAFE AFTER WEIGHT CAME OFF HTE WHEEL THE INDICATION TURNED TO SAFE. REPLACED NOSE SWITCHES S93 AND S96 AND PERF NOSE GEAR SWING. GEAR AND INDICATION OPERATION NORMAL.
- [SDR DL72S971464](https://openairdocs.org/sdr/DL72S971464.md): Controller · failed · Jul 26, 1997 · N485DA · Boeing 727232 · Cabin Pressure Controller
  > SMOKE IN THE CABIN WITH SMOKE DETECTORS GOING OFF. EMERGENCY RETURN INITIATED. SMOKE IN THE CABIN WITH TWO PACKS OPERATING. COMPRESSOR DISCHARGE TEMP LESS THAN 150 DEGREES, FLAPS UP AND LANDING GEAR DOWN. MAINTENANCE REPLACED 35 DEG CONTROLLER AND ACCOMPLI
- [SDR DL72S971109](https://openairdocs.org/sdr/DL72S971109.md): Floorbeam · corrosion · Jun 3, 1997 · N485DA · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT STA 344 AND RBL 1. REPLACED SECTION OF BEAM PER SRM 53-10-8 FIG 11.
- [SDR DL72S970278](https://openairdocs.org/sdr/DL72S970278.md): Valve · cracked · Feb 13, 1997 · N485DA · Boeing 727232 · Landing Gear Retraction/Extension System
  > DURING CLIMBOUT, LOST ALL A-SYS HYDRAULIC QTY. FOUND RT MLG LOCK OPERATED SEQUENCE VALVE CASE SPLIT. REPLACED VALVE ASSY AND A-SYS HYDRAULIC FILTERS.
- [SDR DL72S962452](https://openairdocs.org/sdr/DL72S962452.md): Skin · cracked · Nov 5, 1996 · N485DA · Boeing 727232 · Service Doors
  > FOUND A.25 INCH CRACK ON THE EXTERNAL SKIN AT R-1 DOOR LWR FWD CORNER. REPAIRED PER M/M 52-12-0, PAR. 10.
- [SDR DL72S962276](https://openairdocs.org/sdr/DL72S962276.md): Window · smoking · Oct 9, 1996 · N485DA · Boeing 727232 · Flight Compartment Windows
  > WHITE SMOKE EMITTED FROM UPPER RIGHT CORNER OF R-1 WINDOW WHILE CLIMBING THROUGH 27,000 FT. NO OVERHEAT LIGHT, WINDOW WAS HOTTER TO TOUCH THAN R-2, L-1, L-2. SECURED R-1 HEAT, FOUND OUTBD WINDOW HEAT CONTACT TOUCHING WINDOW FRAME. RETERMINATED WIRE AND DRES
- [SDR DL72S960899](https://openairdocs.org/sdr/DL72S960899.md): Skin · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Rudder, Plate/Skin
  > FOUND ON B1 LETTER CHECK, UPPER RUDDER OUTER SKIN CRACKED 3 INCH RT SIDE, 1 FT FROM TOP CENTER. INSTALLED DOUBLER PER SRM 55-40-2 FIG 1.
- [SDR DL72S960886](https://openairdocs.org/sdr/DL72S960886.md): Stiffener · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON B-1 LETTER CHECK, VERT SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK O/B SIDE. REPLACED PER M/M 57-20-21.
- [SDR DL72S960885](https://openairdocs.org/sdr/DL72S960885.md): Act Mount Box · cracked angle · Apr 16, 1996 · N485DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON B-1 LETTER CHECK, NR 5 L/E FLAP ACT MOUNT BOX I/B LWR ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PG 811.
- [SDR DL72S960884](https://openairdocs.org/sdr/DL72S960884.md): Stiffener · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT SPAR STIFFENER AT NR 7 O/B SLAT TRACK O/B ANGLE. REPLACED STIFFENER PER M/M 57-20-21 PG 813.
- [SDR DL72S960883](https://openairdocs.org/sdr/DL72S960883.md): Act Attach Box · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON B-1 LETTER CHECK, 1 INCH CRACK NR 2 L/E FLAP ACT ATTACH BOX O/B SIDE. REPAIRED PER M/M 57-20-21.
- [SDR DL72S960882](https://openairdocs.org/sdr/DL72S960882.md): Skin · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Nacelle/Pylon Structure
  > FOUND ON B-1 LETTER CHECK, THREE.5 INCH CRACKS EXTENDING FROM FASTENERS FWD OF PANEL 9501 RT SIDE AND TWO.5 INCH CRACKS EXTENDING FROM FASTENERS BELOW PANEL 9501 RT SIDE. REPAIRED PER M/M 54-30-0 PG 801 AND 802.
- [SDR DL72S960880](https://openairdocs.org/sdr/DL72S960880.md): Skin · cracked · Apr 16, 1996 · N485DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT WEB OF TORQUE BOX TOP ROW OF RIVETS LT SIDE AT STA 1233. REPAIRED PER M/M 53-11-0 PG 832.
- [SDR DL72S960243](https://openairdocs.org/sdr/DL72S960243.md): Light · inoperative · Jan 31, 1996 · N485DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT R1 AND R2 DOOR INOP. REPLACED EMERGENCY LIGHTS OVER R1 AND R2 DOORS AND OPERATION NORMAL.
- [SDR DL72S960221](https://openairdocs.org/sdr/DL72S960221.md): Light · inoperative · Jan 29, 1996 · N485DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS OVER DOOR INOP AT R1 AND R2. REPLACED LIGHT ASSYS.
- [SDR DL72S953674](https://openairdocs.org/sdr/DL72S953674.md): Angle · cracked · Sep 11, 1995 · N485DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A2 LETTER CHECK, NUMBER 2 SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT INBD STOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72S953673](https://openairdocs.org/sdr/DL72S953673.md): Angle · cracked · Sep 11, 1995 · N485DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT OUTBD STOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72S951113](https://openairdocs.org/sdr/DL72S951113.md): Transverse Beam · cracked · Mar 4, 1995 · N485DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING LETTER CHECK INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED. PER THE B727 S/B 53-0129, REV 4, THE PART WILL BE REPLACED.
- [SDR DL72S950795](https://openairdocs.org/sdr/DL72S950795.md): Skin · dented · Feb 22, 1995 · N485DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION, FOUND NR 6 SLAT WITH CRACKED L-ANGLE UNDER UP-STOP. REPAIRED PER MM 57-54-0.

## 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 = 'N485DA' AND deregistration_id = 'N485DA-2000-02-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N485DA-2000-02-14/reports

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