# Service difficulty reports: N476DA, cancelled Nov 23, 1999

A list on [N476DA, cancelled Nov 23, 1999](https://openairdocs.org/deregistered/N476DA-1999-11-23.md).

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

- [SDR DL72S991291](https://openairdocs.org/sdr/DL72S991291.md): Track · corroded · Jun 5, 1999 · N476DA · Boeing 727232 · Trailing Edge Flaps
  > AN I/B FLAP TRACK WAS FOUND WITH CORROSION IN TWO BOLT HOLES WHICH ARE THE SUBJECT OF AD 90-07-05. THE CORROSION WAS CLEANED UP BY OVERSIZING THE HOLES WITHIN THE LIMITS OF B727, S/B 57-0178, REV 5 AND DOCUMENTED PER ER/A 367543-14AD.
- [SDR DL72S991083](https://openairdocs.org/sdr/DL72S991083.md): Battery · discharged · May 16, 1999 · N476DA · Boeing 727232 · Emergency Lighting
  > AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP.
- [SDR DL72S990137](https://openairdocs.org/sdr/DL72S990137.md): Frame · cracked · Jan 21, 1999 · N476DA · Boeing 727232 · Service Doors
  > FOUND AT A-1 LETTER CHECK,.5 INCH VISIBLE CRACK ON AFT FRAME OF R-1 DOOR AT FWD SIDE OF LWR STOP CASTING. REPAIRED PER MM 52-12-0.
- [SDR DL72S990136](https://openairdocs.org/sdr/DL72S990136.md): Frame · cracked · Jan 21, 1999 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT A-1 LETTER CHECK,.5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.
- [SDR DL72S982136](https://openairdocs.org/sdr/DL72S982136.md): Skin · damaged · Oct 13, 1998 · N476DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT STRINGER 22L BETWEEN FS 1110 AND 1166 WAS TORN AND GOUGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGE WAS REMOVED FROM THE SKIN WITH TWO CUTOUTS MEASURING 4 X 28.25 AND 3.25 X 16.5. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL A
- [SDR DL72S981306](https://openairdocs.org/sdr/DL72S981306.md): Skin · cracked · Jun 19, 1998 · N476DA · Boeing 727232 · Elevator, Plate/Skin
  > LT ELEVATOR CRACKED ADJACENT PREVIOUS REPAIR LOWER SIDE AFT OF NR 3 BALANCE BOARD PANEL SRM 55-20-3.
- [SDR DL72S980135](https://openairdocs.org/sdr/DL72S980135.md): Battery Pack · discharged · Jan 17, 1998 · N476DA · Boeing 727232 · Emergency Lighting
  > AFT LT EXT EMERG LIGHT INOP. REPLACED BATTERY PACK M955, CHKS GOOD.
- [SDR DL72S972643](https://openairdocs.org/sdr/DL72S972643.md): Doubler · cracked · Dec 12, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FUSELAGE, FWD GALLEY DOOR SURROUND DOUBLER, UPPER HINGE: REPAIR FOR CRACK AT HINGE CUTOUT. THE FWD GALLEY DOOR SURROUND DOUBLER WAS FOUND WITH A 1.8 CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR INSTALLED PER BOEING S/B 727
- [SDR DL72S972360](https://openairdocs.org/sdr/DL72S972360.md): Frame · cracked · Nov 13, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 1.5 INCH CRACK IN UPPER AFT RADIUS OF R-1 DOOR AFT FRAME. REPAIRED PER ERA 363204-14 AND M/M 52-12-0.
- [SDR DL72S972358](https://openairdocs.org/sdr/DL72S972358.md): Bracket · cracked · Nov 13, 1997 · N476DA · Boeing 727232 · Drag Control Actuator
  > FOUND DURING F-1 LETTER CHECK, 2 INCH CRACK NR 8 SPOILER ACTUATOR MOUNT CASTING LWR ATTACH BRACKET. REPAIRED PER M/M 57-20-22.
- [SDR DL72S972099](https://openairdocs.org/sdr/DL72S972099.md): Fitting · worn · Oct 19, 1997 · N476DA · Boeing 727232 · Landing Gear Doors
  > RT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807, IPC REF 65-26763-10 ITEM 350.
- [SDR DL72S972098](https://openairdocs.org/sdr/DL72S972098.md): Fitting · worn · Oct 19, 1997 · N476DA · Boeing 727232 · Landing Gear Doors
  > LT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807 IPC LOC 32-10-00-10 ITEM 345.
- [SDR DL72S971716](https://openairdocs.org/sdr/DL72S971716.md): Light · inoperative · Aug 29, 1997 · N476DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOP. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSY AND BATTERY.
- [SDR DL72S971395](https://openairdocs.org/sdr/DL72S971395.md): Stop Pad · cracked · Jul 3, 1997 · N476DA · Boeing 727232 · Leading Edge Devices
  > DOUBLER CRACKED AT LWR COVER SKIN ANGLE AT NR 7 SLAT I/B STOP PAD. REPAIRED PER DELTA ER/A 362251-14.
- [SDR DL72S971394](https://openairdocs.org/sdr/DL72S971394.md): Vert Web · cracked · Jul 3, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 EA CRACKS ONE AT LWR RT CORNER AND ONE AT LWR LT CORNER. INSTALLED REPAIR PER SRM 53-10-4.
- [SDR DL72S971311](https://openairdocs.org/sdr/DL72S971311.md): Skin · cracked · Jul 3, 1997 · N476DA · Boeing 727232 · Leading Edge Devices
  > A.25 INCH VISIBLE CRACK AT NR 2 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72S971310](https://openairdocs.org/sdr/DL72S971310.md): Web · cracked · Jul 3, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LT VERT TORQUE BOX WEB CRACKED AT LIGHTENING HOLE STA 1230. REPAIRED PER MM 53-11-0.
- [SDR DL72S971374](https://openairdocs.org/sdr/DL72S971374.md): Torque Box · cracked · Jul 2, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TORQUE BOX CHORD CRACKED STA 1273R. CRACK HORIZ TORQUE BOX ANGLE STA 1273. REPAIRED PER SRM 53-10-10.
- [SDR DL72S971354](https://openairdocs.org/sdr/DL72S971354.md): Torque Box · cracked · Jul 2, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.75 INCH CRACK IN UPPER LT TORQUE BOX WEB STA 1215 CRACKED AT CHORD ATTACH POINT, MARKED. STOP DRILLED CRACKS, DRILLED REPAIR DOUBLER PER M/M 53-11-0, INSTALLED REPAIR.
- [SDR DL72S971280](https://openairdocs.org/sdr/DL72S971280.md): Floorbeam · corroded · Jul 1, 1997 · N476DA · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOORBEAM STA 344 AND RBL 2. INSTALLED REPAIR PER SRM 53-10-8 FIG 11.
- [SDR DL72S970770](https://openairdocs.org/sdr/DL72S970770.md): Skin · cracked · Apr 25, 1997 · N476DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > A 1 INCH CRACK ACROSS RIVET HOLE AT RT SIDE OF VERT STAB BELOW ACCESS PANEL APPROX 10 FT AFT OF L/E. REPAIRED PER SRM 54-30-0.
- [SDR DL72S970769](https://openairdocs.org/sdr/DL72S970769.md): Skin · cracked · Apr 25, 1997 · N476DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND 1 INCH CRACK FUSELAGE SKIN COMING FROM R-5 COCKPIT WINDOW CUTOUT UPPER AFT CORNER. REPAIRED PER SRM 53-30-3.
- [SDR DL72S970768](https://openairdocs.org/sdr/DL72S970768.md): Web · cracked · Apr 25, 1997 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.375 AND.3125 INCH CRACK RT TORQUE BOX VERT WEB LIGHTENING HOLE AT STA 1235. REPAIRED PER MM 53-11-0.
- [SDR DL72S970767](https://openairdocs.org/sdr/DL72S970767.md): Skin · cracked · Apr 25, 1997 · N476DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > FOUND 3 CRACKS EXTENDING FROM RIVET HOLE AT BASE OF VERTICAL STABILIZER LT SIDE APPROX 10 FT AFT OF L/E. REPAIR PER MM 54-30-0.
- [SDR DL72S970243](https://openairdocs.org/sdr/DL72S970243.md): Air Distribution · smoke · Feb 7, 1997 · N476DA · Boeing 727232 · Air Distribution System
  > IN CRUISE, FLT ATT REPORTED SMOKE IN MID CABIN AREA WITH ELECTRICAL SMELL. UNABLE TO DUPLICATE PROBLEM OR FIND ANY DESCREPENCIES THAT MAY HAVE CAUSED PROBLEM.
- [SDR DL72S962213](https://openairdocs.org/sdr/DL72S962213.md): Light · inoperative · Oct 2, 1996 · N476DA · Boeing 727232 · Emergency Lighting
  > ESCAPE PATH LIGHTING LENS CRACKED AND LIGHT INOP. REPLACED LENS AND LIGHT, OPS CHECK NORMAL.
- [SDR DL72S961755](https://openairdocs.org/sdr/DL72S961755.md): Light · inoperative · Jul 22, 1996 · N476DA · Boeing 727232 · Emergency Lighting
  > LT AFT SERVICE DOOR OVERHEAD EMERGNECY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES, CHECKS NORMAL.
- [SDR DL72S960998](https://openairdocs.org/sdr/DL72S960998.md): Wheel Bearing · failed · Apr 25, 1996 · N476DA · Boeing 727232 · Wheel/Ski/Float
  > ON TAXI IN TO GATE, NR 1 MAIN WHEEL ASSY LOCKED UP. FOUND NR 1 WHEEL ASSY DAMAGED. INBOARD WHEEL BEARING DESTROYED, AXLE CRACKED AND BROKEN AT INBOARD BEARING RACE. FOUND BRAKE ATTACH BOLT FROM ELEVEN O`CLOCK POSTION LAYING BETWEEN AXLE AND WHEEL ASSY. REP
- [SDR DL72S960461](https://openairdocs.org/sdr/DL72S960461.md): Skin · cracked · Feb 28, 1996 · N476DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A.25 INCH CRACK IN THE UPPER FORWARD CORNER OF THE L-1 DOOR CUTOUT. A TIME LIMITED REPAIR HAS BEEN INSTALLED AND A PERMANENT REPAIR WILL BE INSTALLED PER SB 727-53-0186, REV 1.
- [SDR DL72S961607](https://openairdocs.org/sdr/DL72S961607.md): Web · cracked · Feb 27, 1996 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 2.5 INCH CRACK BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE WEB AT THIS LOCATION IS 0.040 CLAD 2024-T3. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND TWO STRAPS WILL B
- [SDR DL72S960437](https://openairdocs.org/sdr/DL72S960437.md): Web · cracked · Feb 26, 1996 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TWO LIGHTENING HOLES IN RT VERT WEB OF AFT AIR STAIR TORQUE BOX WERE FOUND WITH CRACKS ROUTED PAST LIMITS. FOUND AT D-2 LTR CHECK AND REPAIRED PER MM 53-11-0.
- [SDR DL72S954104](https://openairdocs.org/sdr/DL72S954104.md): Battery · discharged · Oct 25, 1995 · N476DA · Boeing 727232 · Emergency Lighting
  > L-2 PORTABLE EMERGENCY LIGHT INOP, REPLACED BATTERIES, OPERATION NORMAL.
- [SDR DL72S953292](https://openairdocs.org/sdr/DL72S953292.md): Light Ballast · failed · Aug 5, 1995 · N476DA · Boeing 727232 · Passenger Compartment Lighting
  > AFTER STOPPING AT GATE AND DEPLANING, SMOKE STARTED COMING OUT OF OVERHEAD PANEL ABOVE 21A. PULLED ALL CABIN LIGHTING C/BS. FOUND CEILING LIGHT BALLAST BETWEEN 21 AND 22 ABC BURNT UP. DISCONNECTED SAME FWD TOMCO AND PLACED PER MEL 33-00-02. BALLAST WAS SUB
- [SDR DL72S951523](https://openairdocs.org/sdr/DL72S951523.md): Clip · corrosion · Apr 12, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING CV-2 CHECK, CORROSION FWD OF FORMER 950F WHERE IT ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 FIG 825.
- [SDR DL72S951522](https://openairdocs.org/sdr/DL72S951522.md): Clip · corrosion · Apr 12, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING CV-2 CHECK, CORROSION WHERE FORMER 970 ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 PG 825.
- [SDR DL72S951521](https://openairdocs.org/sdr/DL72S951521.md): Stringer · corrosion · Apr 12, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING CV-2 CHECK, CORROSION AROUND RIVETS IN STRINGER 25L BETWEEN STA 950D AND 950E. REPAIRED PER MM 53-11-0.
- [SDR DL72S951578](https://openairdocs.org/sdr/DL72S951578.md): Sidewall · cracked · Apr 6, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1 INCH CRACK BET STA 294.5 AND 285.5 APPROX AT WL 170. THE WEB AT THIS LOCATION IS 0.040 INCH THK 2024-T3 CLAD. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND STRAP WILL BE INSTALL
- [SDR DL72S951449](https://openairdocs.org/sdr/DL72S951449.md): Web · cracked · Apr 3, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CHECK.25 INCH CRACK LIGHTNING HOLE TORQUE BOX SIDE WEBB STA 1263 LT SIDE. REPAIR: ROUTE OUT DAMAGED AREA PER M/M 53-11-0.
- [SDR DL72S951444](https://openairdocs.org/sdr/DL72S951444.md): Skin · corroded · Apr 3, 1995 · N476DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON CV2 CHECK, CORROSION ON SKIN BETWEEN STA 480 AND 500 AT BL 0. REPAIRED PER SRM 53-30-3 FIG 1.
- [SDR DL72S951495](https://openairdocs.org/sdr/DL72S951495.md): Stringer · corroded · Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STRINGER 25L FROM 950A TO 950B. REPAIRED PER SRM 53-10-3 AND PER PS 900-5-1.
- [SDR DL72S951451](https://openairdocs.org/sdr/DL72S951451.md): Clip · cracked · Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CHECK, ONE INCH CRACK IN SKIN CLIP BETWEEN STR 28L AND 29L FWD SIDE STA 990. REPAIR: REPAIRED PER M/M 53-11-0.
- [SDR DL72S951445](https://openairdocs.org/sdr/DL72S951445.md): Stringer · corroded · Apr 2, 1995 · N476DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STR 27L STA 1030 TO STA 1050. REPAIRED PER ERA 301506-14 CODE 4-53-14.
- [SDR DL72S951441](https://openairdocs.org/sdr/DL72S951441.md): Seat Track · corroded · Apr 1, 1995 · N476DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CHECK, CORROSION AT O/B GALLEY ATTACH TRACK LBL 56 BETWEEN STA 1070 AND STA 1115. REPLACED SEAT TRACK FROM STA 1070 TO STA 1110 PER SRM 53-10-5 FIG 7.
- [SDR DL72S951450](https://openairdocs.org/sdr/DL72S951450.md): Angle · cracked · Mar 31, 1995 · N476DA · Boeing 727232 · Spoilers
  > FOUND ON CV2 CHECK, ONE INCH CRACK IN ATTACH ANGLE LOWER END OF NR 7 SPOILER ACTUATOR ATTACH FITTING. REPAIR: REPAIRED PER M/M 57-20-22 PAR 10.
- [SDR DL72S951447](https://openairdocs.org/sdr/DL72S951447.md): Skin · cracked · Mar 31, 1995 · N476DA · Boeing 727232 · Service Doors
  > FOUND ON CV2 CHECK RT FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED.50 INCH. REPAIR: REPAIRED PER M/M 52-11-0 PG 808.
- [SDR DL72S951446](https://openairdocs.org/sdr/DL72S951446.md): Angle · cracked · Mar 31, 1995 · N476DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON CV2 NR 8 SLAT ANGLE CRACKED UNDER TELESCOPING TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.
- [SDR DL72S951443](https://openairdocs.org/sdr/DL72S951443.md): Seat Track · corroded · Mar 31, 1995 · N476DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CHECK, CORROSION ON RT INBD SEAT TRACK STA 380 TO 480. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.
- [SDR DL72S951442](https://openairdocs.org/sdr/DL72S951442.md): Seat Track · corroded · Mar 31, 1995 · N476DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CHECK, CORROSION ON RT CENTER SEAT TRACK STA 344 TO 480. CLEANED TREATED AND PAINTED FROM STA 460 TO 480 PER SRM 53-10-1, FROM STA 344 TO 460 REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.
- [SDR DL72S950371](https://openairdocs.org/sdr/DL72S950371.md): Web · corrosion · Jan 26, 1995 · N476DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE SKIN CLIP AND WEB JUST O/B OF THE LT NOSE CHORD AT STA 303.9. THE DAMAGE WAS REPAIRED PER MM 53-30-0 FIG 806. DAMAGE FOUND DURING SPECIAL INSPECTION.

## 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 = 'N476DA' AND deregistration_id = 'N476DA-1999-11-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N476DA-1999-11-23/reports

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