# Service difficulty reports: N2821W, cancelled Aug 27, 2012

A list on [N2821W, cancelled Aug 27, 2012](https://openairdocs.org/deregistered/N2821W-2012-08-27.md).

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

- [SDR DL72W010107](https://openairdocs.org/sdr/DL72W010107.md): Windshield · cracked · Jan 21, 2001 · N2821W · Boeing 727247 · Flight Compartment Windows
  > R-1 OUTER WINDOW PANE IS CRACKED. REPLACED R-1 WINDOW PER M/M.
- [SDR DL72W002227](https://openairdocs.org/sdr/DL72W002227.md): Web · cracked · Nov 14, 2000 · N2821W · Boeing 727247 · Leading Edge Devices
  > NR 2 SLAT ACT O/B MOUNT WEB BROKEN. REPAIR PER MM 57-42-0.
- [SDR DL72W002174](https://openairdocs.org/sdr/DL72W002174.md): Engine · failed · Nov 6, 2000 · N2821W · Boeing 727247 · Turbine Engine Accessory Drive
  > ENG SHUT DOWN IN FLT AFTER OIL CLOG LIGHT AND OIL TEMP RISE OF 130 DEG. FOUND METAL IN GEARBOX CHIP DET AND MAIN OIL FILTER. REPLACED NR 1 ENG.
- [SDR DL72W001305](https://openairdocs.org/sdr/DL72W001305.md): Engine · failed · Jul 10, 2000 · N2821W · Boeing 727247 · Engine (Turbine/Turboprop)
  > ON CLIMB, NR 3 ENG HAD VIBRATION, LOUD BANG, AND LOSS OF THRUST. NO FIRE WARNING. REPLACED NR 3 ENGINE.
- [SDR DL72W001299](https://openairdocs.org/sdr/DL72W001299.md): Switch · failed · Jul 9, 2000 · N2821W · Boeing 727247 · Cabin Cooling System
  > AUTO PACK TRIP LIGHT FAILED TO ILLUMINATE ON TAKEOFF. RETURN TO GATE. REPLACED AUTO PACK TRIP SWITCHES.
- [SDR DL72W001199](https://openairdocs.org/sdr/DL72W001199.md): Skin · cracked · Jun 22, 2000 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT FS 303 BELOW THE FWD LAVATORY SERVICE DOOR CUTOUT (BETWEEN STRINGERS 21R_& 22R) WAS FOUND WITH A 1INCH CRACK DUE TO CORROSION. THE CORRODED AREA OF SKIN WAS REMOVED WITH A 4.5 INCH X 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTE
- [SDR DL72W000696](https://openairdocs.org/sdr/DL72W000696.md): Angle · cracked · Apr 11, 2000 · N2821W · Boeing 727247 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED IN RADIUS ABOVE UPPER RADIUS BLOCK ON FWD ANGLE AT FS 910 O/B OF H BRACKET. REPAIRED PER MM 53-11-0.
- [SDR DL72W000695](https://openairdocs.org/sdr/DL72W000695.md): Angle · cracked · Apr 11, 2000 · N2821W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 8 SLAT I/B ACT ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72W992561](https://openairdocs.org/sdr/DL72W992561.md): Battery · discharged · Nov 21, 1999 · N2821W · Boeing 727247 · Emergency Lighting
  > ROW 28 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES.
- [SDR DL72W992560](https://openairdocs.org/sdr/DL72W992560.md): Battery · discharged · Nov 21, 1999 · N2821W · Boeing 727247 · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES.
- [SDR DL72W992559](https://openairdocs.org/sdr/DL72W992559.md): Battery Pack · discharged · Nov 21, 1999 · N2821W · Boeing 727247 · Emergency Lighting
  > AFT CABIN DOOR EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72W991958](https://openairdocs.org/sdr/DL72W991958.md): Skin · cracked · Sep 3, 1999 · N2821W · Boeing 727247 · Elevator, Plate/Skin
  > RT ELEVATOR LOWER SKIN CRACKED. REPAIRED PER SRM 55-20-3.
- [SDR DL72W991957](https://openairdocs.org/sdr/DL72W991957.md): Bracket · cracked · Sep 3, 1999 · N2821W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 5 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED BELOW LOWER MOUNT BOLT. REPAIRED PER M/M 57-20-21 PAGE 811.
- [SDR DL72W991494](https://openairdocs.org/sdr/DL72W991494.md): Ballast · failed · Jul 2, 1999 · N2821W · Boeing 727247 · Passenger Compartment Lighting
  > AT DEPARTURE TIME, BURNING SMELL IN CABIN AND RT AFT CEILING LIGHT CIRCUIT BREAKER POPPED. FOUND CEILING BALLAST BAD AT SEAT 17. REPLACED SAME..
- [SDR DL72W990907](https://openairdocs.org/sdr/DL72W990907.md): Skin · cracked · Apr 25, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE CK REPAIR, LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUTOUT AN
- [SDR DL72W990906](https://openairdocs.org/sdr/DL72W990906.md): Skin · cracked · Apr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-681,STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG TH
- [SDR DL72W990901](https://openairdocs.org/sdr/DL72W990901.md): Skin · cracked · Apr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONF
- [SDR DL72W990607](https://openairdocs.org/sdr/DL72W990607.md): Skin · corroded · Mar 19, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FS 680 BUTT SPLICE BETWEEN STRINGER 28L AND 28R. AN EXISTING LOCAL REPAIR WAS REMOVED AT THIS LOCATION AND ALL CORROSION AREAS WERE CUT OUT OF THE SKIN WITH A 1 X 3 CUTOUT AND A 10 X 5 CUTOUT. BOTH CUTOUTS WERE REP
- [SDR DL72W990583](https://openairdocs.org/sdr/DL72W990583.md): Stringer · cracked · Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/Stringer
  > A.25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 629 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.
- [SDR DL72W990582](https://openairdocs.org/sdr/DL72W990582.md): Stringer · cracked · Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/Stringer
  > A.25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 656.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.
- [SDR DL72W990581](https://openairdocs.org/sdr/DL72W990581.md): Stringer · cracked · Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/Stringer
  > A.25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 686.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.
- [SDR DL72W990476](https://openairdocs.org/sdr/DL72W990476.md): Angle · cracked · Mar 1, 1999 · N2821W · Boeing 727247 · Wing Miscellaneous Structure
  > CRACK ORIGINATING UNDER I/B UPSTOP PAD ON NR 7 SLAT ANGLE RUNNING I/B.25 INCH. REPAIRED PER MM 57-40-0 PAGE 816.
- [SDR DL72W981379](https://openairdocs.org/sdr/DL72W981379.md): Beam · chafed · Jul 1, 1998 · N2821W · Boeing 727247 · Wing Miscellaneous Structure
  > MLG CHAFFING FWD SIDE OF MLG BEAM BELOW STR 18A. REPAIR PER M/M 57-43-0.
- [SDR DL72W981378](https://openairdocs.org/sdr/DL72W981378.md): Web · cracked · Jul 1, 1998 · N2821W · Boeing 727247 · Fuselage Miscellaneous Structure
  > VERT WEB CRACKED AT LIGHTENING HOLES STA 1280 AND 1303 LT. REPAIRED PER MM 53-11-0 P 828.
- [SDR DL72W981377](https://openairdocs.org/sdr/DL72W981377.md): Web · cracked · Jul 1, 1998 · N2821W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CRACK IN RT AIR STAIR WEB AT STA 1240 VERTICAL WEB. REPAIRED PER MM 53-11-0 P 832.
- [SDR DL72W980163](https://openairdocs.org/sdr/DL72W980163.md): Battery Pack · discharged · Jan 19, 1998 · N2821W · Boeing 727247 · Emergency Lighting
  > AFT AISLE OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD.
- [SDR DL72W980162](https://openairdocs.org/sdr/DL72W980162.md): Battery Pack · discharged · Jan 19, 1998 · N2821W · Boeing 727247 · Emergency Lighting
  > AFT OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD.
- [SDR DL72W972458](https://openairdocs.org/sdr/DL72W972458.md): Bracket · cracked · Nov 24, 1997 · N2821W · Boeing 727247 · Leading Edge Slat Actuator
  > A.125 INCH VISIBLE CRACK NR 1 L/E FLAP ACTUATOR I/B MOUNT BRACKET. REPAIR PER MM 57-20-21.
- [SDR DL72W972457](https://openairdocs.org/sdr/DL72W972457.md): Baffle · cracked · Nov 24, 1997 · N2821W · Boeing 727247 · Leading Edge Devices
  > A.75 INCH CRACK NR 3 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACT AND.5 INCH CRACK NR 2 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACTUATOR. REPAIR PER MM 57-54-0.
- [SDR DL72W970476](https://openairdocs.org/sdr/DL72W970476.md): Indicator · inoperative · Mar 13, 1997 · N2821W · Boeing 727247 · Trailing Flap Position Indicating System
  > OUTBOARD FLAPS IND. 25/25 FLAPS 30 SELECTED. AT APPROXIMATELY 200 FEET, GPWS WARNING FLAPS. PERFORMED GO AROUND I.A.W. DELTA PROCEDURES AND COMPLIED WITH P.O.M. NOTE ALT FLAP MASTER USED. REPLACED OUTBOARD FLAP IND AND RESET. CKS OK PER MM CHAPT. 27.
- [SDR DL72W962711](https://openairdocs.org/sdr/DL72W962711.md): Skin · corrosion · Dec 8, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON FUSELAGE SKIN AT STA 486. REPAIRED IN ACCORDANCE DAL ER/A 258313-14, REV A.
- [SDR DL72W962712](https://openairdocs.org/sdr/DL72W962712.md): Skin · corrosion · Dec 3, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON THE LOWER EDGE OF THE C-1 DOOR CUTOUT AT STATION 580. REPAIRED PER DAL ER/A 304497-14, REV A.
- [SDR DL72W962651](https://openairdocs.org/sdr/DL72W962651.md): Frame · cracked · Dec 2, 1996 · N2821W · Boeing 727247 · Passenger/Crew Doors
  > R-1 DOORS 550 HAS A 1.5 INCH CRACK IN AFT LOWER FRAME AT CUTOUT FOR LOCK MECHANISM. DRILLED UP REPAIR DOUBLER PER M/M 52-12-0 PG 807, INSTALLED DOUBLER PER M/M 52-12-0 PG 807, CLOSED WEB.
- [SDR DL72W962650](https://openairdocs.org/sdr/DL72W962650.md): Frame · cracked · Nov 25, 1996 · N2821W · Boeing 727247 · Passenger/Crew Doors
  > A.375 INCH CRACK R-2 DOOR FRAME AT UPPER HINGE CUTOUT. REMOVED DOOR FROM A/C, REPAIRED DOOR FRAME PER SRM 52-40-2.
- [SDR DL72W960576](https://openairdocs.org/sdr/DL72W960576.md): Skin · cracked · Mar 8, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING LETTER CHECK AT TAMPA, A.5 INCH CRACK IN THE FUSELAGE SKIN AT STA 1098 ALONG S-1. CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIGURE 3.
- [SDR DL72W960519](https://openairdocs.org/sdr/DL72W960519.md): Angle · cracked · Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge Devices
  > FOUND DURING B-2 LETTER CHECK - NR 8 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR 5A.
- [SDR DL72W960518](https://openairdocs.org/sdr/DL72W960518.md): Angle · cracked · Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge Devices
  > FOUND DURING B-2 LETTER CHECK - 1 INCH CRACK NR 1 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 PAR 12.
- [SDR DL72W954158](https://openairdocs.org/sdr/DL72W954158.md): Eel Power Supply · failed · Oct 31, 1995 · N2821W · Boeing 727247 · Emergency Lighting
  > IRREG - CABIN EMERG EXIT LIGHT AT AIRSTAIR DOOR INOP. CORRECTIVE ACTION - REPLACED PWR SUPPLY AND BATTERY.
- [SDR DL72W954071](https://openairdocs.org/sdr/DL72W954071.md): Lines · cracked · Oct 18, 1995 · N2821W · Boeing 727247 · Aircraft Fuel Distribution System
  > FUEL VENTED OUT OF RT VENT BOX ON ACTIVE RUNWAY, FUEL MIGRATING FROM OTHER TANK CAUSING THE NR 3 TANK TO OVERFILL. FOUND CRACK LINES MFG (P/N 65-22731-2 AND 65-16710-52) REF IPC 28-30-0-16 ITEMS 120 AND 140. BOTH LINES SENT TO SHOP FOR REPAIRS.
- [SDR DL72W953950](https://openairdocs.org/sdr/DL72W953950.md): Frame · misdrilled · Sep 29, 1995 · N2821W · Boeing 727247 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF E.O. 4-61904-3AD FOR THE LT STA 783.95 FRAME, MTC FOUND THAT ONE OF THE FASTENERS INSTALLED THROUGH FRAME AND RING DOUBLER (65-16236-35) FELL OUT IN THE RADIUS OF THE 65C36280-3 REPAIR ANGLE. REPAIRS ACCOMPLISHED PER DL ERA 302567-14A
- [SDR DL72W953842](https://openairdocs.org/sdr/DL72W953842.md): Eel Pack · discharged · Sep 28, 1995 · N2821W · Boeing 727247 · Emergency Lighting
  > RIGHT FWD OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK NORMAL.
- [SDR DL72W953208](https://openairdocs.org/sdr/DL72W953208.md): Stiffner · cracked · Jul 27, 1995 · N2821W · Boeing 727247 · Leading Edge Devices
  > I/B SPAR STIFFENER CRACKED LWR END AT NR 7 SLAT I/B TRACK. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21 PG 813.
- [SDR DL72W953005](https://openairdocs.org/sdr/DL72W953005.md): Overheat Loop · cut · Jul 9, 1995 · N2821W · Boeing 727247 · Overheat Detection
  > AT FL 270, 25 MIN INTO FL, LOWER AFT BODY O/H LIGHT ILLUM INTERMITTENTLY FOR APPROX 1 MIN, THEN STEADY. C/W POM PROC AND LIGHT REMAINED ILLUM FOR 15 TO 20 MIN WITH NR 2 THROTTLE AT IDLE. AFTER 20 MIN WITH NR 2 THROTTLE AT IDLE LIGHT EXT WITH A COUPLE OF FLIC
- [SDR DL72W951928](https://openairdocs.org/sdr/DL72W951928.md): Skin · cracked · May 7, 1995 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED 1 INCH LONG STA 684 ONE INCH ABOVE STR 18R. CUT OUT SKIN DAMAGE 2.5 LONG BY 1.0625 WIDE,.5 INCH RAD TYP, USING THE SRM 53-30-3 PAGES 6 AND 7.

## 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 = 'N2821W' AND deregistration_id = 'N2821W-2012-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2821W-2012-08-27/reports

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