# Service difficulty reports: N2810W, cancelled Feb 1, 2000

A list on [N2810W, cancelled Feb 1, 2000](https://openairdocs.org/deregistered/N2810W-2000-02-01.md).

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

- [SDR DL72W992456](https://openairdocs.org/sdr/DL72W992456.md): Light · inop · Nov 7, 1999 · N2810W · Boeing 727247 · Emergency Lighting
  > FC AISLE EMERGENCY LIGHTS AFT OF LIFE RAFT COMPARTMENT INOP. REPLACED CHARGING RACK.
- [SDR DL72W992099](https://openairdocs.org/sdr/DL72W992099.md): Power Supply · inop · Sep 18, 1999 · N2810W · Boeing 727247 · Emergency Lighting
  > DURING S/C, FOUND OVERHEAD EMERGENCY EXIT SIGN AT ROW 3 INOP. REPLACED POWER SUPPY RACK ASSY, OPS NORMAL.
- [SDR DL72W991974](https://openairdocs.org/sdr/DL72W991974.md): Battery Pack · discharged · Sep 6, 1999 · N2810W · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHTS TEST INOP. REPLACED PACK.
- [SDR DL72W991973](https://openairdocs.org/sdr/DL72W991973.md): Battery Pack · discharged · Sep 6, 1999 · N2810W · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT TEST CORRECTLY. REPLACED BATTERY PACKS.
- [SDR DL72W991309](https://openairdocs.org/sdr/DL72W991309.md): Web · cracked · Jun 10, 1999 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A CRACK BETWEEN BS 294 AND 286 AT APPROX WL 170. REPAIRED PER ERA 367566-14.
- [SDR DL72W991296](https://openairdocs.org/sdr/DL72W991296.md): Angle · cracked · Jun 8, 1999 · N2810W · Boeing 727247 · Spoilers
  > NR 13 SPOILER ACTUATOR SUPPORT FITTING O/B ATTACH ANGLE CRACKED. REPLACED ANGLE PER M/M 57-42-0 PG 802.
- [SDR DL72W991295](https://openairdocs.org/sdr/DL72W991295.md): Skin · cracked · Jun 8, 1999 · N2810W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND ON F1 LETTER CK,.375 INCH CRACK ON LT ELEVATOR LOWER SKIN. REPAIRED PER SRM 55-20-3.
- [SDR DL72W991293](https://openairdocs.org/sdr/DL72W991293.md): Frame · cracked · Jun 8, 1999 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT F-1 LETTER CHECK, AFT ENTRY DOOR CUTOUT RT FRAME HAS.5 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.
- [SDR DL72W991088](https://openairdocs.org/sdr/DL72W991088.md): Skin · dented · May 15, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DENTED BETWEEN FS 1130 AND 1166 BETWEEN STRINGERS 23R AND 24R. THE SKIN DENT WAS CUT OUT WITH A 22.5 INCH X 6.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367383-14, REV A.
- [SDR DL72W991066](https://openairdocs.org/sdr/DL72W991066.md): Skin · gouged · May 13, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > GOUGE ON THE OUTER SKIN FS 1148 STRINGER 24R. REPAIRED PER ERA 367383-14.
- [SDR DL72W990147](https://openairdocs.org/sdr/DL72W990147.md): Frame · dented · Jan 20, 1999 · N2810W · Boeing 727247 · Fuselage Main, Frame
  > BS 1030 FRAME I/B OF LBL 40 WAS FOUND DENTED AT THE TOP AND EXCEEDED SRM ALLOWABLE LIMITS. A CUT OUT WAS NECESSARY. REPAIRED PER ERA 332661-14
- [SDR DL72W990145](https://openairdocs.org/sdr/DL72W990145.md): Skin · corroded · Jan 20, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > SKIN WAS FOUND CORRODED AND THREE ADDITIONAL REPAIRS REMOVED AND ALL DAMAGE INCORPORATED INTO ONE REPAIR. DAMAGE IS LOCATED AT BS 673, S28L. REPAIRED PER ERA 303790-14, REV C.
- [SDR DL72W990144](https://openairdocs.org/sdr/DL72W990144.md): Bulkhead Web · cracked · Jan 20, 1999 · N2810W · Boeing 727247 · Fuselage Main, Bulkhead
  > BS 178 BULKHEAD WAS FOUND WITH CRACKS IN THE TYP LOCATIONS AS SHOWN IN THE BACO SRM 53-10-9, FIGURE 14. ADDITIONAL CRACK FOUND OUTSIDE THE TYP LOCATION. REPAIRED PER ERA 332712-14.
- [SDR DL72W990143](https://openairdocs.org/sdr/DL72W990143.md): Stringer · damaged · Jan 20, 1999 · N2810W · Boeing 727247 · Vertical Stabilizer
  > WEAR WAS FOUND ON THE S7L ON THE VERT STAB. DAMAGE IS TO THE O/B SURFACE OF THE UPPER FLANGE AT APPROX FIN STA 230. REPAIRED PER ERA 332689-14.
- [SDR DL72W990142](https://openairdocs.org/sdr/DL72W990142.md): Spar Chord · cracked · Jan 20, 1999 · N2810W · Boeing 727247 · Wing Spar
  > THE FRONT SPAR CHORD WAS FOUND WITH CRACKS IN THE FWD FLANGE AT A FASTENER HOLE AT APPROX WS 333. REPAIRED PER ERA 332687-14.
- [SDR DL72W990141](https://openairdocs.org/sdr/DL72W990141.md): Frame · misdrilled · Jan 20, 1999 · N2810W · Boeing 727247 · Fuselage Main, Frame
  > MTC DISCOVERED TWO MISDRILLED HOLES IN THE I/B CHORD OF THE BS 560 FRAME NEAR S27R. REPAIRED PER ERA 332713-14.
- [SDR DL72W990140](https://openairdocs.org/sdr/DL72W990140.md): Skin · cracked · Jan 20, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUR HOLES WERE DISCOVERED CRACKED IN THE SKIN AT BS 940. THE HOLES WERE O/S THRU THE SKIN, STRINGER (18A) AND FITTING. FINAL HOLES ARE SHOWN ON FIGURE 1 OF ERA 332686-14. REPAIRED PER ERA 332686-14.
- [SDR DL72W990036](https://openairdocs.org/sdr/DL72W990036.md): Trunnion · corroded · Jan 5, 1999 · N2810W · Boeing 727247 · Fuselage, Landing Gear Attach Fittings
  > AT MV2 FOUND BOLT BORE CORRODED LT TRUNNION CAP FWD BORE NLG. REMOVED HOLE TO.892 TO REMOVE CORROSION PER MM 53-40-0, OK TREAT/PAINT HOLE.
- [SDR DL72W990035](https://openairdocs.org/sdr/DL72W990035.md): Trunnion · corroded · Jan 5, 1999 · N2810W · Boeing 727247 · Fuselage, Landing Gear Attach Fittings
  > FOUND AT MV2 BOLT BORE, CORROSION RT NLG TRUNNION CAP FWD BORE. REAMED HOLE TO 0907 TO REMOVE CORROSION PER MM 53-40-00 TREAT/PAINT.
- [SDR DL72W981743](https://openairdocs.org/sdr/DL72W981743.md): Switch · failed · Aug 23, 1998 · N2810W · Boeing 727247 · Cabin Cooling System
  > ON DESCENT, MOMENTARY WHITE SMOKE ON COCKPIT AND A MUSTY OILY SMELL IN CABIN AND COCKPIT. GALLEYS AND GASPER FANS TURNED OFF CABIN RAISED TO 9500 FT SMOKE AND SMELL DISSIPATED. RAN ENGINES FOUND LEFT PACK OVERHEATING BUT WOULD NOT TRIP. REPLACED TURBINE INLE
- [SDR DL72W981442](https://openairdocs.org/sdr/DL72W981442.md): Air Distribution · smoke · Jul 8, 1998 · N2810W · Boeing 727247 · Air Distribution System
  > SMOKE IN CBN/COCKPIT DURING DESCENT 22K TO 11K FT AT IDLE PWR. TOOK A/C FOR PWR RUN. UNABLE TO DUPLICATE. PACK OPN/BLEEDS CK NORMAL.
- [SDR DL72W981254](https://openairdocs.org/sdr/DL72W981254.md): Battery Pack · discharged · Jun 12, 1998 · N2810W · Boeing 727247 · Emergency Lighting
  > RT OVERWING EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72W980768](https://openairdocs.org/sdr/DL72W980768.md): Bracket · cracked · Apr 7, 1998 · N2810W · Boeing 727247 · Leading Edge Slat Actuator
  > FOUND ON E1 LETTER CK, NR 8 SLAT ACTUATOR I/B MOUNT BRACKET IS CRACKED. REPAIR PER MM 57-20-21.
- [SDR DL72W980767](https://openairdocs.org/sdr/DL72W980767.md): Rib · cracked · Apr 7, 1998 · N2810W · Boeing 727247 · Leading Edge Devices
  > FOUND ON E1 LETTER CK, 1 INCH CRACK AT NR 7 SLAT ACTUATOR ATTACH RIB I/B SIDE. REPAIRED PER MM 57-54-0.
- [SDR DL72W980766](https://openairdocs.org/sdr/DL72W980766.md): Angle · cracked · Apr 7, 1998 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON E1 LETTER CK, LT KEEL BEAM ANGLE CRACKED I/B OF APU MOUNT STA 870. REPLACED ANGLE PER SRM 53-10-9.
- [SDR DL72W980764](https://openairdocs.org/sdr/DL72W980764.md): Bracket · cracked · Apr 7, 1998 · N2810W · Boeing 727247 · Leading Edge Slat Actuator
  > FOUND ON E1 LETTER CK,.25 INCH VISIBLE CRACK INBD MOUNT BRACKET NR 1 L/E FLAP ACTUATOR. REPAIRED PER MM 57-20-21.
- [SDR DL72W980513](https://openairdocs.org/sdr/DL72W980513.md): Skin · cracked · Mar 3, 1998 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN R1 DOOR CUTOUT SURROUND UPPER HINGE CUTOUT, CRACK REPAIR. THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE UNDERLYING REINFORCING DOUBLER (BEAR STRAP). THE SKIN WAS LOCALLY CUTOUT TO ACCESS THE CRACK ANDTHE CRA
- [SDR DL72W971877](https://openairdocs.org/sdr/DL72W971877.md): Skin · cracked · Sep 19, 1997 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A/C WAS FOUND IN LGA ON 9-17-97 WITH A 3 CRACK IN THE FUSELAGE SKIN AT S20R BETWEEN STA 660 AND 680 AND OIL-CANNING CONDITION AT THE SAME STATION IN THE FIVE STRINGER BAYS BELOW THE CRACK. CRACK WAS REPAIRED PER SRM AND THE OIL-CANNING CONDITION WAS AUTHORIZE
- [SDR DL72W971813](https://openairdocs.org/sdr/DL72W971813.md): Skin · cracked · Sep 17, 1997 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND CRACK IN SKIN AFT OF FWD CARGO DOOR WITH EXTENSIVE OIL CANNING. REPAIRED PER ERA 362766-14.
- [SDR DL72W971492](https://openairdocs.org/sdr/DL72W971492.md): Sense Line · split · Jul 29, 1997 · N2810W · Boeing 727247 · Pneumatic Indicating System
  > LITE SMOKE IN CABIN AND COCKPIT ASSOCIATED WITH A/C SMELL WITH SMOKE. CABIN AND COCKPIT COOL AIR VERY INEFFICIENT. AIR FORCEFULLY BLOWING OUT OF RT RAM COOLING DOOR. LOST PRESSURIZATION IN CABIN WHEN THROTTLES ARE AT IDLE. FOUND HI PRESS REG SENSE LINE FOR
- [SDR DL72W970026](https://openairdocs.org/sdr/DL72W970026.md): Battery Pack · discharged · Jan 5, 1997 · N2810W · Boeing 727247 · Emergency Lighting
  > BOTH LT OVERWING INTERIOR EMERGENCY LIGHTS OUT ON OVERWING DOORS. REMOVED AND REPLACED OVERWING DOOR BATTERY PACKS PER M/M, CKD OK.
- [SDR DL72W962548](https://openairdocs.org/sdr/DL72W962548.md): Coalescer Bag · dirty · Nov 19, 1996 · N2810W · Boeing 727247 · Humidity Control System
  > AT FL 11,000 WITH LT PACK ONLY ON F/AS REPORTED, SMOKE IN CABIN COMING FROM OVHD VENTS. REPLACED LT WATER SEPARATOR BAG, RAN NR 1 ENG AND OPERATED BOTH PACKS. ALL OK, NO SMOKE.
- [SDR DL72W962109](https://openairdocs.org/sdr/DL72W962109.md): Battery · discharged · Sep 14, 1996 · N2810W · Boeing 727247 · Emergency Lighting
  > FOUND AFT AIRSTAIR_EMERGENCY EXIT LIGHTS AND LIGHT BELOW FLIGHT ATTENDANT PANEL INOP. REPLACED BATTERIES, RELAMPED, REPLACED EMERG. LIGHT ASSY AND RESECURED WIRES TO THE LIGHT ASSY BELOW FLT ATT PNL.
- [SDR DL72W961544](https://openairdocs.org/sdr/DL72W961544.md): Web · cracked · Jun 27, 1996 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > TORQUE BOX WEB CRACKED.5 INCH IN ADJACENT RT HAND RAIL STA 1233. INSTALLED DOUBLER PER MM 53-11-0.
- [SDR DL72W960808](https://openairdocs.org/sdr/DL72W960808.md): S-Duct Skin · cracked · Apr 8, 1996 · N2810W · Boeing 727247 · Nacelle/Pylon Structure
  > FOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING RT SIDE JUST FWD OF SADDLE PANEL, VERT STAB FRONT SPAR. INSTALLED PERMANENT REPAIR PER M/M 54-30-0 PG 801 FIG 802.
- [SDR DL72W960978](https://openairdocs.org/sdr/DL72W960978.md): Skin · corrosion · Apr 5, 1996 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND CORRODED JUST AFT OF THE BUTT SPLICE AT STA 480 FROM STRINGER 28R-28L. CORROSION WAS ALSO FOUND ON THE SPLICE STRAP AT ONE FASTENER LOCATION BETWEEN BL ZERO AND 28L. THE SKIN DAMAGE RESULTED IN CUTOUT THAT EXTENDS AFT APPROX. 1.75 INC
- [SDR DL72W960763](https://openairdocs.org/sdr/DL72W960763.md): Frame · cracked · Mar 29, 1996 · N2810W · Boeing 727247 · Passenger/Crew Doors
  > FOUND ON MV1 CHECK, L-2 DOOR FWD FRAME HAS.375 INCH CRACK AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.
- [SDR DL72W960764](https://openairdocs.org/sdr/DL72W960764.md): Skin · cracked · Mar 27, 1996 · N2810W · Boeing 727247 · Service Doors
  > FOUND ON MV1 CHECK,.375 INCH VISIBLE CRACK IN R-2 SERVICE DOOR AT UPPER FWD HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.
- [SDR DL72W960747](https://openairdocs.org/sdr/DL72W960747.md): Skin · cracked · Mar 27, 1996 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND UNDERLYING DOUBLER HAVE.25 INCH CRACK IN UPPER FWD CORNER OF L-1 DOOR CUTOUT. ACCOMPLISHED REPAIRS PER DL ERS 303365-14AD.
- [SDR DL72W960762](https://openairdocs.org/sdr/DL72W960762.md): S-Duct · cracked · Mar 25, 1996 · N2810W · Boeing 727247 · Nacelle/Pylon Structure
  > FOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING LT SIDE JUST ABOVE AND AFT OF ACCESS PLATE 9523. REPAIRED PER M/M 54-30-0 PG 801 FIG 802, INSTALLED PERMANENT REPAIR.
- [SDR DL72W970015](https://openairdocs.org/sdr/DL72W970015.md): Battery Pack · discharged · Jan 5, 1996 · N2810W · Boeing 727247 · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK, CHECKS NORMAL.
- [SDR DL72W954556](https://openairdocs.org/sdr/DL72W954556.md): Angle · cracked · Nov 28, 1995 · N2810W · Boeing 727247 · Leading Edge Devices
  > FOUND ON C-1 LETTER CHECK,.25 INCH CRACK IN SLAT COVE SKIN ATTACH ANGLE BELOW THE ANTI-ICE DUCT, NR 2 SLAT. REPAIRED PER MM 57-54-0.
- [SDR DL72W954555](https://openairdocs.org/sdr/DL72W954555.md): Angle · cracked · Nov 28, 1995 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON C-1 LETTER CHECK, 1.250 INCH CRACK IN THE RT W/W VERTICAL KEEL BEAM ANGLE AT STA 870. REPAIRED PER SRM 53-10-9 TIME LIMITED INSTRUCTIONS.
- [SDR DL72W952130](https://openairdocs.org/sdr/DL72W952130.md): Skin · corroded · May 9, 1995 · N2810W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING LETTER CHECK, FOUND LOWER FUSELAGE SKIN AT FS 720 BETWEEN STR 28L AND 28R WITH CORROSION DAMAGE THAT REQUIRED AN 8.5 INCH X 3 INCH SKIN CUT-OUT. AN EXTERNAL DOUBLER WAS INSTALLED PER DL ERA 301729-14 AD.
- [SDR DL72W951988](https://openairdocs.org/sdr/DL72W951988.md): Skin · damaged · May 8, 1995 · N2810W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND ON B2 LTR CK,.75 BY.625 HOLE LOWER SKIN RT ELEVATOR AFT NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3.
- [SDR DL72W951981](https://openairdocs.org/sdr/DL72W951981.md): Skin · cracked · May 8, 1995 · N2810W · Boeing 727247 · Nacelle/Pylon, Plate/Skin
  > FOUND ON B-2 LETTER CHECK,.25 INCH CRACK VERTICAL STABILIZER EXTERIOR SKIN AT RT SIDE FWD OF ACCESS PANEL 9524 NR 2 ENGINE INTAKE COWL. REPAIRED PER SRM 54-30-01.
- [SDR DL72W951980](https://openairdocs.org/sdr/DL72W951980.md): Web · cracked · May 8, 1995 · N2810W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON B-2 LETTER CHECK,.5 INCH CRACK TORQUE BOX VERTICAL WEB STA 1213 LT ABOVE AFT STAIRS STEPS CLOSE-OUT PANEL. REPAIRED PER M/M 53-11-0 PG 832.
- [SDR DL72W951979](https://openairdocs.org/sdr/DL72W951979.md): Skin · cracked · May 8, 1995 · N2810W · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > FOUND ON B-2 LETTER CHECK,.375 CRACK AT VERTICAL STABILIZER EXTERIOR SKIN RT SIDE STR 910 AT BASE OF VERTICAL. REPAIRED AS PER M/M 55-30-0 PG 801.

## 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 = 'N2810W' AND deregistration_id = 'N2810W-2000-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2810W-2000-02-01/reports

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