# Service difficulty reports: N2809W, cancelled Feb 29, 2000

A list on [N2809W, cancelled Feb 29, 2000](https://openairdocs.org/deregistered/N2809W-2000-02-29.md).

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

- [SDR DL72W991954](https://openairdocs.org/sdr/DL72W991954.md): Angle · cracked · Sep 2, 1999 · N2809W · Boeing 727247 · Leading Edge Devices
  > NR 6 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED ANGLE PER M/M 57-20-21 PAGE 813.
- [SDR DL72W991953](https://openairdocs.org/sdr/DL72W991953.md): Bracket · cracked · Sep 2, 1999 · N2809W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 8 SLAT ACTUATOR I/B AND O/B MOUNT BRACKETS CRACKED ON WEBS. REPAIRED PER M/M 57-20-21 PAGE 812.
- [SDR DL72W991951](https://openairdocs.org/sdr/DL72W991951.md): Web · cracked · Sep 2, 1999 · N2809W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON F1 LETTER C,.25 INCH CRACK LOWER LIGHTENING HOLE RT VERTICAL TORQUE BOX WEB STA 1260. REPAIRED PER MM 53-11-0.
- [SDR DL72W991802](https://openairdocs.org/sdr/DL72W991802.md): Cadc · failed · Aug 12, 1999 · N2809W · Boeing 727247 · Air Data Computer
  > AFTER T/O CAPTAINS MACH INDICATOR DISPLAYED AN OFF FLAG. ALSO, CAPTAINS ALTIMETER HAD A STANDBY FLAG ALSO NEITHER TRANSPONDER DISPLAYED MODE C TO ATL. REPLACED NR 1 CADC CHECKED NORMAL.
- [SDR DL72W982637](https://openairdocs.org/sdr/DL72W982637.md): Skin · cracked · Dec 28, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE UPPER FUSE SKIN AT BS 351 ON THE UPPER ROW OF THE S24R LAP SPLICE WAS FOUND CRACKED. THE CRACK EXTENDED THRU THREE CONSECUTIVE FASTENERS WITH A TOTAL LENGTH OF 3. REPAIRED PER ERA 366371-14.
- [SDR DL72W982181](https://openairdocs.org/sdr/DL72W982181.md): Light · inop · Oct 21, 1998 · N2809W · Boeing 727247 · Emergency Lighting
  > COCKPIT OVERHEAD EMERGENCY LIGHT PACK INOP ON TEST. REPLACED BATTERIES, CKS OK.
- [SDR DL72W982110](https://openairdocs.org/sdr/DL72W982110.md): Light · illuminated · Oct 11, 1998 · N2809W · Boeing 727247 · Landing Gear Position and Warning
  > AFTER GEAR EXTENSION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN NOSE GEAR LIGHT. POM PROCEDURES COMPLIED WITH AND A SAFE INDICATION OBTAINED AFTER MANUAL EXTENSION PROCEDURES ACCOMPLISHED.
- [SDR DL72W981658](https://openairdocs.org/sdr/DL72W981658.md): Sequence Valve · cracked · Aug 11, 1998 · N2809W · Boeing 727247 · Landing Gear Retraction/Extension System
  > DURING CLIMBOUT, LOST 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID QTY. FOUND RIGHT MLG DOOR SEQUENCING VALVE CRACKED. REPLACED VALVE. LEAK CHECK AND GEAR SWING GOOD.
- [SDR DL72W981401](https://openairdocs.org/sdr/DL72W981401.md): Battery Rack · discharged · Jul 2, 1998 · N2809W · Boeing 727247 · Emergency Lighting
  > SEAT ROW 18 ABCDEF OVERHEAD EMER LIGHT INOP. REPLACED BATTERY RACK OPS NOW NML.
- [SDR DL72W981393](https://openairdocs.org/sdr/DL72W981393.md): Skin · cracked · Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE BELLY SKIN WAS FOUND WITH CRACKS AND CORROSION AT STA 700 AND STR 28L - 28R. BELLY SKIN WILL BE REPLACED DUE TO NUMEROUS EXISTING REPAIRS. REPAIRED PER ERA 303637-14.
- [SDR DL72W981384](https://openairdocs.org/sdr/DL72W981384.md): Skin · gouged · Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS GOUGED FWD OF THE L1 DOOR AT S10L LAP SPLICE. REPAIRED PER ERA 331851-14.
- [SDR DL72W981383](https://openairdocs.org/sdr/DL72W981383.md): Stringer · corroded · Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER 29R WAS FOUND WITH CORROSION AT FS 950E PLUS 10. A NEW SECTION OF STRINGER IS SPLICED IN. REPAIRED PER ERA 331848-14.
- [SDR DL72W981382](https://openairdocs.org/sdr/DL72W981382.md): Spar Chord · cracked · Jun 29, 1998 · N2809W · Boeing 727247 · Wing Spar
  > FRONT SPAR UPPER CHORD WAS FOUND WITH A CRACK IN THE FORWARD FLANGE AT A FASTENER HOLE AT APPROX WL340. REPAIRED PER ERA 331817-14.
- [SDR DL72W981381](https://openairdocs.org/sdr/DL72W981381.md): Stringer · corroded · Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L WAS FOUND CORRODED. THE STRINGER WAS TRIMMED AT STA 950D+10 AND THE AFT PORTION REMOVED. REPAIRED PER ERA 331787-14.
- [SDR DL72W981214](https://openairdocs.org/sdr/DL72W981214.md): Frame · cracked · Jun 8, 1998 · N2809W · Boeing 727247 · Fuselage Main, Frame
  > FS 784 FRAME ON THE LT SIDE HAD TWO CRACKS AT THE SECOND HOLE UP FROM THE FLOOR LINE. REPAIRED PER ERA 331783-14AD.
- [SDR DL72W981225](https://openairdocs.org/sdr/DL72W981225.md): Actuator · loose · Jun 1, 1998 · N2809W · Boeing 727247 · Drag Control Actuator
  > NR 13 SPOILER ACTUATOR MOUNT LOWER INBD AND OUTBD BOLTS ARE LOOSE. REPAIRED MOUNT HOLES IAW MM 57-42-0.
- [SDR DL72W981244](https://openairdocs.org/sdr/DL72W981244.md): Trunnion · cracked · May 29, 1998 · N2809W · Boeing 727247 · Fuselage, Landing Gear Attach Fittings
  > RT MLG TRUNNION BEAM SUPPORT FITTING AT FS 940 FOUND WITH 1.5 INCH FATIGUE CRACK ON INBRD SURFACE, WL 190. REPAIRED WITH FABRICATED DOUBLER PER ER/A 373040-14. CRACK FOUND DURING MID VISIT INSPECTION.
- [SDR DL72W981354](https://openairdocs.org/sdr/DL72W981354.md): Floorbeam · corroded · May 14, 1998 · N2809W · Boeing 727247 · Fuselage Main, Floor Beam
  > REMOVED EXISTING T-CAP REPAIR, FWD AND AFT SPLICE ANGLES, 1 VERTICAL STIFFENER AND 1 FLOORBOARD SUPPORT. REMOVED EXISTING T-CAP FROM C/L TO RBL 52. BEGAN DRILLING NEW T-CAP. COMPLETED FABRICATION OF REPAIR PER SRM 53-10-8 PG 56-57. INSTALLED T-CAP BEAM SPL
- [SDR DL72W980068](https://openairdocs.org/sdr/DL72W980068.md): Engine · bird strike · Jan 9, 1998 · N2809W · Boeing 727247 · Engine (Turbine/Turboprop)
  > AIRCRAFT FLEW THROUGH FLOCK OF GEESE. NR 1 AND 2 ENGINES WILL BE REPLACED. NR 3 WILL BE BORESCOPED. NR 6 SLAT WILL BE REPLACED. RADOME AND RADAR ANTENNA WILL BE REPLACED.
- [SDR DL72W971480](https://openairdocs.org/sdr/DL72W971480.md): Trunnion Ftg · corrosion · Jul 23, 1997 · N2809W · Boeing 727247 · Wing, Landing Gear Attach Fittings
  > THE TRUNNION ATTACH FITTING OUTBOARD CLEVIS AND MATING TEE ATTACH FLANGE HAD CORROSION IN THE BORE. IN ADDITION, THE COUTER SINK THROUGH THE ATTACH FITTING LUG WAS FOUND TO EXTEND ALMOST COMPLETELY THROUGH THE LUG FLANGE. THIS DAMAGE WAS REMOVED BY OVERSIZED
- [SDR DL72W971452](https://openairdocs.org/sdr/DL72W971452.md): Spar Cap · damaged · Jul 15, 1997 · N2809W · Boeing 727247 · Wing Spar
  > THE SUBJECT AIRCRAFT EXPERIENCED A COLLAPSE OF THE RT MAIN LANDING GEAR DURING LANDING ROLLOUT. THIS RESULTED IN DAMAGE TO THE RT WING FRONT SPAR LOWER CAP ON THE OUTBOARD END. THE EXTENT OF THE DAMAGE REQUIRED THAT THE LOWER CAP TO BE CUT AT APPROX FS 770 A
- [SDR DL72W970760](https://openairdocs.org/sdr/DL72W970760.md): Battery Pack · discharged · Apr 24, 1997 · N2809W · Boeing 727247 · Emergency Lighting
  > LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS OK.
- [SDR DL72W970759](https://openairdocs.org/sdr/DL72W970759.md): Light · inoperative · Apr 24, 1997 · N2809W · Boeing 727247 · Emergency Lighting
  > AFT STAIRS EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CHECKS OK.
- [SDR DL72W970638](https://openairdocs.org/sdr/DL72W970638.md): Skin · cracked · Apr 9, 1997 · N2809W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND A 1.5 IN CRACK RT ELEV LOWER SKIN FWD OF TAB. REPAIRED PER SRM 55-20-3.
- [SDR DL72W961468](https://openairdocs.org/sdr/DL72W961468.md): Skin · cracked · May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE SKIN JUST FWD OF STA 700 BETWEEN STR 28L AND 28R NEAR BL 0 WAS FOUND CRACKED AND CORRODED. REPAIRED WITH A DOUBLER AND TRIPLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-9-57.
- [SDR DL72W961283](https://openairdocs.org/sdr/DL72W961283.md): Skin · cracked · May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > SKIN CORROSION AND CRACK JUST FWD OF STA 700 BETWEEN STRINGERS 28L AND 28R NEAR BL 0. CUTOUT MEASURED 7.5 BY 3.75 INCH. REPAIRED PER DAL ER/A 303637-14, REV A.
- [SDR DL72W961462](https://openairdocs.org/sdr/DL72W961462.md): Skin · corrosion · May 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > SKIN CORROSION AT FS 720F AT STR 27R. REMOVED A 1.75 INCH BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730. ERA WILL INCORPORATE BOTH REPAIRS INTO ONE REPAIR.
- [SDR DL72W961282](https://openairdocs.org/sdr/DL72W961282.md): Skin · corroded · May 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > SKIN CORROSION AT STA 720F AT STRINGER 27R. DAMAGE REMOVAL RESULTED IN A 1.75 BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730, ERA 213172. EXISTING REPAIR REQUIRED THE REMOVAL OF THE CORNER OF THE LWR SKIN AT STA 740 AND STRINGER 26R. REPAIRED PE
- [SDR DL72W961234](https://openairdocs.org/sdr/DL72W961234.md): Floor Beam · corroded · May 15, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor Beam
  > FOUND ON MV1 CK, CORROSION/RIVETS SHEARD AT CABIN FLOOR BEAM STA 1070 AT RT O/B GALLEY FLOOR TRACK. REPAIRED PER M/M 53-20-11 FIG 804.
- [SDR DL72W961171](https://openairdocs.org/sdr/DL72W961171.md): Floor Beam · corroded · May 14, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOOR BEAM UPPER ANGLE STA 400 RBL 55. REPAIRED PER M/M 53-20-11 PG 811 B.
- [SDR DL72W961047](https://openairdocs.org/sdr/DL72W961047.md): Light · inoperative · Apr 28, 1996 · N2809W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES.
- [SDR DL72W960697](https://openairdocs.org/sdr/DL72W960697.md): Skin · cracked · Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge Devices
  > INNER SKIN CRACKED AT NUTPLATES, RIBS 10, 11, 12 AND 13. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.
- [SDR DL72W960696](https://openairdocs.org/sdr/DL72W960696.md): Rib · cracked · Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge Devices
  > DURING INSPECTION, FOUND NR 6 L/E SLAT WITH INTERNAL SUPPORT RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72W960695](https://openairdocs.org/sdr/DL72W960695.md): Rib · cracked · Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge Devices
  > DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH INTERNAL SUPPORT RIB NR 11 CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72W960592](https://openairdocs.org/sdr/DL72W960592.md): Attach Fitting · broken · Mar 16, 1996 · N2809W · Boeing 727247 · Landing Gear Door Actuator
  > LT MAIN LANDING GEAR DOOR OPENED IN FLIGHT. FOUND LANDING GEAR DOOR ACTUATOR ATTACH FITTING BROKEN, IPC 32-10-4 FIG 2 ITEM 250.
- [SDR DL72W960321](https://openairdocs.org/sdr/DL72W960321.md): Skin · worn · Feb 13, 1996 · N2809W · Boeing 727247 · Ailerons
  > DURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. SPLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801.
- [SDR DL72W960320](https://openairdocs.org/sdr/DL72W960320.md): Web · cracked · Feb 10, 1996 · N2809W · Boeing 727247 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 1.25 INCH CRACK AT STA 294.5, APPROXIMATELY AT WL 170. THE DAMAGED PORTION WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAPS WAS INSTALLED IN ACCORDANCE WITH B727-53-145.
- [SDR DL72W960309](https://openairdocs.org/sdr/DL72W960309.md): Angle · cracked · Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge Slat Control System
  > A 1.5 INCH CRACK AT NR 1 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57 20-21.
- [SDR DL72W960308](https://openairdocs.org/sdr/DL72W960308.md): Bracket · cracked · Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge Slat Control System
  > FOUND AT LETTER CHECK, NR 6 L/E FLAP ACTUATOR MOUNT BOX CRACKED, I/B SIDE UPPER AND LWR CORNERS. REPAIRED PER MM 57-20-21.
- [SDR DL72W960307](https://openairdocs.org/sdr/DL72W960307.md): Stringer · cracked · Feb 9, 1996 · N2809W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > A 1 INCH CRACK THROUGH HORIZ LEG OF STR 18A AND STA 950. REPAIRED PER MM 53-12-0, FOUND AT LETTER CHECK.
- [SDR DL72W960306](https://openairdocs.org/sdr/DL72W960306.md): Angle · cracked · Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge Devices
  > SLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER MM 57-54-0.
- [SDR DL72W953149](https://openairdocs.org/sdr/DL72W953149.md): Angle · cracked · Jul 8, 1995 · N2809W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA302097-14AD.
- [SDR DL72W952850](https://openairdocs.org/sdr/DL72W952850.md): Skin · gouged · Jun 26, 1995 · N2809W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND TOOLING DAMAGE TO RT FUSELAGE NOSE AT FS 243.7, APPROXIMATELY HALFWAY UP THE SKIN PANEL. REPAIRED PER SRM 53-30-3 FIG 3.
- [SDR DL72W952861](https://openairdocs.org/sdr/DL72W952861.md): Rib · cracked · Jun 22, 1995 · N2809W · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 3 SLAT PANEL WAS FOUND WITH L/E RIB NR 17 CRACKED. REPAIRED PER MM 57-54-00 FIG 809.
- [SDR DL72W952853](https://openairdocs.org/sdr/DL72W952853.md): Bulkhead · mismfg · Jun 22, 1995 · N2809W · Boeing 727247 · Fuselage Main, Bulkhead
  > DURING INSPECTION, LT FS 178 BULKHEAD HAD ACCESS HOLE. INSTALLED PER SRM 53-10-9 FIG 3.
- [SDR DL72W952851](https://openairdocs.org/sdr/DL72W952851.md): Bulkhead · mismfg · Jun 22, 1995 · N2809W · Boeing 727247 · Fuselage Main, Bulkhead
  > DURING INSPECTION, FS 178 RT BULKHEAD HAD AN ACCESS HOLE. INSTALLED PER SRM 53-10-0 FIG 3.
- [SDR DL72W952782](https://openairdocs.org/sdr/DL72W952782.md): Rib · cracked · Jun 22, 1995 · N2809W · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 9 CRACKED. REPAIRED PER SRM 57-54-0 FIG 805.

## 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 = 'N2809W' AND deregistration_id = 'N2809W-2000-02-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2809W-2000-02-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.