# Service difficulty reports: N2811W, cancelled Feb 1, 2000

A list on [N2811W, cancelled Feb 1, 2000](https://openairdocs.org/deregistered/N2811W-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 DL72W992766](https://openairdocs.org/sdr/DL72W992766.md): Rib · cracked · Dec 16, 1999 · N2811W · Boeing 727247 · Leading Edge Devices
  > NR 12 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0 FIG 804.
- [SDR DL72W992765](https://openairdocs.org/sdr/DL72W992765.md): Rib · cracked · Dec 16, 1999 · N2811W · Boeing 727247 · Leading Edge Devices
  > NR 11 RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 804.
- [SDR DL72W991858](https://openairdocs.org/sdr/DL72W991858.md): Smoke Light · illuminated · Aug 19, 1999 · N2811W · Boeing 727247 · Smoke Detection
  > LAV SMOKE LIGHT ILLUMINATED. LAVS CHECKED AND NO SMOKE/FIRE/FUMES OBSERVED. POM PROCEDURES FOLLOWED AND LIGHT AND CABIN CHIMES EXTINGUISHED WHEN SWITCH IN STARBOARD AFT LAV WAS PLACED OFF. VERIFIED LAV SMOKE DETECTORS IN ALL LAVS CHECK NORMAL. NO SIGNS OF
- [SDR DL72W991856](https://openairdocs.org/sdr/DL72W991856.md): Fan · failed · Aug 19, 1999 · N2811W · Boeing 727247 · Air Distribution Fan
  > ON DESCENT INTO PHL, FLT ATTENDANTS REPORTED SMOKE IN CABIN. POM PROCEDURES FOLLOWED BUT WERE UNABLE TO DETERMINE SOURCE. FLT ATTENDANTS LATER REPORTED, SUSPECTED AN ELECTRICAL PROBLEM. TROUBLESHOT PACK SYSTEM AND ALL NORMAL. FOUND GASPER FAN POPPING C/B A
- [SDR DL72W991680](https://openairdocs.org/sdr/DL72W991680.md): Bracket · cracked · Jul 26, 1999 · N2811W · Boeing 727247 · Leading Edge Devices
  > FOUND ON F-1 LETTER CK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED OUTBOARD END. REPAIRED PER MM 57-20-0.
- [SDR DL72W991609](https://openairdocs.org/sdr/DL72W991609.md): Bulb · failed · Jul 17, 1999 · N2811W · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHT INOP LOCATED ON EXTERIOR OW BETWEEN RT EMERGENCY ESCAPE HATCHES. RELAMPED SAME, CHECKS GOOD.
- [SDR DL72W990543](https://openairdocs.org/sdr/DL72W990543.md): Skin · cracked · Mar 12, 1999 · N2811W · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE BETWEEN FS 360 AND 681 REVEALED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INSPECTION CONFIRMED TWO CRACKS/CORROSION AT FS 505. THE SKIN WAS CUTOUT WITH A 2 X 1 CUTOUT IN THE LAP
- [SDR DL72W990139](https://openairdocs.org/sdr/DL72W990139.md): Engine · failed · Jan 22, 1999 · N2811W · Boeing 727247 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE OIL PRESSURE INDICATION WENT TO 100 PSI. ON ENGINE SHUTDOWN, INDICATION WENT TO 60 PSI. ALL OTHER ENGINE INDICATIONS NORMAL WHEN ENGINE RUNNING. SHUTDOWN ENGINE PER POM, REPLACED ENGINE.
- [SDR DL72W981260](https://openairdocs.org/sdr/DL72W981260.md): Slide · inoperative · Jun 13, 1998 · N2811W · Boeing 727247 · Escape Slide
  > 2R PASSENGER DOOR SLIDE PRESSURE LOW. REPLACED SLIDE ASSY.
- [SDR DL72W981066](https://openairdocs.org/sdr/DL72W981066.md): Skin · corroded · May 18, 1998 · N2811W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE SKIN AROUND THE FWD LAV PAN WAS FOUND CORRODED AROUND THE AFT LWR CORNER OF THE CUTOUT. REPAIRED PER ERA 331722-14.
- [SDR DL72W981065](https://openairdocs.org/sdr/DL72W981065.md): Bulkhead Web · cracked · May 18, 1998 · N2811W · Boeing 727247 · Fuselage Main, Bulkhead
  > CRACKS WERE DISCOVERED IN THE FS 178 BLKHD WEB AT WL 200 ANDLBL 5.8. REPAIRED PER ERA 331668-14.
- [SDR DL72W981012](https://openairdocs.org/sdr/DL72W981012.md): Brace · cracked · May 12, 1998 · N2811W · Boeing 727247 · Fuselage Miscellaneous Structure
  > DRAG BRACE SUPPORT ANGLE WAS FOUND DAMAGED AT APPROX BL 0. REPAIRED PER ERA 331714-14.
- [SDR DL72W981011](https://openairdocs.org/sdr/DL72W981011.md): Frame · cracked · May 12, 1998 · N2811W · Boeing 727247 · Fuselage Main, Frame
  > FS 784 LT OVERWING EXIT FRAME WAS FOUND CRACKED IN THE OUTBD CHORD AT THE LWR EDGE. REPAIRED PER ERA 331643-14AD.
- [SDR DL72W980972](https://openairdocs.org/sdr/DL72W980972.md): Fairing · cracked · Apr 22, 1998 · N2811W · Boeing 727247 · Aerodynamic Fairings
  > ANGLE OUT AT STA 957 LT SIDE OF FUSELAGE OVER STA 18A. FAIRING ATTACH WEB CRACKED REF EO 4-60175-3. STARTED FABRICATING REPAIR AS PER M/M 53-12-0 FIG 1. FABRICATED REPAIR PER M/M 53-12-0. HEAT TREATED REPAIR PORTS PER PS 900-4-1 NR 1. OK TO INST SPLICE ANG
- [SDR DL72W981016](https://openairdocs.org/sdr/DL72W981016.md): S-Duct · cracked · Apr 15, 1998 · N2811W · Boeing 727247 · Nacelle/Pylon Structure
  > NR 2 ENG INLET DUCT INTERNAL UPPER S-DUCT CRACKED AT 9 O'CLOCK AT STA 1151. BLENDED AREA AND DYE CHECKED AND TREATED AND PAINTED AREA, NO MORE CRACKS WERE FOUND. ALL WORK PERFORMED PER ERA 331669-14 OK PER PRI 331669-14.C/W ERA 33169-14.
- [SDR DL72W981015](https://openairdocs.org/sdr/DL72W981015.md): S-Duct · cracked · Apr 15, 1998 · N2811W · Boeing 727247 · Nacelle/Pylon Structure
  > NR 2 ENG INLET DUCT INTERNAL TWO CRACKS AT 3 O'CLOCK AND 11 O'CLOCK AT STA 1151 DOGHOUSE SIDE. REMOVED DAMAGE PER SRM 54-10-3 FIG 13. FABRICATED DOUBLER AND FILLER PER SRM 54-10-3 FIG 13. DYE CHECKED AREA PER PS 900-6-3 NR 1. NO CRACKS FOUND. OK TO INSTAL
- [SDR DL72W980971](https://openairdocs.org/sdr/DL72W980971.md): Panel · damaged · Apr 15, 1998 · N2811W · Boeing 727247 · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STABILIZER T/E LT SIDE HAS HOLE PUNCHED IN THE UPPER PANEL APPROX 10 INCHES INBD OF ELEVATOR POWERPACK CUTOUT. REMOVED DAMAGE WITH.375 DIA HOLE. DYE CHECKED, NO CRACKS FOUND. MANUFACTURED REPAIR PER SRM 55-10-3 FIG 3. INSTALLED REPAIR PER SRM 5
- [SDR DL72W980970](https://openairdocs.org/sdr/DL72W980970.md): Floorbeam · corroded · Apr 15, 1998 · N2811W · Boeing 727247 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED STA 344 BL 0. REMOVED CORROSION PER SRM 51-10-3. OUT OF LIMITS PER SRM 53-10-1 FIG 4. REMOVED ANGLE SUPPORTS, STARTED MANUFACTURING NEW SUPPORT. BEGAN REMOVAL OF T-CAP. COMPLETED REMOVAL OF T-CAP. DRILLED UP NEW T-CAP, EXCEPT TOP OF S
- [SDR DL72W980973](https://openairdocs.org/sdr/DL72W980973.md): Bracket · cracked · Apr 14, 1998 · N2811W · Boeing 727247 · Leading Edge Slat Actuator
  > BRACKET CRACKED NR 1 KRUEGER ACTUATOR SUPPORT BRACKET AT I/B LOWER CORNER. REMOVED FASTENERS TO FACILITATE DOUBLER AND STOP DRILLED CRACK PER M/M 57-20-21 PG 811. FABRICATED DOUBLER PER M/M 57-20-21 PG 811. INSTALLED DOUBLER PER MM 57-20-21 FIG 807.
- [SDR DL72W972353](https://openairdocs.org/sdr/DL72W972353.md): Skin · corroded · Nov 12, 1997 · N2811W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN LAP SPLICE AT STR 26L WAS FOUND WITH SEVERAL AREAS OF CORROSION AND SEVERAL EXISTING SRM REPAIRS. THE SECTION OF SKIN BETWEEN STA 480 TO 680 AND S24L TO 27L WAS REMOVED AND A NEW SECTION OF SKIN SPLICED IN PER ER/A 363125-14, REV B.
- [SDR DL72W972106](https://openairdocs.org/sdr/DL72W972106.md): Skin · cracked · Oct 4, 1997 · N2811W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING VISUAL INSPECTION, TPA MTC FOUND THREE CRACKS EMANATING FROM THE LAP JOINT BOLT HOLES. THESE CRACKS ARE.125,.25 AND.25 IN LENGTH. ALL CRACKS ARE CONFINED TO STA 594, STR 26L. THE REPAIR WILL CONSIST OF STANDARD SRM REPAIR PROCEDURES PER SRM 53-30-
- [SDR DL72W971970](https://openairdocs.org/sdr/DL72W971970.md): Stringer · cracked · Oct 3, 1997 · N2811W · Boeing 727247 · Vertical Stabilizer
  > VERT STAB STR 9L IS CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.
- [SDR DL72W971969](https://openairdocs.org/sdr/DL72W971969.md): Skin · cracked · Oct 3, 1997 · N2811W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND DURING D2 LETTER CHECK,.5 INCH CRACK RT ELEVATOR LOWER SKIN FWD OF ACCESS PANEL 9414. REPAIRED PER SRM 55-20-3.
- [SDR DL72W971968](https://openairdocs.org/sdr/DL72W971968.md): Stringer · cracked · Oct 3, 1997 · N2811W · Boeing 727247 · Vertical Stabilizer
  > FOUND DURING D2 LETTER CHECK, VERT STAB STR 9L CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.
- [SDR DL72W971212](https://openairdocs.org/sdr/DL72W971212.md): Batteries · discharged · Jun 22, 1997 · N2811W · Boeing 727247 · Emergency Lighting
  > AFT EMERG EXIT LIGHT IN AIRSTAIR WILL NOT TEST. REPLACED BATTERIES, OPN CKS OK.
- [SDR DL72W961459](https://openairdocs.org/sdr/DL72W961459.md): Skin · cracked · Jun 2, 1996 · N2811W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE SKIN JUST BELOW FWD LAV SERVICE PANEL WAS FOUND CRACKED. THE SKIN IS MADE FROM 0.040 2024-T3 AND THE_FINAL CUTOUT DIMENSIONS WERE 1.375 FWD/AFT AND 2.5 ABOVE/BELOW. THIS ERA GIVES INSTRUCTIONS TO REPAIR THE DAMAGE WITH A 0.050 2024-T3 DOUBLER.
- [SDR DL72W961314](https://openairdocs.org/sdr/DL72W961314.md): Relay · failed · May 29, 1996 · N2811W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT GO OUT AFTER TEST. REPLACED R-70 RELAY AND SYSTEM TEST CHECKED NORMAL (P/N 244201154) (MFG 10-60450-3). EVENT OCCURED ON THE GROUND AFTER FLT 1739 ARRIVED FROM TUS\AND THE CREW NOTICED THAT THE EXIT LIGHTS WERE ON AFTER TESTING
- [SDR DL72W961020](https://openairdocs.org/sdr/DL72W961020.md): Blkhd Web · cracked · Apr 15, 1996 · N2811W · Boeing 727247 · Fuselage Main, Bulkhead
  > THE STA 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS. THE DAMAGE WAS TRIMMED OUT WITH DIMENSIONS OF 2.6250 INCH AT LBL 8, WL 190 AND 8 INCH BY 3.1250 INCH AT LBL 14, WL 173. THE BULKHEAD WEB IS MANUFACTURED FROM 0.050 INCH CLAD 2024-T3. THIS ER/A AU
- [SDR DL72W960938](https://openairdocs.org/sdr/DL72W960938.md): Floor Beam · corroded · Apr 12, 1996 · N2811W · Boeing 727247 · Fuselage Main, Floor Beam
  > FOUND ON MV1 CHECK - CORROSION ON FLOOR BEAM TOP SURFACE STA 1050 FROM RBL 10 TO 14. REPAIR - REPAIRED PER M/M 53-20-11.
- [SDR DL72W960535](https://openairdocs.org/sdr/DL72W960535.md): Light · inoperative · Mar 9, 1996 · N2811W · Boeing 727247 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. OPS CHECKS GOOD.
- [SDR DL72W960092](https://openairdocs.org/sdr/DL72W960092.md): Angle · cracked · Jan 15, 1996 · N2811W · Boeing 727247 · Leading Edge Devices
  > DURING C-1 LETTER CHECK, FOUND.5 INCH CRACK AT NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.
- [SDR DL72W953401](https://openairdocs.org/sdr/DL72W953401.md): Sensor · failed · Aug 15, 1995 · N2811W · Boeing 727247 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO RETRACT ALL HYD SYS NML - REPLACED FAULTY M831 SENSOR AND DAMAGED WIRES AT SAME SENSOR. OPERATION NORMAL.
- [SDR DL72W952513](https://openairdocs.org/sdr/DL72W952513.md): Skin · cracked · Jun 8, 1995 · N2811W · Boeing 727247 · Trailing Edge Flaps
  > .3750 INCH CRACK, NR 3 AFT FLAP UPPER SURFACE AFT OF 2ND FROM O/B LOWER ROLLER TRACK CUTOUT. FOUND AT B-2 LTR CK. REPAIRED PER SRM 57-50-4.
- [SDR DL72W952512](https://openairdocs.org/sdr/DL72W952512.md): Web · cracked · Jun 8, 1995 · N2811W · Boeing 727247 · Leading Edge Devices
  > NR 6 SLAT O/B ACT ROD END WEB CRACKED AFT SIDE. FOUND AT B-2 LTR CK. REPAIRED PER SRM 57-54-0.
- [SDR DL72W952511](https://openairdocs.org/sdr/DL72W952511.md): Angle · cracked · Jun 8, 1995 · N2811W · Boeing 727247 · Leading Edge Devices
  > NR 2 SLAT I/B STOP PAD LWR ATTACH ANGLE IS CRACKED. FOUND AT B-2 LTR CK. 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 = 'N2811W' AND deregistration_id = 'N2811W-2000-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2811W-2000-02-01/reports

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