# Service difficulty reports: N831WA, cancelled Jan 29, 2004

A list on [N831WA, cancelled Jan 29, 2004](https://openairdocs.org/deregistered/N831WA-2004-01-29.md).

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

Page 1 of 2 · 82 reports

- [SDR DL72E011877](https://openairdocs.org/sdr/DL72E011877.md): Battery · discharged · Nov 28, 2001 · N831WA · Boeing 727247 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT 29 ABC INOP - REPLACED BATTERY
- [SDR DL72E011725](https://openairdocs.org/sdr/DL72E011725.md): Battery · discharged · Oct 26, 2001 · N831WA · Boeing 727247 · Emergency Lighting
  > R-2 EMERGENCY EXIT LIGHT INOP FOUND ON L/O. REPLACED BATTERIES
- [SDR DL72E011268](https://openairdocs.org/sdr/DL72E011268.md): Sign · inoperative · Jul 31, 2001 · N831WA · Boeing 727247 · Emergency Lighting
  > L1 EXIT SIGN INOP IN EMERG MODE. REPLACED L1 EMER LIGHT ASSY.
- [SDR DL72E010468](https://openairdocs.org/sdr/DL72E010468.md): Actuator · leaking · Mar 22, 2001 · N831WA · Boeing 727247 · Trailing Edge Flap Control System
  > DURING APPROACH LOST A SYSTEM HYD PRESS. MANUALLY EXTENDED GEAR. FOUND FLAP HYD MOTOR LEAKING FLUID. REPLACED FLAP HYD MOTOR, AND CASE DRAIN CHECK VALVE PER MM. INSPECTED CASE DRAIN FILTERS, NO METAL FOUND. PERFORMED ENG RUN, OPS CHECKS NORMAL.
- [SDR DL72E010114](https://openairdocs.org/sdr/DL72E010114.md): Access Panel · cracked · Jan 22, 2001 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND ON B2 LETTER CK 1 INCH CRACK AT INNER ACCESS PANEL BEAD ON PANEL 9216. REPAIRED PER SRM 55-20-3.
- [SDR DL72E010113](https://openairdocs.org/sdr/DL72E010113.md): Skin · cracked · Jan 22, 2001 · N831WA · Boeing 727247 · Vertical Stabilizer, Spar/Rib
  > FOUND ON B2 LETTER CK,.25 INCH CRACK AND SHEARED RIVET AT BASE OF VERTICAL STAB AT STR 7 LT SIDE. REPLACED FASTENER AND REPAIRED PER B727DRD 55-30-3D.
- [SDR DL72E010112](https://openairdocs.org/sdr/DL72E010112.md): Skin · cracked · Jan 22, 2001 · N831WA · Boeing 727247 · Elevator, Plate/Skin
  > FOUND ON B2 LETTER CK 1 INCH AND.375 INCH CRACK TOGETHER AT LOWER SKIN LT ELEVATOR JUST AFT AND O/B OF ACCESS PNL 9311. REPAIRED PER SRM 55-20-3.
- [SDR DL72E010057](https://openairdocs.org/sdr/DL72E010057.md): Radome · bird strike · Jan 11, 2001 · N831WA · Boeing 727247 · Aerodynamic Fairings
  > BIRD STRIKE ON T/O IN BWI. AIRSPEED INDICATORS DIFFER AT FL 240. ENGINE PARAMETERS NORMAL. REPLACED RADOME PER MM. ALSO, CLEARED DEBRIS FROM CO-PILOTS PITOT TUBE. TESTED PITOT SYSTEM IAW M/M. NO SPLITS NOTED.
- [SDR DL72E001270](https://openairdocs.org/sdr/DL72E001270.md): Battery Pack · inoperative · Jul 5, 2000 · N831WA · Boeing 727247 · Emergency Lighting
  > LT AFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK GOOD.
- [SDR DL72E001261](https://openairdocs.org/sdr/DL72E001261.md): Warning System · false activation · Jul 4, 2000 · N831WA · Boeing 727247 · Fire Detection
  > TEN MINS PRIOR ARRIVAL LEX, HAD NR 2 ENG FIRE WARN. NR 2 ENG F/W A LOOP ON MCO. SHUTDOWN ENG PER POM. FIRED BOTH BOTTLES. LIGHT DID NOT GO OUT. LIGHT WENT OUT 2 MINS PRIOR LANDING. DECLARED EMERGENCY, NO FIRE CONFIRMED BY GROUND EQUIP. REPLACED FWD AND
- [SDR DL72E001096](https://openairdocs.org/sdr/DL72E001096.md): Control Valve · malfunctioned · Jun 5, 2000 · N831WA · Boeing 727247 · Cabin Cooling System
  > SIDEWALL AT SEAT 19 FELT WARM WITH SMELL. S/O BALANCE PACK SUPPLY BY USING ZONE TEMP CONTROL VLV. MOVED VLV TO WARMER POSITION, TRIED TO GET VLV BACK TO COOLER POSITION AND OVHEAT LIGHT ILLUMINATED. CREW UNSURE WHAT THEY HAD AND TALKED ABOUT DIVERTING WHILE
- [SDR DL72E000198](https://openairdocs.org/sdr/DL72E000198.md): Skin · bent · Jan 1, 2000 · N831WA · Boeing 727247 · Trailing Edge Flaps
  > I/B END, UPPER SKIN BENT. REPAIRED PER MM 57-52-0 FIG 803.
- [SDR DL72E992693](https://openairdocs.org/sdr/DL72E992693.md): Sensor · failed · Dec 9, 1999 · N831WA · Boeing 727247 · Cabin Pressure Indicator
  > DURING CRUISE AT FL 290, A PASSENGER NOTICED THE AREA APPROXIMATELY 10 INCHES BELOW THE WINDOWS AT SEATS 16E & 17E WAS HOT TO THE TOUCH AND A SLIGHT BURNING ODOR WAS PRESENT. AFTER RT PACK TURNED OFF AND DESCENDED TO FL240, THE AREA COOLED IMMEDIATELY AND ODO
- [SDR DL72E992645](https://openairdocs.org/sdr/DL72E992645.md): Actuator · failed · Dec 4, 1999 · N831WA · Boeing 727247 · Trailing Edge Flap Actuator
  > AFTER TAKEOFF, NR 7 SLAT WOULD NOT RETRACT UNTIL BACK ON GROUND. REPLACED NR 7 SLAT ACTUATOR AND EXTEND SWITCH, CHECKS OK.
- [SDR DL72E992573](https://openairdocs.org/sdr/DL72E992573.md): Skin · cracked · Nov 22, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > A 1.5 CRACK WAS FOUND IN THE L1 DOOR SURROUND STRAP. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333818-14.
- [SDR DL72E992572](https://openairdocs.org/sdr/DL72E992572.md): Skin · cracked · Nov 22, 1999 · N831WA · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > A CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN, LEFT HAND SIDE, WHERE THE SKIN MEETS THE UPPER TORQUE BOX AT APPROX FS 1210. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333807-14.
- [SDR DL72E992570](https://openairdocs.org/sdr/DL72E992570.md): Skin · cracked · Nov 22, 1999 · N831WA · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > THE SKIN OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FUSELAGE CREASE LINE AND STRINGER 10L. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333830-14AD.
- [SDR DL72E992496](https://openairdocs.org/sdr/DL72E992496.md): Web · cracked · Nov 11, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > FWD WEB CRACKED INSIDE NR 3 L/E SLAT AT ANTI-ICE DUCT. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS PER M/M 57-40-0 FIG 802 A. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-40-0 FIG 802 A.
- [SDR DL72E992478](https://openairdocs.org/sdr/DL72E992478.md): Skin · cracked · Nov 10, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN LAP WAS FOUND CRACKED AT STRINGER 4R BETWEEN FS 540 AND FS 560. THE DAMAGE WAS REPIARED PER ERA 333763-14 DURING HMV.
- [SDR DL72E992465](https://openairdocs.org/sdr/DL72E992465.md): Rib · cracked · Nov 8, 1999 · N831WA · Boeing 727247 · Wing, Rib/Bulkhead
  > ACTUATOR RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.
- [SDR DL72E992461](https://openairdocs.org/sdr/DL72E992461.md): Skin · cracked · Nov 8, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4R LAP JOINT BETWEEN FS 620 AND 640. THE DISCREPANCY WAS REPAIRED BY ER/A 333765-14 AT HMV.
- [SDR DL72E992459](https://openairdocs.org/sdr/DL72E992459.md): Skin · cracked · Nov 8, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE STRINGER 4L LAP JOINT BETWEEN FS 1030 AND 1050 DURING INSPECTIONS PER AD 99-04-22. ERA 333766-14 REPAIRED THE DAMAGE AT HMV.
- [SDR DL72E992521](https://openairdocs.org/sdr/DL72E992521.md): Attach Bolt · cracks · Nov 5, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND NR 5 L/E SLAT 2 CRACKS AT FENCE ATTACH BOLT HOLES AT L/E. MFR REPAIR DOUBLER PER MM 57-54-0 FIG 813, REPAIRED PER SAME.
- [SDR DL72E992837](https://openairdocs.org/sdr/DL72E992837.md): Skin · worn · Nov 3, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, THE LOWER L/E SKIN WAS FOUND WORN APPROX 1 INCH LENGTH AT THE O/B END OF THE FLAP. THE L/E WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 803.
- [SDR DL72E992460](https://openairdocs.org/sdr/DL72E992460.md): Blkhd Stiffener · cracked · Nov 3, 1999 · N831WA · Boeing 727247 · Fuselage Main, Bulkhead
  > THE LBL 36.83 VERTICAL STIFFENER OF THE 1183 BULKHEAD WAS FOUND CRACKED AT HMV. ERA 333764-14 REPAIRED THIS CONDITION.
- [SDR DL72E992524](https://openairdocs.org/sdr/DL72E992524.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND DOUBLER CRACKED ON RIB LOC I/B SIDE OF ACTUATOR FITTING ON NR 3 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0. FABRICATED DOUBLER, FOUND SECOND RIB CRACK, DRILLED SECOND RIB, FABRICATED ANOTHER DOUBLER, CUT AND REMOVED RIBS. INSTALLED DOUBLERS
- [SDR DL72E992485](https://openairdocs.org/sdr/DL72E992485.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2 FOUND NR 3 L/E SLAT, RIB CRACKED I/B SIDE OF I/B TRACK. REMOVED FASTENERS, STOPPED DRILLED CRACK. FABRICATED DOUBLER PER MM 54-57-0 FIG 811. INSTALLED DOUBLER PER SAME.
- [SDR DL72E992484](https://openairdocs.org/sdr/DL72E992484.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND RIB CRACKED INSIDE NR 3 L/E SLAT ON O/B SIDE OF I/B TRACK. TRIMMED OUT DAMAGE, AND REPAIR ANGLE PER MM 57-54-0 FIG 811. INSTALLED DOUBLER PER SAME.
- [SDR DL72E992483](https://openairdocs.org/sdr/DL72E992483.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND RIB CRACKED ON O/B SIDE OF ACT FITTING ON NR 2 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0 FIG 804. FABRICATED DOUBLER PER SAME, INSTALLED.
- [SDR DL72E992482](https://openairdocs.org/sdr/DL72E992482.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND NR 2 L/E SLAT, RIB TEMP REPAIR STOP DRILLED CRACK, I/B SIDE OF ACT FITTING. STOP DRILLED CRACK PER MM 57-54-0 FIG 804, FAB'D DOUBLER PER SAME, INSTALLED.
- [SDR DL72E992481](https://openairdocs.org/sdr/DL72E992481.md): Rib · cracked · Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND NR 2 L/E SLAT, RIB CRACKED I/B SIDE OF ACT FITTING. STOPPED DRILLED CRACK PER MM 57-54-0 FIG 804. FAB'D DOUBLER PER SAME, AND INSTALLED.
- [SDR DL72E991379](https://openairdocs.org/sdr/DL72E991379.md): Bracket · cracked · Jun 17, 1999 · N831WA · Boeing 727247 · Leading Edge Devices
  > FOUND ON A1 LETTER CK, NR 8 SLAT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72E991366](https://openairdocs.org/sdr/DL72E991366.md): Line · leaking · Jun 16, 1999 · N831WA · Boeing 727247 · Hydraulic System, Main
  > ON TAKEOFF IMMEDIATELY AFTER SELECTING FLAPS TO 2 DEGREES FROM 5 DEGREES, EXPERIENCED A SYSTEM HYDRAULIC LOSS QTY AND PRESSURE DECREASED RAPIDLY TO 0. SYSTEM B NORMAL THROUGHOUT. MAINTENANCE FOUND ACTUATOR LINE IN NLG WHEELWELL LEAKING. REPLACED LINE, SERVI
- [SDR DL72E991292](https://openairdocs.org/sdr/DL72E991292.md): Skin · cracked · Jun 6, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > 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 PANEL. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT AND AN EXTERNAL
- [SDR DL72E990733](https://openairdocs.org/sdr/DL72E990733.md): Battery Pack · discharged · Apr 3, 1999 · N831WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SIGN OVER RT OVERWING EXIT INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK.
- [SDR DL72E982337](https://openairdocs.org/sdr/DL72E982337.md): Angle · cracked · Nov 12, 1998 · N831WA · Boeing 727247 · Leading Edge Devices
  > NR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PG 816.
- [SDR DL72E982336](https://openairdocs.org/sdr/DL72E982336.md): Chord · cracked · Nov 12, 1998 · N831WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON F2 LETTER CK, 1 INCH CRACK IN STA 1342 CHORD ABOVE THE NUMBER 2 ENGINE S-DUCT. STOP DRILLED CRACK PER MM 53-11-0.
- [SDR DL72E980874](https://openairdocs.org/sdr/DL72E980874.md): Skin · cracked · Apr 22, 1998 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND F1 LETTER CHECK, FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED APPROX.25 IN. REPAIR PER M/M 53-30-03.
- [SDR DL72E980871](https://openairdocs.org/sdr/DL72E980871.md): Bracket · cracked · Apr 22, 1998 · N831WA · Boeing 727247 · Leading Edge Devices
  > FOUND ON F1 LETTER CHK, NR 1 SLAT ACT IB MOUNT BRACKET CRACKED AT WEB. REPAIR PER M/M 57-20-21.
- [SDR DL72E980086](https://openairdocs.org/sdr/DL72E980086.md): Light · inoperative · Jan 13, 1998 · N831WA · Boeing 727247 · Emergency Lighting
  > FA AFT FLASHLIGHT INOP. REPLACED BATTERY, OPN NML.
- [SDR DL72E972524](https://openairdocs.org/sdr/DL72E972524.md): Battery · discharged · Dec 2, 1997 · N831WA · Boeing 727247 · Emergency Lighting
  > AFT CARGO DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK, ALL CKS NORMAL.
- [SDR DL72E972331](https://openairdocs.org/sdr/DL72E972331.md): Stringer · cracked · Oct 27, 1997 · N831WA · Boeing 727247 · Vertical Stabilizer
  > STRINGER CRACKED VERT STAB INTERIOR STRINGER 1R AT RIB NR 4. STOP DRILLED CRACKS PER M/M 55-30-0 FIG 803. FABRICATED REP AIR PER M/M 55-30-0 PG 803 FIG 803. OK TO INSTALL. INSTALLED REPAIR PER M/M 55-30-0 PG 803 FIG 803.
- [SDR DL72E971881](https://openairdocs.org/sdr/DL72E971881.md): Skin · corrosion · Sep 12, 1997 · N831WA · Boeing 727247 · Wing, Plate/Skin
  > DURING INSPECTION OF THE LOWER WIND SKIN PER EO 4-37113-3, CORROSION WAS FOUND ON THE SKIN AT APPROX FS 825 AND LBL 32.2. THE DAMAGE CUTOUT MEASURED 7.5 (IB/OB) BY 6.125 (FORE/AFT). REPAIRED PER ERA 330730-14AD.
- [SDR DL72E971878](https://openairdocs.org/sdr/DL72E971878.md): Blkhd Stiffener · cracked · Sep 10, 1997 · N831WA · Boeing 727247 · Fuselage Main, Bulkhead
  > AN EXISTING REPAIR WAS FOUND ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THIS REPAIR WAS REMOVED AND A 2.5 CRACK WAS DISCOVERED IN THE IB FLANGE-TO-WEB RADIUS. S/B 727-53-0175 WHICH IS REQUIRED BY AD 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND
- [SDR DL72E970362](https://openairdocs.org/sdr/DL72E970362.md): Battery Pack · discharged · Feb 26, 1997 · N831WA · Boeing 727247 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK M983.
- [SDR DL72E961567](https://openairdocs.org/sdr/DL72E961567.md): Skin · cracked · Jul 1, 1996 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND ON D2 LETTER CK,.4687 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER MM 53-30-0.
- [SDR DL72E961566](https://openairdocs.org/sdr/DL72E961566.md): Skin · cracked · Jul 1, 1996 · N831WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND ON D2 LETTER CK, AFT AIRSTAIR DOOR CUTOUT RT FWD RADIUS CRACKED. REPAIRED PER MM 53-30-0.
- [SDR DL72E960868](https://openairdocs.org/sdr/DL72E960868.md): Wire · broken · Apr 15, 1996 · N831WA · Boeing 727247 · Light System Wiring
  > EMERGENCY TRACK LIGHTS INOP FROM 20ABC TO 27ABC. FOUND WIRES BROKEN AT 20ABC AND 27ABC. REPAIRED SAME, EMERGENCY TRACK LIGHTING SYSTEM OPS CHECKS GOOD.
- [SDR DL72E960549](https://openairdocs.org/sdr/DL72E960549.md): Fitting · pitted · Feb 27, 1996 · N831WA · Boeing 727247 · Wing, Control Surface Attach Fittings
  > LT MLG NR 4 FLAP TRACK PORKCHOP FITTING HAS PITTED BUSHING. FORWARD HOLE BORED TO 1.7068 INCH PER MM 57-42-0, PAGE 814.MPI PER PS 900-6-2, NR 01. OK. TURNED O/D OF BUSHING BRUSH CAD FITTING IN STRIKE CAD PLATE BUSHING, PAINTED FITTING PER MM 57-42-0. INSTA
- [SDR DL72E960285](https://openairdocs.org/sdr/DL72E960285.md): Power Supply · inoperative · Feb 5, 1996 · N831WA · Boeing 727247 · Emergency Lighting
  > ON PREFLIGHT, EMERGENCY TRACK LIGHTS INOP IN FWD CABIN. REPLACED POWER SUPPLY, OPS NORMAL.

Next page: https://openairdocs.org/deregistered/N831WA-2004-01-29/reports.md?page=2

## 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 = 'N831WA' AND deregistration_id = 'N831WA-2004-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N831WA-2004-01-29/reports

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