# Service difficulty reports: N2829W, cancelled Jul 20, 2010

A list on [N2829W, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N2829W-2010-07-20.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 · 61 reports

- [SDR DL72E021155](https://openairdocs.org/sdr/DL72E021155.md): Battery Pack · discharged · Sep 30, 2002 · N2829W · Boeing 727247 · Emergency Lighting
  > AFT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK AND PACK.
- [SDR DL72E020548](https://openairdocs.org/sdr/DL72E020548.md): Battery · discharged · May 14, 2002 · N2829W · Boeing 727247 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. FOUND BATTERY DEFECTIVE IN LIGHT ASSY. REPLACED BATTERY ASSY.
- [SDR DL72E020366](https://openairdocs.org/sdr/DL72E020366.md): Battery Pack · discharged · Mar 23, 2002 · N2829W · Boeing 727247 · Emergency Lighting
  > AFT EMERGENCY EXIT SIGN INOP. REPLACED BATTERY RACK AND LIGHT ASSY.
- [SDR DL72E020269](https://openairdocs.org/sdr/DL72E020269.md): Mount · cracked · Mar 5, 2002 · N2829W · Boeing 727247 · Engine Mount Section
  > DURING INSPECTIONS OF THE FORWARD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICATION WAS NOTED IN HOLE C AS REFERENCED IN BAC S/B 727-54A0010. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITIONAL INSURANCE CUT.
- [SDR DL72E011957](https://openairdocs.org/sdr/DL72E011957.md): Clamp · broken · Dec 14, 2001 · N2829W · Boeing 727247 · Pneumatic Distribution System
  > A/C PERFORMED AIR TURNBACK DUE TO AFT CARGO DETECTION OVERHEAT/FIRE. REPLACED BROKEN CLAMP ON PNEUMATIC DUCT IN AFT BAG BIN.
- [SDR DL72E011779](https://openairdocs.org/sdr/DL72E011779.md): Bulkhead · cracked · Nov 8, 2001 · N2829W · Boeing 727247 · Fuselage Main, Bulkhead
  > FUSELAGE BULKHEAD STA 1183 RBL 8, A 3/8 INCH CRACK WAS FOUND IN THE FS 1183 BULKHEAD WEB UNDER THE LOWER END OF THE RBL VERTICAL STIFFENER NEAR WL 182. THE CRACK IS TYPICAL OF BAC S/B 727-53-0175. THE CRACK WAS REMOVED AND REPAIR INSTALLED PER ER/A 382099-14.
- [SDR DL72E011771](https://openairdocs.org/sdr/DL72E011771.md): Attach Angle · cracked · Nov 7, 2001 · N2829W · Boeing 727247 · Leading Edge Devices
  > FOUND ON F1 CK NR 8 SLAT INBD STOP ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-000-8.
- [SDR DL72E010491](https://openairdocs.org/sdr/DL72E010491.md): Battery Pack · discharged · Mar 25, 2001 · N2829W · Boeing 727247 · Emergency Lighting
  > RT OVERWING EMERGENCY EVAC LIGHT INOP. REPLACED BATT PACK OPS NML.
- [SDR DL72E002232](https://openairdocs.org/sdr/DL72E002232.md): Engine · malfunctioned · Nov 15, 2000 · N2829W · Boeing 727247 · Engine (Turbine/Turboprop)
  > NUMBER ONE ENG EPR ERRATIC AROUND 1.8. RAN ENGINES. UNABLE TO DUPLICATE. INSPECTED SYSTEM - NTF.
- [SDR DL72E001778](https://openairdocs.org/sdr/DL72E001778.md): Stiffener · cracked · Sep 14, 2000 · N2829W · Boeing 727247 · Leading Edge Devices
  > L/E SPAR STIFFENER CRACKED AT NR 2 SLAT O/B TRACK O/B SIDE. TPA E-1 LETTER CHECK. REPLACED STIFFENER PER M/M 57-20-21 NR 14.
- [SDR DL72E001239](https://openairdocs.org/sdr/DL72E001239.md): Bulkhead · cracked · Jun 29, 2000 · N2829W · Boeing 727247 · Fuselage Main, Bulkhead
  > THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL.75 INCH LONG CRACK AT RBL 30 AND WL 169. THE CRACK IS TYPICAL OF BAC S/B 727-53-0215. THE CRACK WAS CUTOUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER S/B AND ER/A 377664-14
- [SDR DL72E000972](https://openairdocs.org/sdr/DL72E000972.md): Light · inoperative · May 16, 2000 · N2829W · Boeing 727247 · Passenger Compartment Lighting
  > EMERGENCY LIGHT ABOVE R1 DOOR WOULD NOT ILLUMINATE WHEN OPERATED BY COCKPIT SWITCH. RELAMPED, NO HELP. REPLACED LIGHT ASSY, CKS OK.
- [SDR DL72E991961](https://openairdocs.org/sdr/DL72E991961.md): Charger · inop · Sep 4, 1999 · N2829W · Boeing 727247 · Lighting System
  > DURING L/O CK, FOUND EXTERIOR OVERWING EXIT AFT EMERGENCY LIGHT INOP ON LEFT SIDE. REPLACED CHARGER ASSY. OPS CKS GOOD.
- [SDR DL72E990723](https://openairdocs.org/sdr/DL72E990723.md): Battery · discharged · Apr 1, 1999 · N2829W · Boeing 727247 · Emergency Lighting
  > CENTER LT OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT M954, OPS CHKS GOOD.
- [SDR DL72E990536](https://openairdocs.org/sdr/DL72E990536.md): Battery · shorted · Mar 12, 1999 · N2829W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ILLUMINATE WHEN ARMED SEAT 1 TO 26. FOUND LIGHTS ILLUM INTERMITTENTLY. ISOLATED PROBLEM TO RT CONTROL SYSTEM, FOUND POWER AT PIN 4 AT FWD BATTERY PACK. INSPECTED WIRE BUNDLE IN CEILING, AT ALL BATTERY PACKS. FOUND AFT AIRSTAIR LIGHT A
- [SDR DL72E990513](https://openairdocs.org/sdr/DL72E990513.md): Power Supply · inoperative · Mar 11, 1999 · N2829W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT, CHECKED COCKPIT SWITCH. REPLACED AFT EMERGENCY LIGHTS POWER SUPPLY.
- [SDR DL72E990502](https://openairdocs.org/sdr/DL72E990502.md): Power Supply · inop · Mar 10, 1999 · N2829W · Boeing 727247 · Emergency Lighting
  > ALL EMER LIGHTS TURN ON AND OFF WITHOUT CONTROL SWITCH TURNED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY.
- [SDR DL72E990499](https://openairdocs.org/sdr/DL72E990499.md): Power Supply · inop · Mar 10, 1999 · N2829W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED F/C EMER LIGHT POWER SUPPLY AND BATTERY TEST OK.
- [SDR DL72E982643](https://openairdocs.org/sdr/DL72E982643.md): Battery Pack · discharged · Dec 28, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > EMERG EXIT LIGHT SIGN ON FACE OF LIFE RAFT COMPARTMENT, MAIN CABIN INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK.
- [SDR DL72E982492](https://openairdocs.org/sdr/DL72E982492.md): Web · cracked · Dec 3, 1998 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > REF SHIP 576 TPA LTR CHK C2 12-03-98,.25 INCH CRACK IN TORQUE BOX VERT WEB RT SIDE STA 1243,.5 INCH CRACK IN TORQUE BOX VERT WEB LT SIDE STA 1323. REPAIRED BOTH ITEMS PER MM 53-11-0.
- [SDR DL72E982394](https://openairdocs.org/sdr/DL72E982394.md): Battery Pack · discharged · Nov 18, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > LT CTR OVERWING EMER LIGHT INOP. REPLACED BULB AND BATT PACK, NO HELP. REPLACED CHARGING RACK, CKS OK.
- [SDR DL72E981740](https://openairdocs.org/sdr/DL72E981740.md): Rack · inoperative · Aug 23, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHT INOP. REPLACED RACK.
- [SDR DL72E981103](https://openairdocs.org/sdr/DL72E981103.md): Battery Pack · discharged · May 22, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > LT WING CTR EMER EXIT LIGHT INOP. REPLACED RACK AND BATTERY M956.
- [SDR DL72E980980](https://openairdocs.org/sdr/DL72E980980.md): Bracket · cracked · May 8, 1998 · N2829W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED 1.5 INCH VISIBLE O/B END. REPAIRED PER M/M 57-20-21.
- [SDR DL72E980979](https://openairdocs.org/sdr/DL72E980979.md): Skin · cracked · May 8, 1998 · N2829W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND ON C1 LETTER CK, TWO.75 INCH CRACKS IN THE RT ELEVATOR LOWER SKIN LOWER FWD EDGE OF ELEVATOR. REPAIRED PER SRM 55-20-3.
- [SDR DL72E980570](https://openairdocs.org/sdr/DL72E980570.md): Connector · loose · Mar 13, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > ON LAYOVER CK, FOUND 2 AFT LEFT OVERWING EMERG EXIT LIGHTS INOP. FOUND CONNECTOR PLUG OFF OF BATTERY PACK FOR AFT O/W BATTERY PACK. REINSTALLED CONNECTOR CHECKS GOOD. REPLACED BATTERY FOR MIDDLE O/W EXIT LIGHT, NO HELP. REPLACED BATTERY PACK, OPS CKS GOOD.
- [SDR DL72E980188](https://openairdocs.org/sdr/DL72E980188.md): Battery Pack · discharged · Jan 21, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72E980187](https://openairdocs.org/sdr/DL72E980187.md): Battery Pack · discharged · Jan 21, 1998 · N2829W · Boeing 727247 · Emergency Lighting
  > RIGHT FORWARD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72E972030](https://openairdocs.org/sdr/DL72E972030.md): Sill · corroded · Oct 8, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > C2 DOOR SILL WAS FOUND CORRODED ON THE OUTBD FLANGE. CORROSION CONFINED TO THE UPPER SURFACE OF OUTBD FLANGE. CUT OUT IN FLANGE IS 6.125 BY 1.625. REPAIRED PER ERA 330801-14.
- [SDR DL72E972035](https://openairdocs.org/sdr/DL72E972035.md): Sill · corroded · Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > C2 DOOR SILL WAS FOUND CORRODED AT THE OUTBD CHORD AT FS 980. REPAIRED PER ERA 330800-14.
- [SDR DL72E972034](https://openairdocs.org/sdr/DL72E972034.md): Skin · corroded · Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BUTT SPLICE AND STRINGER WERE FOUND CORRODED AT S29R AND FS 1010. REPAIRED PER ERA 330802-14.
- [SDR DL72E972032](https://openairdocs.org/sdr/DL72E972032.md): Frame · cracked · Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > WHILE ACCOMPLISHING EO 4-61247-12AD, A 0.75 CRACK WAS FOUND IN THE WEB OF THE NR 2 CARGO DOORWAY AFT FRAME. REPAIRED PER ERA 330827-14AD.
- [SDR DL72E971950](https://openairdocs.org/sdr/DL72E971950.md): Frame · cracked · Sep 14, 1997 · N2829W · Boeing 727247 · Fuselage Main, Frame
  > FUSELAGE FRAME CRACKED AT STA 930 STR 13 AND 14 LT SIDE. REPAIRED PER M/M 53-10-4 FIG 25 AND ERA 330775-14.
- [SDR DL72E971855](https://openairdocs.org/sdr/DL72E971855.md): Rib · cracked · Sep 14, 1997 · N2829W · Boeing 727247 · Leading Edge Devices
  > RIB IS CRACKED AT ACTUATOR ATTACH HOLE I/B RIB. PLATE AT ATTACH HOLE IS WORN ON SAME RIB. SMALL LEG ON RIB IS MISSING THAT ATTACHES CHORD ANGLE. REPAIRED PER MM 57-54-00 PG 805 ITEM 2, REPLACED PLATE PER SRM 51-00.
- [SDR DL72E971854](https://openairdocs.org/sdr/DL72E971854.md): Rib · cracked · Sep 14, 1997 · N2829W · Boeing 727247 · Leading Edge Devices
  > RIB IS CRACKED AT NUT PLATE O/B RIB AT ACTUATOR ATTACH HOLE ON NR 4 SLAT. REPAIR DOUBLER IS CRACKED ON SAME RIB. REPAIRED PER MM 57-54-0 PG 805.
- [SDR DL72E972129](https://openairdocs.org/sdr/DL72E972129.md): Spar · cracked · Sep 11, 1997 · N2829W · Boeing 727247 · Trailing Edge Flaps
  > CRACK AFT SPAR 53 FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0.
- [SDR DL72E971644](https://openairdocs.org/sdr/DL72E971644.md): Act Bracket · cracked · Aug 21, 1997 · N2829W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 5 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED AT O/B UPPER CORNER. INSTALLED DOUBLER PER M/M 57-20-21.
- [SDR DL72E971643](https://openairdocs.org/sdr/DL72E971643.md): Act Bracket · cracked · Aug 21, 1997 · N2829W · Boeing 727247 · Leading Edge Slat Actuator
  > A 2 INCH CRACK AT NR 8 L/E SLAT ACTUATOR ATTACH BRACKET O/B SIDE. INSTALLED DOUBLER PER M/M 57-20-21.
- [SDR DL72E970215](https://openairdocs.org/sdr/DL72E970215.md): Stiffener · corrosion · Jan 18, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED AT THE LOWER END OF LBL 17.8 VERTICAL STIFFENER, JUST BELOW THE SUPPORT ROD END AT STA 1183. CORROSION IS ON THE O/B FACE OF THE VERTICAL WEB WHICH RUNS FWD-AFT. THIS DAMAGE HAS BEEN REPAIRED IN ACCORDANCE WITH S/B 727-53-0202.
- [SDR DL72E970087](https://openairdocs.org/sdr/DL72E970087.md): Web · cracked · Jan 17, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > LT TORQUE BOX VERTICAL WEB LIGHTENING HOLE CRACKED 2 PLACES AT STA 1235, MARKED. REPAIRED PER M/M 53-11-0 PG 828.
- [SDR DL72E970085](https://openairdocs.org/sdr/DL72E970085.md): Web · cracked · Jan 17, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > LT TORQUE BOX VERTICAL WEB LIGHTENING HOLE CRACKED 2 PLACES AT STA 1235. INSTALLED DOUBLER PER MM 53-11-0 PG 828.
- [SDR DL72E961629](https://openairdocs.org/sdr/DL72E961629.md): Skin · corrosion · Jul 9, 1996 · N2829W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR STR 28R. THE SKIN IS MANUFACTURED FROM CLAD 2024-T3 CHEM-MILLED WITH A LOCAL THICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DISCOVERED, STR 28R AT FS
- [SDR DL72E961269](https://openairdocs.org/sdr/DL72E961269.md): Angle · corroded · May 13, 1996 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > AT MID VISIT FASTENER HOLES WERE FOUND CORRODDED AT STA 400 RBL 33. CAP AND ANGLES REPLACED PER SRM 53-10-8.
- [SDR DL72E961226](https://openairdocs.org/sdr/DL72E961226.md): Skin · corrosion · May 13, 1996 · N2829W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR S-28R. THE SKIN IS 2024-T3 CLAD CHEM-MILLED SKIN WITH A LOCAL THICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. S-28R AT STATION 1050 HAS EX
- [SDR DL72E961143](https://openairdocs.org/sdr/DL72E961143.md): Stringer · corrosion · May 13, 1996 · N2829W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. STRINGER 28R AT STATION 1050 HAS EXTENSIVE CORROSION AND WILL REQUIRE INSTALLATION OF A SPLICE SECTION. ADDITIONAL CORROSION DAMAGE IS LOCATED APPROXIMATELY 2 INCHES INBOARD AN
- [SDR DL72E960583](https://openairdocs.org/sdr/DL72E960583.md): Fuel Contl Unit · failed · Mar 14, 1996 · N2829W · Boeing 727247 · Fuel Control/Turbine Engines
  > NR 1 ENGINE FLAMED-OUT AS TAKEOFF POWER WAS BEING APPLIED. C/A: REPLACED FCU AND FUEL PUMP. LEAK CHECKED AND RIGGED PER PFHB. OPS CKS OK.
- [SDR DL72E960086](https://openairdocs.org/sdr/DL72E960086.md): Rib · cracked · Jan 14, 1996 · N2829W · Boeing 727247 · Leading Edge Devices
  > SLAT NR 6, RIB NR 10 AND 12 CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.
- [SDR DL72E960064](https://openairdocs.org/sdr/DL72E960064.md): Rib · cracked · Nov 28, 1995 · N2829W · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH RIB NR 12 CRACKED PAST PREVIOUS STOP DRILL. REPAIRED PER MM 57-54-00.
- [SDR DL72E954489](https://openairdocs.org/sdr/DL72E954489.md): Pack Valve · malfunctioned · Nov 25, 1995 · N2829W · Boeing 727247 · Cabin Cooling System
  > ON CLIMBOUT, A/C WOULD NOT HOLD PRESSURIZATION. DESCENDED AND CABIN STILL CLIMBED, LT DUCT PRESS 20 LBS HIGHER THAN RT. CA REPLACED LT PAC VALVE, CLEANED TRASH FROM LWR AFT CORNER OF C2 BIN DOOR AND A/C PRESSURE CHECK OK.
- [SDR DL72E961586](https://openairdocs.org/sdr/DL72E961586.md): Beam · cracked · Nov 20, 1995 · N2829W · Boeing 727247 · Fuselage Miscellaneous Structure
  > THERE IS A 1 INCH CRACK IN THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273 AND A 3 INCH CRACK IN THE AFT SIDE GUSSET. THE INBD UPPER CHORD HAS A 4 INCH LONGITUDINAL CRACK. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07

Next page: https://openairdocs.org/deregistered/N2829W-2010-07-20/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 = 'N2829W' AND deregistration_id = 'N2829W-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2829W-2010-07-20/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.