# Service difficulty reports: N2819W

A list on [N2819W](https://openairdocs.org/aircraft/N2819W.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 · 68 reports

- [SDR DL72W020656](https://openairdocs.org/sdr/DL72W020656.md): Spar · cracked · Jun 13, 2002 · N2819W · Boeing 727247 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF TERMINATING ACTION ON NR 3 MIDFLAP REAR SPAR UPPER CHORD, CRACKED FASTENER HOLE WAS DISCOVERED. REPAIR PER ER/A 417400-14AD.
- [SDR DL72W011742](https://openairdocs.org/sdr/DL72W011742.md): Rack · faulty · Oct 31, 2001 · N2819W · Boeing 727247 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOP. FOUND BATTERY MOUNT RACK BAD. REPLACED BATTERY RACK AND BATTERY. CHECKS GOOD.
- [SDR DL72W011413](https://openairdocs.org/sdr/DL72W011413.md): Wire · damaged · Aug 26, 2001 · N2819W · Boeing 727247 · Light System Wiring
  > PAX SEATS 23, 24, 25, 26 EMERGENCY LIGHTS INOPERATIVE, REPAIRED PINCHED WIRING. ALL CHECKED OK.
- [SDR DL72W010402](https://openairdocs.org/sdr/DL72W010402.md): Frame · cracked · Mar 12, 2001 · N2819W · Boeing 727247 · Fuselage Main, Frame
  > CRACKS WERE FOUND IN TWO LOCATIONS OF THE FS 990 FRAME. ONEWAS AT STR 28R AND THE OTHER AT STR 29R. THE CRACKS WERE CUT OUT AND A DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72W010401](https://openairdocs.org/sdr/DL72W010401.md): Bulkhead · cracked · Mar 12, 2001 · N2819W · Boeing 727247 · Fuselage Main, Bulkhead
  > CRACKS WERE FOUND IN THE WEBS AND FAIL SAFE CHORDS OF THE FS294.5 BULKHEAD. CRACKS WERE EMANATING FROM FASTENER LOCATIONS AT WL 180 AND LBL 14. ONE WEB AND THE CHORDS WEREREPLACED AND ONE OF THE WEBS WAS SPLICED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72W010349](https://openairdocs.org/sdr/DL72W010349.md): Skin · cracked · Mar 1, 2001 · N2819W · Boeing 727247 · Passenger/Crew Doors
  > DURING MAINTENANCE VISIT, THE FWD ENTRY DOOR WAS FOUND CRACKED AROUND THE UPPER LATCH CUTOUT. REPAIR PER ER/A 401383-14.
- [SDR DL72W010331](https://openairdocs.org/sdr/DL72W010331.md): Stringer · cracked · Feb 26, 2001 · N2819W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 29R WAS FOUND CRACKED AT FS 950E AND 975. THE STRINGER WAS CUT AT FS 950D +10 AND REPLACED AFT TO THE MFG SPLICE LOCATION. THE DAMAGE WAS FOUND AT MV.
- [SDR DL72W010313](https://openairdocs.org/sdr/DL72W010313.md): Door Frame · misdrilled · Feb 22, 2001 · N2819W · Boeing 727247 · Fuselage Main, Structure
  > THE RT AFT ENTRY DOOR FRAME SPLICE INSTALLED PER S/B 727-53-0210 WAS FOUND TO HAVE SHORT EDGE DISTANCE. THE AREA WAS MODIFIED PER S/B AT HMV.
- [SDR DL72W010179](https://openairdocs.org/sdr/DL72W010179.md): Flap Track · corroded · Jan 31, 2001 · N2819W · Boeing 727247 · Trailing Edge Flaps
  > DURING OVERHAUL, THE NR 4 INBD FLAP TRACK WAS FOUND WITH WEAR AND CORROSION, WHICH WAS BEYOND ALLOWABLE LIMITS, AT THE MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, SPOILER BEAM ATTACH HOLES, HINGE SUPPORT FITTING ATTACH BOLT HOLES, AND THE CLIP ASSY ATTACH BOLT
- [SDR DL72W010178](https://openairdocs.org/sdr/DL72W010178.md): Slat Track · corroded · Jan 31, 2001 · N2819W · Boeing 727247 · Leading Edge Devices
  > DURING OVERHAUL THE INBD TRACK, CORROSION AND WEAR WAS FOUND, WHICH WERE BEYOND ALLOWABLE LIMITS, AT MLG BEAM ATTACH BOLT HOLE AND SPOTFACES, SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGE FITTING HOLES, THE TOGGLE DETENT HOLE AND THE CLIP ASSEMBLY ATTACH B
- [SDR DL72W010308](https://openairdocs.org/sdr/DL72W010308.md): Rib · cracked · Jan 30, 2001 · N2819W · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP VISIT THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOVING THE DAMAGE AND INSTALLING A FILLER AND DOUBLER.
- [SDR DL72W010048](https://openairdocs.org/sdr/DL72W010048.md): Skin · cracked · Jan 10, 2001 · N2819W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A 2.75 INCH LONG CRACK WAS FOUND IN THE UPPER SKIN AT THE UPPER FASTENER ROW OF THE STRINGER 26L SKIN LAP JOINT AT FS 700. THE DAMAGED SECTION OF SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER PER B727 SRM 53-30-3, FIG 14 AND ER/A 379754-14.
- [SDR DL72W002141](https://openairdocs.org/sdr/DL72W002141.md): Battery Pack · discharged · Oct 31, 2000 · N2819W · Boeing 727247 · Emergency Lighting
  > FOUND L2 DOOR OVERHEAD EMER LIGHT INOP. REPLACED L2 DOOR OVERHEAD EMER LIGHT BATTERY PACK.
- [SDR DL72W001441](https://openairdocs.org/sdr/DL72W001441.md): Megaphone · inoperative · Jul 31, 2000 · N2819W · Boeing 727247 · Emergency Equipment
  > MEGAPHONE IN FWD CLOSET INOP. REPLACED SAME.
- [SDR DL72W001109](https://openairdocs.org/sdr/DL72W001109.md): Skin · cracked · Jun 8, 2000 · N2819W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A 0.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN EMANATING FROM THE LWR FWD CORNER OF THE L-4 WINDOW CUTOUT. REPAIR PER ERA 377485-14, REV A.
- [SDR DL72W001095](https://openairdocs.org/sdr/DL72W001095.md): Beam · cracked · Jun 2, 2000 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > HFEC INSPECTION OF A FASTENER HOLE IN THE RBL 17.3 VERTICAL BEAM ON THE FS 1183 BULKHEAD AT WL 283 REVEALED A CRACK INDICATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITIONAL INSURANCE CUT. THE HOLE WAS BUSHED AND THE NOMINAL FASTENER INS
- [SDR DL72W000320](https://openairdocs.org/sdr/DL72W000320.md): Battery · discharged · Feb 15, 2000 · N2819W · Boeing 727247 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHTS FLASHING. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERIES.
- [SDR DL72W992432](https://openairdocs.org/sdr/DL72W992432.md): Bracket · cracked · Nov 3, 1999 · N2819W · Boeing 727247 · Leading Edge Slat Actuator
  > INBD ATTACH BRACKET CRACKED NR 1 SLAT ACTUATOR BRKT. INSTALLED DOUBLER PER M/M 57-20-21. TPA F-1 LETTER CHECK.
- [SDR DL72W992126](https://openairdocs.org/sdr/DL72W992126.md): Actuator · failed · Sep 22, 1999 · N2819W · Boeing 727247 · Leading Edge Slat Actuator
  > ARRIVING DFW, LOST 'A' SYS HYD. GEAR CAME DOWN NORMALLY, BUT UPON LANDING ZERO QTY AND INTERMITTENT PRESSURE UNTIL PUMP SHUT DOWN AT STOP. REMOVED AND REPLACED NR 8 SLAT ACTUATOR. REPLACED SYS 'A' FILTERS AND CASE DRAIN FILTERS. LEAK CKS GOOD. SERVICED H
- [SDR DL72W991834](https://openairdocs.org/sdr/DL72W991834.md): Beam · damaged · Aug 17, 1999 · N2819W · Boeing 727247 · Cargo/Baggage Doors
  > C2 DOOR / UPPER PRESSURE BEAM, THE UPPER PRESSURE BEAM WAS FOUND DAMAGED DUE TO GROUND HANDLING AT THE AFT PRESSURE STOP FITTING ATTACH LOCATION. AUTHORIZED REPAIR TO TRIM AND REMOVE AFT HALF OF PRESSURE BEAM AND SPLICE-IN REPLACEMENT SECTION.
- [SDR DL72W991001](https://openairdocs.org/sdr/DL72W991001.md): Compressor · stalled · May 6, 1999 · N2819W · Boeing 727247 · Turbine Engine Compressor Section
  > DEPARTING DFW AFT CARGO DOOR CAME OPEN DURING ROTATION AT T/O. NUMBER 3 ENGINE PRECAUTIONARY SHUT DOWN IN FLIGHT DUE TO MULTIPLE COMPRESSOR STALLS. ONE FAN BLADE NICKED AND MINOR DAMAGE TO ACCOUSTICAL PANEL.
- [SDR DL72W990710](https://openairdocs.org/sdr/DL72W990710.md): Web · cracked · Mar 31, 1999 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > A TYPICAL CRACK WAS FOUND IN THE INBOARD VERTICAL WEB OF THE RT AFT ENTRY DOOR TORQUE BOX AT FS 1271. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 367089-14AD.
- [SDR DL72W990320](https://openairdocs.org/sdr/DL72W990320.md): Skin · cracked · Feb 17, 1999 · N2819W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 681-740 STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS
- [SDR DL72W990319](https://openairdocs.org/sdr/DL72W990319.md): Skin · cracked · Feb 17, 1999 · N2819W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-680 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 23 CRACK
- [SDR DL72W990285](https://openairdocs.org/sdr/DL72W990285.md): Battery Pack · discharged · Feb 12, 1999 · N2819W · Boeing 727247 · Emergency Lighting
  > REAR AISLE EMERGENCY EXIT SIGN BATTERY WEAK. REPLACED BATTERY PACK.
- [SDR DL72W982475](https://openairdocs.org/sdr/DL72W982475.md): Skin · corroded · Nov 26, 1998 · N2819W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 720A-720B, STRINGER 27R-28R. REPAIR FOR CORROSION CUTOUT. THE FUSLAGE SKIN WAS FOUND CORRODED BETWEEN FS 720A AND FS 720B BETWEEN STRINGERS 27R AND 28R. THE CORROSION WAS REMOVED WITH A 3 BY 3.75 CUTOUT AND A 7.5 BY 3 CUTOUT. THE CUTOUTS W
- [SDR DL72W982474](https://openairdocs.org/sdr/DL72W982474.md): Fitting · cracked · Nov 26, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FUSELAGE RT STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG FITTING AREA WAS INSPECTED PER BAC S/B 727-53-0141. CORROSION AND CRACK INDICATIONS WERE FOUND IN THE FITTING, STRINGER, AND SKIN. THE DAMAGED AREA OF SKIN WAS CUTOUT AND
- [SDR DL72W982473](https://openairdocs.org/sdr/DL72W982473.md): Fitting · cracked · Nov 26, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FUSELAGE STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG ATTACH FITTING WAS INSPECTED PER BAC S/B727-53-0141 (LT SIDE). TWO FASTENER HOLES COMMON TO STRINGER 18-A WERE FOUND TO HAVE CRACK INDICATIONS. THE HOLES WERE OVERSIZED TO REM
- [SDR DL72W982434](https://openairdocs.org/sdr/DL72W982434.md): Panel · puncture · Nov 20, 1998 · N2819W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND DURING MV2 CORROSION VISIT NRC 330, HOLE IN LT ELEVATOR BALANCE BOARD ACCESS PANEL NR 9119. REPAIRED PER SRM 55-20-3 FIG 1.
- [SDR DL72W982343](https://openairdocs.org/sdr/DL72W982343.md): Strap · cracked · Nov 11, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE R2 DOOR SURROUND BEAR STRAP WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS APPROX 2 INCHES LONG AND CONFINED TO THE BEAR STRAP ONLY. THE CRACK WAS REPAIRED WITH AN EXTERNAL DOUBLER PER BAC S/B 727-53-0136 & DOCUMENTED PER ER/A
- [SDR DL72W982435](https://openairdocs.org/sdr/DL72W982435.md): Floorbeam · corrosion · Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Main, Floor Beam
  > FOUND DURING MV2 CORROSION VISIT NRC 16, CORROSION ON FLOORBEAM STA 344 BETWEEN RBL 13 AND RBL 25. REPAIRED PER SRM 53-10-8 FIG 11.
- [SDR DL72W982335](https://openairdocs.org/sdr/DL72W982335.md): Floorbeam · corroded · Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Main, Floor Beam
  > FOUND DURING MV2 CORROSION VISIT NRC 81, CORROSION ON FLOORBEAM STA 1050 AT RBL 33. REPAIRED PER M/M 53-20-11 FIG 804A RBL 33 TO RBL 19.
- [SDR DL72W982334](https://openairdocs.org/sdr/DL72W982334.md): Frame · cracked · Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > A.5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER DOOR STOP. REPAIRED PER SRM 53-10-09.
- [SDR DL72W981782](https://openairdocs.org/sdr/DL72W981782.md): Chord · cracked · Aug 24, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE 65-17510-90 INNER CHORD OF THE VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A CRACK AT FS 1274. THE CRACK IS TYPICAL OF BAC S/B 53-0129. THE CRACKED CHORD WAS REPAIRED WITH A REPAIR ANGLE AND STRAPS PER THE PROCEDURES OUTLINED IN THE BAC S/B. THE REPAIR
- [SDR DL72W981755](https://openairdocs.org/sdr/DL72W981755.md): Web · cracked · Aug 24, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > RT VERTICAL TORQUE BOX WEB UPPER LIGHTENING HOLE HAS.375 INCH CRACK AT STA 1293. REPAIRED PER M/M 53-11-0 FIG 819.
- [SDR DL72W981684](https://openairdocs.org/sdr/DL72W981684.md): Light · inoperative · Aug 15, 1998 · N2819W · Boeing 727247 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT AFT AIRSTAIRS INOP. MTC REPLACED LIGHT ASSY, OPS CKS. OK.
- [SDR DL72W981296](https://openairdocs.org/sdr/DL72W981296.md): Lights · inoperative · Jun 18, 1998 · N2819W · Boeing 727247 · Emergency Lighting
  > FWD SECTION OF FLOOR TRACK LIGHTING IN FC INOP. REPLACED FWD AND AFT FLOOR TRACK LGT PWR SUPPLIES AND BATTS. REPAIRED CHAFFED WIRE UNDER SEAT 1 AB.
- [SDR DL72W980947](https://openairdocs.org/sdr/DL72W980947.md): Rack · inoperative · May 2, 1998 · N2819W · Boeing 727247 · Emergency Lighting
  > RT AFT OVERWING EMER EXIT LIGHT INOP. REPLACED BATT RACK, OPS NOW NML.
- [SDR DL72W971378](https://openairdocs.org/sdr/DL72W971378.md): Csd · failed · Jul 14, 1997 · N2819W · Boeing 727247 · Alternator-Generator Drive
  > ON FINAL APPROACH NR 1 ENG DRIVEN GEN FAILED. AFTER LANDING NR 1 ENG FIRE WARNING ILLUMINATED AND BELL CAME ON. FIRE HANDLE WAS PULLED AND BOTH BOTTLES DISCHARGED. AFTER OPENING COWLING FOUND THE CSD AND GEN TO BE THE SOURCE OF IGNITION. REPLACED CSD AND G
- [SDR DL72W971296](https://openairdocs.org/sdr/DL72W971296.md): Sequence Valve · malfunctioned · Jul 4, 1997 · N2819W · Boeing 727247 · Landing Gear Retraction/Extension System
  > RIGHT MAIN LANDING GEAR FAILED TO EXTEND. CRANKED AS PER POM AND LANDED NORMALLY. REPLACED RIGHT MAIN GEAR SEQUENCE VALVE AND UP LOCK ACTUATOR. OPERATED LANDING GEAR SEVERAL TIMES, CKS OK.
- [SDR DL72W962480](https://openairdocs.org/sdr/DL72W962480.md): Side Wall · cracked · Nov 8, 1996 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND A.75 INCH CRACK AT RIGH-HAND SIDE WALL OF THE NOSE LANDING GEAR WHEELWELL. REPAIRED PER DAL ER/A 304418-14AD.
- [SDR DL72W962472](https://openairdocs.org/sdr/DL72W962472.md): Tee Angle · corrosion · Nov 7, 1996 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON ATTACH ANGLE FOR ACCESS DOOR 3348L. REPAIRED PER MM 53-30-1.
- [SDR DL72W961762](https://openairdocs.org/sdr/DL72W961762.md): Bulkhead Web · cracked · Jul 23, 1996 · N2819W · Boeing 727247 · Fuselage Main, Bulkhead
  > FOUND CRACK AT RBL 27 OF BS 1183 BULKHEAD WEB. THE DAMAGE CONSISTED OF A.75 INCH CRACK AT WL 170. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY S/B 727-53-171. REPAIRED PER B727 SRM 53-10-9, FIG. 4.
- [SDR DL72W961518](https://openairdocs.org/sdr/DL72W961518.md): Bulb · failed · Jun 24, 1996 · N2819W · Boeing 727247 · Emergency Lighting
  > ON LAYOVER, FOUND RIGHT AFT SLIDE LIGHT INOP. RELAMPED SAME, CHECKS GOOD.
- [SDR DL72W960930](https://openairdocs.org/sdr/DL72W960930.md): Act Angle · cracked · Apr 18, 1996 · N2819W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 8 SLAT ACTUATOR INBOARD ATTACH ANGLE CRACKED. REPAIR PER M/M 57-20-21.
- [SDR DL72W960929](https://openairdocs.org/sdr/DL72W960929.md): Act Support · cracked · Apr 18, 1996 · N2819W · Boeing 727247 · Leading Edge Slat Actuator
  > FOUND TWO-INCH CRACK IN NR 8 SLAT OUTBOARD ACTUATOR SUPPORT WHILE SHOWING MAINTENANCE LOCATION OF CRACK AT INBOARD SUPPORT. REPAIR PER M/M 57-20-21.
- [SDR DL72W960927](https://openairdocs.org/sdr/DL72W960927.md): Swivel Fitting · out of adjust · Apr 18, 1996 · N2819W · Boeing 727247 · Wing, Landing Gear Attach Fittings
  > MLG SPAR BEING CHAFED BY STRUT DOOR SIDE BRACE SWIVEL FITTING. REWORK PER M/M 57-43-0.
- [SDR DL72W960926](https://openairdocs.org/sdr/DL72W960926.md): Web · cracked · Apr 18, 1996 · N2819W · Boeing 727247 · Fuselage Miscellaneous Structure
  > .3750 INCH CRACK IN LIGHTNING HOLE OF LT LOWER TORQUE BOX WEB, STA 1263, TOP HOLE. REPAIR PER M/M 53-11-0.
- [SDR DL72W954772](https://openairdocs.org/sdr/DL72W954772.md): Battery Pack · discharged · Dec 26, 1995 · N2819W · Boeing 727247 · Emergency Lighting
  > TWO AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CK GOOD.
- [SDR DL72W953704](https://openairdocs.org/sdr/DL72W953704.md): Angle · cracked · Sep 14, 1995 · N2819W · Boeing 727247 · Leading Edge Devices
  > FOUND ON B2 LETTER CHECK, CRACK IN NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.

Next page: https://openairdocs.org/aircraft/N2819W/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 = 'N2819W' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N2819W/reports

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