# Service difficulty reports: N2814W, cancelled Mar 27, 2001

A list on [N2814W, cancelled Mar 27, 2001](https://openairdocs.org/deregistered/N2814W-2001-03-27.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 · 67 reports

- [SDR DL72W002523](https://openairdocs.org/sdr/DL72W002523.md): Slat · missing · Dec 26, 2000 · N2814W · Boeing 727247 · Leading Edge Devices
  > DURING APPROACH CONTROLS REQUIRED 20 DEGREES RIGHT AILERON AND 2 UNITS RIGHT RUDDER TO TRACK CENTER LINE. CA FOUND SECTION OF FOREFLAP MISSING FROM LT OUTBD T.E FLAP - REPLACED FLPA PER M/M. OPS CHK OK
- [SDR DL72W002172](https://openairdocs.org/sdr/DL72W002172.md): Screw · loose · Nov 5, 2000 · N2814W · Boeing 727247 · Passenger Compartment Windows
  > A/C DIVERTED TO DFW FOR AN R2 WINDOW SQUEAL. PRESSURIZED A/C TO 5 PSI AND FOUND LEAK ON BOTTOM OF R3 WINDOW. RETORQUED AND PRESSURIZED A/C TO 6 PSI AND LEAK CKS GOOD.
- [SDR DL72W001266](https://openairdocs.org/sdr/DL72W001266.md): Smoke · detected · Jul 5, 2000 · N2814W · Boeing 727247 · Air Distribution System
  > AFTER GENERATORS TRIPPED PACKS, OVERHEATED AND SMOKE ENTERED CABIN. SHUT DOWN PACKS. RAN PACKS AFTER GEN MTC AND ALL CKS NORMAL.
- [SDR DL72W001217](https://openairdocs.org/sdr/DL72W001217.md): Web · cracked · Jun 27, 2000 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON D-2 CHECK, 1 INCH CRACK IN LOWER RT CORNER OF VERTICAL WEB ABOVE -S- DUCT AT STA 1303. REPAIRED PER B727 DRD 53-10-4D FIG 802D.
- [SDR DL72W001216](https://openairdocs.org/sdr/DL72W001216.md): Skin · cracked · Jun 27, 2000 · N2814W · Boeing 727247 · Elevator, Plate/Skin
  > FOUND ON D-2 CHECK, 7 INCH CRACK ON RT ELEVATOR LOWER SKIN, AFT OF NR 4 BALANCE BOARD. REPAIRED PER B727 DRD 55-20-3D FIG 4.
- [SDR DL72W000645](https://openairdocs.org/sdr/DL72W000645.md): Line · broken · Apr 5, 2000 · N2814W · Boeing 727247 · Hydraulic System, Main
  > FIFTEEN MINUTES OUT OF DCA, FLIGHT CREW REPORTED A HYDRAULIC SYSTEM FLUID LOSS. FOUND HYDRAULIC LINE LEAKING. REPLACED SAME.
- [SDR DL72W992623](https://openairdocs.org/sdr/DL72W992623.md): Light · inoperative · Nov 30, 1999 · N2814W · Boeing 727247 · Emergency Lighting
  > ON PREFLIGHT CHECKLIST, CREW FOUND RIGHT REAR EMERGENCY OVERWING LIGHT INOP IN EMERGENCY MODE ON TEST. FOUND CANNON PLUG DISCONNECTED ON ASSOCIATED BATTERY PACK. RECONNECTED CANNON PLUG, LIGHT TESTS GOOD IN EMERGENCY MODE ON CHECK OUT.
- [SDR DL72W992589](https://openairdocs.org/sdr/DL72W992589.md): Stiffener · cracked · Nov 23, 1999 · N2814W · Boeing 727247 · Leading Edge Devices
  > L/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER M/M 57-20-21 PG 813 {NR 6 SLAT}.
- [SDR DL72W992587](https://openairdocs.org/sdr/DL72W992587.md): Stiffener · cracked · Nov 23, 1999 · N2814W · Boeing 727247 · Wing Miscellaneous Structure
  > A 1 INCH CRACK WING L/E SPAR STIFFENER O/B SIDE OF I/B TRACK BOX NR 4 SLAT. REPLACED SPAR STIFFENER PER MM 57-20-21.
- [SDR DL72W992359](https://openairdocs.org/sdr/DL72W992359.md): Insulation · damaged · Oct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System Wiring
  > ON HUSH KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL
- [SDR DL72W992358](https://openairdocs.org/sdr/DL72W992358.md): Insulation · damaged · Oct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System Wiring
  > ON HUSH KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL
- [SDR DL72W992168](https://openairdocs.org/sdr/DL72W992168.md): Mechanism · malfunctioned · Sep 28, 1999 · N2814W · Boeing 727247 · Landing Gear Door Retract Section
  > LANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION AND REMAINED OPEN AFTER EXTENSION. SECURED BOLT IN NOSE GEAR DOOR LINKAGE.
- [SDR DL72W992028](https://openairdocs.org/sdr/DL72W992028.md): Light · inop · Sep 12, 1999 · N2814W · Boeing 727247 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED LIGHT, CKS NML.
- [SDR DL72W991977](https://openairdocs.org/sdr/DL72W991977.md): Fan · failed · Sep 6, 1999 · N2814W · Boeing 727247 · Air Distribution Fan
  > SMOKE IN COCKPIT COMING FROM THE GASPER VENTS. REPLACED GASPER FAN PER M/M. OPS NORMAL.
- [SDR DL72W991972](https://openairdocs.org/sdr/DL72W991972.md): Fan · failed · Sep 5, 1999 · N2814W · Boeing 727247 · Air Distribution Fan
  > JUST PRIOR TO DESCENT INTO TUS, A SLIGHT SMELL OF SMOKE WAS SMELLED IN THE COCKPIT AND BY THE FLIGHT ATTENDENTS IN THE VBACK OF THE CABIN. THE ODOR APPEARED TO BE COMING OUT OF THE GASPERS. THE SMELL OF SMOKE DISSIPATED AFTER A COUPLE OF MINUTES. REPLACED G
- [SDR DL72W991948](https://openairdocs.org/sdr/DL72W991948.md): Static Line · failed · Sep 1, 1999 · N2814W · Boeing 727247 · Pitot/Static System
  > CAPT'S AIRSPEED INDICATOR FROZE AT 210KTS AT ABOUT 2000 FOO ON CLIMB-OUT. ALTIMETER READINGS CONSISTENTLY LOWER THAN F/O'S. ALTIMETER READINGS. CADC WOULD NOT RESET. SELECTING ALTERNATE SOURCE DID NOT CORRECT PROBLEM. REPLACED CAP'T A/S AND ALT STATIC LIN
- [SDR DL72W990878](https://openairdocs.org/sdr/DL72W990878.md): Bracket · cracked · Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat Actuator
  > REF NRC 84 C-2 LETTER CHECK, NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-20-22.
- [SDR DL72W990877](https://openairdocs.org/sdr/DL72W990877.md): Bracket · cracked · Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat Actuator
  > REF NRC 83 C-2 LETTER CHECK, NR 7 SLAT ACT INBD MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-42-0.
- [SDR DL72W990511](https://openairdocs.org/sdr/DL72W990511.md): Bulb · failed · Mar 10, 1999 · N2814W · Boeing 727247 · Emergency Lighting
  > 2L EMERGENCY EXIT SIGN INOP. RELAMPED EXIT SIGN, OPS CK NORMAL.
- [SDR DL72W990246](https://openairdocs.org/sdr/DL72W990246.md): Sill · corroded · Feb 4, 1999 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE OUTER CHORD OF THE C-2 DOOR SURROUND LOWER SILL WAS FOUND WITH CORROSION ON THE OUTER FLANGE BETWEEN THE DOOR FRAME JAMBS. THE CORRODED AREAS WERE TRIMMED OUT AND TWO STEEL REPAIR ANGLES WERE INSTALLED TO REPAIR THE CUTOUTS. THE REPAIR WAS ACCOMPLISHED
- [SDR DL72W990218](https://openairdocs.org/sdr/DL72W990218.md): Skin · cracked · Feb 2, 1999 · N2814W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND DURING MV1 CORROSION VISIT NRC 126 ON OK TO INSTALL L-4 WINDOW, FOUND.375 INCH CRACK IN FUSELAGE SKIN AT BOTTOM I/B BOLT HOLE. REPAIRED PER SRM 53-30-3 FIG 8.
- [SDR DL72W981904](https://openairdocs.org/sdr/DL72W981904.md): Actuator · failed · Sep 13, 1998 · N2814W · Boeing 727247 · Leading Edge Slat Actuator
  > AFTER T/O, LOST 'A' SYS HYD QTY AND PRESS IND ZERO. PROCEDURES COMPLIED WITH ALT FLAP SW USED GPWS INHIBITED. GEAR PIN INSTALLED BY MTC. REMOVED AND REPLACED NR 1 SLAT ACT. OPS AND LEAK CKS GOOD.
- [SDR DL72W981697](https://openairdocs.org/sdr/DL72W981697.md): Battery · discharged · Aug 14, 1998 · N2814W · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS AT RT WING INOP. REPLACED BATTERY PACK.
- [SDR DL72W981314](https://openairdocs.org/sdr/DL72W981314.md): Battery Pack · discharged · Jun 22, 1998 · N2814W · Boeing 727247 · Emergency Lighting
  > OVERWING RT EMERG LIGHTS INOP ON TEST FOR L/O. REPLACED BATT RACK AND BATT PACK, CKS GOOD.
- [SDR DL72W980465](https://openairdocs.org/sdr/DL72W980465.md): Web · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > I/B VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1214 RT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0.
- [SDR DL72W980463](https://openairdocs.org/sdr/DL72W980463.md): Web · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > A.25 INCH CRACK AT UPPER LIGHTENING HOLE STA 1229 LT SIDE OF I/B VERT WEB. ROUTED OUT DAMAGE PER M/M 53-11-0.
- [SDR DL72W980462](https://openairdocs.org/sdr/DL72W980462.md): Web · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > I/B VERT WEB CRACKED AT UPPER FASTENER HOLE STA 1233 LT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0.
- [SDR DL72W980461](https://openairdocs.org/sdr/DL72W980461.md): Web · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND DURING B-2 LETTER CHECK, LWR LT VERTICAL WEB CRACKED FS 1233 AND FS 1229. REPAIRED PER M/M 53-11-0.
- [SDR DL72W980460](https://openairdocs.org/sdr/DL72W980460.md): Web · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND DURING B-2 LETTER CHECK, LWR RT TORQUE BOX VERTICAL WEB CRACKED FS 1214. REPAIRED PER M/M 53-11-0.
- [SDR DL72W980459](https://openairdocs.org/sdr/DL72W980459.md): Bracket · cracked · Feb 23, 1998 · N2814W · Boeing 727247 · Leading Edge Devices
  > FOUND AT B2 LETTER CHECK, NR 2 LE FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER EDGE. REPAIRED PER M/M 57-20-21.
- [SDR DL72W980018](https://openairdocs.org/sdr/DL72W980018.md): Pbe · defective · Jan 2, 1998 · N2814W · Boeing 727247 · Portable Oxygen System
  > PBE RED INDICATOR EXTENDED PASSED FLUSH. REPLACED PBE.
- [SDR DL72W971939](https://openairdocs.org/sdr/DL72W971939.md): Light · inoperative · Sep 30, 1997 · N2814W · Boeing 727247 · Emergency Lighting
  > RT OVERWING EXIT FWD CENTER AISLE AND AFT RT EXTER FAIRING EMERGENCY LIGHT INOP.
- [SDR DL72W971561](https://openairdocs.org/sdr/DL72W971561.md): Line · leaking · Aug 8, 1997 · N2814W · Boeing 727247 · Hydraulic System, Main
  > SYSTEM B LOW PRESS LIGHT 2 EACH CAME ON AND QUANITY WENT TO 0. FOUND NR 2 A/C HYD PUMP PRESS AND RETURN LINES WITH A SMALL HOLE IN THEM, THE PRESS LINE MADE THE HOLE IN THE RETURN LINE. REPLACED LINES.
- [SDR DL72W962659](https://openairdocs.org/sdr/DL72W962659.md): Angle · cracked · Dec 6, 1996 · N2814W · Boeing 727247 · Leading Edge Devices
  > FOUND DURING A-2 LETTER CHECK, 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B UPSTOP PAD. REPAIRED PER M/M 57-54-0PAR 12.
- [SDR DL72W961200](https://openairdocs.org/sdr/DL72W961200.md): Stiffener · cracked · May 17, 1996 · N2814W · Boeing 727247 · Leading Edge Devices
  > FOUND ON A-1 LETTER CHECK, FWD SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-21.
- [SDR DL72W961199](https://openairdocs.org/sdr/DL72W961199.md): Doubler · damaged · May 17, 1996 · N2814W · Boeing 727247 · Rudder Structure
  > DOUBLER DAMAGED LOWER RUDDER LOWER RT HINGE AREA. REPLACED RUDDER PER SRM 55-2-3.
- [SDR DL72W954754](https://openairdocs.org/sdr/DL72W954754.md): Line · leaking · Dec 22, 1995 · N2814W · Boeing 727247 · Hydraulic System, Main
  > LOSS OF B-SYSTEM QUANITITY DOWN TO ZERO - ON FINAL AFTER GEAR DOWN BRAKE PRESSURE ABOVE 1500 PSI, NR 1 B-SYSTEM PUMP OFF. NR 2 SYSTEM TURNED OFF AND FLICKER OF LOW PRESSURE LIGHT. CORRECTIVE ACTION - FOUND B-HYDRAULIC LINE LEAKING. REPLACED SAME, LEAK CKS AN
- [SDR DL72W954457](https://openairdocs.org/sdr/DL72W954457.md): Skin · damaged · Nov 20, 1995 · N2814W · Boeing 727247 · Elevator, Plate/Skin
  > DURING SHOP INSPECTION, RT ELEVATOR WAS REPAIRED FOR DAMAGE TO LOWER SKIN AT ACCESS ANGLE 9, PER SRM 55-20-3.
- [SDR DL72W954438](https://openairdocs.org/sdr/DL72W954438.md): Ribs · cracked · Nov 19, 1995 · N2814W · Boeing 727247 · Leading Edge Devices
  > RIBS ON I/B AND O/B SIDES OF ACT ATTACH POINT NR 4 SLAT ARE CRACKED FWD OF PREVIOUS REPAIRS. REMOVED OLD DOUBLERS AND DAMAGED AREAS, FABRICATED DOUBLERS PER M/M 57-54-0 FIG 804 AND INSTALLED DOUBLERS PER M/M 57-54-0.
- [SDR DL72W954541](https://openairdocs.org/sdr/DL72W954541.md): Rib · cracked · Nov 17, 1995 · N2814W · Boeing 727247 · Wing, Rib/Bulkhead
  > THE RBL 70.65 WING RIB HAS A CRACK EMANATING FROM THE LOWER OF TWO FASTENER HOLES USED FOR A FUEL CROSSOVER LINE ATTACH CLIP, AND TERMINATING IN THE LOWER FUEL CROSSOVER CUT-OUT LOCATED AT APPROXIMATELY BS 835. THE CRACK MEASURES 0.5 INCH IN LENGTH. THE WEB
- [SDR DL72W954426](https://openairdocs.org/sdr/DL72W954426.md): Skin · damaged · Nov 17, 1995 · N2814W · Boeing 727247 · Rudder, Plate/Skin
  > RT SIDE OF LOWER RUDDER HAS A SMALL 1 INCH CREASE, APPROX 8 INCHES ABOVE PANEL 9901 MIDDLE OF RUDDER. STOP DRILLED DAMAGE AS PER B-727 SRM 55-40-2 FIG 1 AND B727 SRM 55-20-3 FIG 4. FABRICATED REPAIR PART AS PER B727 SRM 55-40-2 FIG 1 AND B727 SRM 55-20-3 FI
- [SDR DL72W954405](https://openairdocs.org/sdr/DL72W954405.md): Skin · damaged · Nov 15, 1995 · N2814W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING LOWERING OF THE NOSE JACK STAND, A STAND SUPPORT PIN SHEARED CAUSING EQUIPMENT ON THE STAND TO STRIKE THE AIRCRAFT. A 2 INCH BY 2 INCH HOLE WAS TORN INTO THE FUSELAGE AT FS 300 BETWEEN STR 9R AND STR 10R. THAT WAS CLEANED UP AND THE FINAL DIMENSIONS O
- [SDR DL72W954403](https://openairdocs.org/sdr/DL72W954403.md): Skin · damaged · Nov 15, 1995 · N2814W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING HMV, AN TIME LIMITED REPAIR WAS FOUND LOCATED APPROXIMATELY 6 INCHES ABOVE AND AFT OF THE RAIN GUTTER AT THE L-1 DOOR, AT APPROXIMATELY FS 344 TO 360. THE EXISTING REPAIR WAS REMOVED AND ADDITIONAL DAMAGE CUT OUT. TOTAL DAMAGE REMOVAL RESULTED IN A 6
- [SDR DL72W954739](https://openairdocs.org/sdr/DL72W954739.md): Doubler · carcked · Nov 14, 1995 · N2814W · Boeing 727247 · Trailing Edge Flaps
  > DURING HMV SHOP INSP, FOUND THAT THE NR 4 O/B MIDFLAP, I/B RIB AFT LOWER CORNER REPAIR DOULBER WAS NOT INSTALLED PER M/M. INSTALLED NEW DOULBER PER M/M 57-52-0.
- [SDR DL72W954245](https://openairdocs.org/sdr/DL72W954245.md): Stringer · cracked · Nov 2, 1995 · N2814W · Boeing 727247 · Wing, Longeron/Stringer
  > ATL - HMV, HFEC INSP OF WS 686.50 STR 9 HAS A CRACK EXITING FASTENER HOLE AWAY FROM RADIUS. REPAIRED PER MM 57-13-0.
- [SDR DL72W954240](https://openairdocs.org/sdr/DL72W954240.md): Stringer · cracked · Nov 2, 1995 · N2814W · Boeing 727247 · Wing, Longeron/Stringer
  > AT HMV INSPECTION, HFEC INSP OF WS 629.00 STR NR 9 HAS A CRACK EXITING FASTENER HOLE AWAY FROM RADIUS. DRILLED REPAIR ANGLE PER M/M 57-13-0, INSTALLED REPAIR.
- [SDR DL72W954221](https://openairdocs.org/sdr/DL72W954221.md): Skin · damaged · Nov 2, 1995 · N2814W · Boeing 727247 · Spoilers
  > SPOILER WAS DENTED ON UPPER SKIN SURFACE APPROX 8 INCHES FROM L/E AND 6 INCHES FROM I/B EDGE. REPAIRED PER MM 57-50-6.
- [SDR DL72W954275](https://openairdocs.org/sdr/DL72W954275.md): Rib · cracked · Oct 31, 1995 · N2814W · Boeing 727247 · Leading Edge Devices
  > DURING HMV, FOUND NR 8 SLAT, NR 3 L/E REINFORCING RIB CRACKED. REMOVED O/B TRACK FOR ACCESS AND REPAIRED RIB PER M/M 57-54-0 PG 806 AND 807.
- [SDR DL72W954261](https://openairdocs.org/sdr/DL72W954261.md): Vertical Beam · cracked · Oct 26, 1995 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > ATL - HMV, A CRACK WAS FOUND ON THE VERTICAL BEAM ON THE OUTBOARD SIDE STATION 1183 RBL 8 AND AN EXISTING REPAIR FOR SIMILAR DAMAGE FOR LBL 8. ALSO, ON THE VERTICAL BEAM ON THE OUTBOARD SIDE STATION 1183, THAT WAS NOT INSTALLED PER EO 4-59275-3AD FIG 3. THIS
- [SDR DL72W954394](https://openairdocs.org/sdr/DL72W954394.md): Angle · cracked · Oct 22, 1995 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
  > AT HMV-1, INSP FOUND CHORD ANGLE CRACKED AT 48 SECTION LT SIDE STA 1342. THE HORIZONTAL CHORD ANGLE IS CRACKED JUST I/B OF FIN TERMINAL FITTING. FITTING IS PREVIOUSLY STOP DRILLED. REPAIRED CRACK PER M/M 53-11-0 PG 808.

Next page: https://openairdocs.org/deregistered/N2814W-2001-03-27/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 = 'N2814W' AND deregistration_id = 'N2814W-2001-03-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2814W-2001-03-27/reports

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