N2814W, cancelled Mar 27, 2001

Service difficulty reports · 67

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DL72W002523Slat · missingDURING 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 OKDec 26, 2000 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W002172Screw · looseA/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.Nov 5, 2000 · N2814W · Boeing 727247 · Passenger Compartment WindowsSDR DL72W001266Smoke · detectedAFTER GENERATORS TRIPPED PACKS, OVERHEATED AND SMOKE ENTERED CABIN. SHUT DOWN PACKS. RAN PACKS AFTER GEN MTC AND ALL CKS NORMAL.Jul 5, 2000 · N2814W · Boeing 727247 · Air Distribution SystemSDR DL72W001217Web · crackedFOUND 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.Jun 27, 2000 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W001216Skin · crackedFOUND 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.Jun 27, 2000 · N2814W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W000645Line · brokenFIFTEEN MINUTES OUT OF DCA, FLIGHT CREW REPORTED A HYDRAULIC SYSTEM FLUID LOSS. FOUND HYDRAULIC LINE LEAKING. REPLACED SAME.Apr 5, 2000 · N2814W · Boeing 727247 · Hydraulic System, MainSDR DL72W992623Light · inoperativeON 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.Nov 30, 1999 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W992589Stiffener · crackedL/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}.Nov 23, 1999 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W992587Stiffener · crackedA 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.Nov 23, 1999 · N2814W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W992359Insulation · damagedON 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-SLOct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System WiringSDR DL72W992358Insulation · damagedON 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-SLOct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System WiringSDR DL72W992168Mechanism · malfunctionedLANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION AND REMAINED OPEN AFTER EXTENSION. SECURED BOLT IN NOSE GEAR DOOR LINKAGE.Sep 28, 1999 · N2814W · Boeing 727247 · Landing Gear Door Retract SectionSDR DL72W992028Light · inopOVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED LIGHT, CKS NML.Sep 12, 1999 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W991977Fan · failedSMOKE IN COCKPIT COMING FROM THE GASPER VENTS. REPLACED GASPER FAN PER M/M. OPS NORMAL.Sep 6, 1999 · N2814W · Boeing 727247 · Air Distribution FanSDR DL72W991972Fan · failedJUST 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 GSep 5, 1999 · N2814W · Boeing 727247 · Air Distribution FanSDR DL72W991948Static Line · failedCAPT'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 LINSep 1, 1999 · N2814W · Boeing 727247 · Pitot/Static SystemSDR DL72W990878Bracket · crackedREF NRC 84 C-2 LETTER CHECK, NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-20-22.Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990877Bracket · crackedREF NRC 83 C-2 LETTER CHECK, NR 7 SLAT ACT INBD MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-42-0.Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990511Bulb · failed2L EMERGENCY EXIT SIGN INOP. RELAMPED EXIT SIGN, OPS CK NORMAL.Mar 10, 1999 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W990246Sill · corrodedTHE 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 ACCOMPLISHEDFeb 4, 1999 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990218Skin · crackedFOUND 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.Feb 2, 1999 · N2814W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W981904Actuator · failedAFTER 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.Sep 13, 1998 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W981697Battery · dischargedEMERGENCY EXIT LIGHTS AT RT WING INOP. REPLACED BATTERY PACK.Aug 14, 1998 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W981314Battery Pack · dischargedOVERWING RT EMERG LIGHTS INOP ON TEST FOR L/O. REPLACED BATT RACK AND BATT PACK, CKS GOOD.Jun 22, 1998 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W980465Web · crackedI/B VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1214 RT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0.Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980463Web · crackedA .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.Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980462Web · crackedI/B VERT WEB CRACKED AT UPPER FASTENER HOLE STA 1233 LT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0.Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980461Web · crackedFOUND DURING B-2 LETTER CHECK, LWR LT VERTICAL WEB CRACKED FS 1233 AND FS 1229. REPAIRED PER M/M 53-11-0.Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980460Web · crackedFOUND DURING B-2 LETTER CHECK, LWR RT TORQUE BOX VERTICAL WEB CRACKED FS 1214. REPAIRED PER M/M 53-11-0.Feb 23, 1998 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980459Bracket · crackedFOUND AT B2 LETTER CHECK, NR 2 LE FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER EDGE. REPAIRED PER M/M 57-20-21.Feb 23, 1998 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W980018Pbe · defectivePBE RED INDICATOR EXTENDED PASSED FLUSH. REPLACED PBE.Jan 2, 1998 · N2814W · Boeing 727247 · Portable Oxygen SystemSDR DL72W971939Light · inoperativeRT OVERWING EXIT FWD CENTER AISLE AND AFT RT EXTER FAIRING EMERGENCY LIGHT INOP.Sep 30, 1997 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W971561Line · leakingSYSTEM 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.Aug 8, 1997 · N2814W · Boeing 727247 · Hydraulic System, MainSDR DL72W962659Angle · crackedFOUND 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.Dec 6, 1996 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W961200Stiffener · crackedFOUND 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.May 17, 1996 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W961199Doubler · damagedDOUBLER DAMAGED LOWER RUDDER LOWER RT HINGE AREA. REPLACED RUDDER PER SRM 55-2-3.May 17, 1996 · N2814W · Boeing 727247 · Rudder StructureSDR DL72W954754Line · leakingLOSS 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 ANDec 22, 1995 · N2814W · Boeing 727247 · Hydraulic System, MainSDR DL72W954457Skin · damagedDURING SHOP INSPECTION, RT ELEVATOR WAS REPAIRED FOR DAMAGE TO LOWER SKIN AT ACCESS ANGLE 9, PER SRM 55-20-3.Nov 20, 1995 · N2814W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W954438Ribs · crackedRIBS 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.Nov 19, 1995 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W954541Rib · crackedTHE 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 Nov 17, 1995 · N2814W · Boeing 727247 · Wing, Rib/BulkheadSDR DL72W954426Skin · damagedRT 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 FINov 17, 1995 · N2814W · Boeing 727247 · Rudder, Plate/SkinSDR DL72W954405Skin · damagedDURING 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 ONov 15, 1995 · N2814W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W954403Skin · damagedDURING 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 Nov 15, 1995 · N2814W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W954739Doubler · carckedDURING 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.Nov 14, 1995 · N2814W · Boeing 727247 · Trailing Edge FlapsSDR DL72W954245Stringer · crackedATL - HMV, HFEC INSP OF WS 686.50 STR 9 HAS A CRACK EXITING FASTENER HOLE AWAY FROM RADIUS. REPAIRED PER MM 57-13-0.Nov 2, 1995 · N2814W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W954240Stringer · crackedAT 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.Nov 2, 1995 · N2814W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W954221Skin · damagedSPOILER 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.Nov 2, 1995 · N2814W · Boeing 727247 · SpoilersSDR DL72W954275Rib · crackedDURING 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.Oct 31, 1995 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W954261Vertical Beam · crackedATL - 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. THISOct 26, 1995 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W954394Angle · crackedAT 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.Oct 22, 1995 · N2814W · Boeing 727247 · Fuselage Miscellaneous Structure
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