N2809W, cancelled Feb 29, 2000

Service difficulty reports · 47

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 = 'N2809W' AND deregistration_id = 'N2809W-2000-02-29'
  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 DL72W991954Angle · crackedNR 6 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED ANGLE PER M/M 57-20-21 PAGE 813.Sep 2, 1999 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W991953Bracket · crackedNR 8 SLAT ACTUATOR I/B AND O/B MOUNT BRACKETS CRACKED ON WEBS. REPAIRED PER M/M 57-20-21 PAGE 812.Sep 2, 1999 · N2809W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W991951Web · crackedFOUND ON F1 LETTER C, .25 INCH CRACK LOWER LIGHTENING HOLE RT VERTICAL TORQUE BOX WEB STA 1260. REPAIRED PER MM 53-11-0.Sep 2, 1999 · N2809W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W991802Cadc · failedAFTER T/O CAPTAINS MACH INDICATOR DISPLAYED AN OFF FLAG. ALSO, CAPTAINS ALTIMETER HAD A STANDBY FLAG ALSO NEITHER TRANSPONDER DISPLAYED MODE C TO ATL. REPLACED NR 1 CADC CHECKED NORMAL.Aug 12, 1999 · N2809W · Boeing 727247 · Air Data ComputerSDR DL72W982637Skin · crackedTHE UPPER FUSE SKIN AT BS 351 ON THE UPPER ROW OF THE S24R LAP SPLICE WAS FOUND CRACKED. THE CRACK EXTENDED THRU THREE CONSECUTIVE FASTENERS WITH A TOTAL LENGTH OF 3. REPAIRED PER ERA 366371-14.Dec 28, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W982181Light · inopCOCKPIT OVERHEAD EMERGENCY LIGHT PACK INOP ON TEST. REPLACED BATTERIES, CKS OK.Oct 21, 1998 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W982110Light · illuminatedAFTER GEAR EXTENSION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN NOSE GEAR LIGHT. POM PROCEDURES COMPLIED WITH AND A SAFE INDICATION OBTAINED AFTER MANUAL EXTENSION PROCEDURES ACCOMPLISHED.Oct 11, 1998 · N2809W · Boeing 727247 · Landing Gear Position and WarningSDR DL72W981658Sequence Valve · crackedDURING CLIMBOUT, LOST 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID QTY. FOUND RIGHT MLG DOOR SEQUENCING VALVE CRACKED. REPLACED VALVE. LEAK CHECK AND GEAR SWING GOOD.Aug 11, 1998 · N2809W · Boeing 727247 · Landing Gear Retraction/Extension SystemSDR DL72W981401Battery Rack · dischargedSEAT ROW 18 ABCDEF OVERHEAD EMER LIGHT INOP. REPLACED BATTERY RACK OPS NOW NML.Jul 2, 1998 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W981393Skin · crackedFUSELAGE BELLY SKIN WAS FOUND WITH CRACKS AND CORROSION AT STA 700 AND STR 28L - 28R. BELLY SKIN WILL BE REPLACED DUE TO NUMEROUS EXISTING REPAIRS. REPAIRED PER ERA 303637-14.Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W981384Skin · gougedFUSELAGE SKIN WAS GOUGED FWD OF THE L1 DOOR AT S10L LAP SPLICE. REPAIRED PER ERA 331851-14.Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W981383Stringer · corrodedFUSELAGE STRINGER 29R WAS FOUND WITH CORROSION AT FS 950E PLUS 10. A NEW SECTION OF STRINGER IS SPLICED IN. REPAIRED PER ERA 331848-14.Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W981382Spar Chord · crackedFRONT SPAR UPPER CHORD WAS FOUND WITH A CRACK IN THE FORWARD FLANGE AT A FASTENER HOLE AT APPROX WL340. REPAIRED PER ERA 331817-14.Jun 29, 1998 · N2809W · Boeing 727247 · Wing SparSDR DL72W981381Stringer · corrodedSTRINGER 29L WAS FOUND CORRODED. THE STRINGER WAS TRIMMED AT STA 950D+10 AND THE AFT PORTION REMOVED. REPAIRED PER ERA 331787-14.Jun 29, 1998 · N2809W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W981214Frame · crackedFS 784 FRAME ON THE LT SIDE HAD TWO CRACKS AT THE SECOND HOLE UP FROM THE FLOOR LINE. REPAIRED PER ERA 331783-14AD.Jun 8, 1998 · N2809W · Boeing 727247 · Fuselage Main, FrameSDR DL72W981225Actuator · looseNR 13 SPOILER ACTUATOR MOUNT LOWER INBD AND OUTBD BOLTS ARE LOOSE. REPAIRED MOUNT HOLES IAW MM 57-42-0.Jun 1, 1998 · N2809W · Boeing 727247 · Drag Control ActuatorSDR DL72W981244Trunnion · crackedRT MLG TRUNNION BEAM SUPPORT FITTING AT FS 940 FOUND WITH 1.5 INCH FATIGUE CRACK ON INBRD SURFACE, WL 190. REPAIRED WITH FABRICATED DOUBLER PER ER/A 373040-14. CRACK FOUND DURING MID VISIT INSPECTION.May 29, 1998 · N2809W · Boeing 727247 · Fuselage, Landing Gear Attach FittingsSDR DL72W981354Floorbeam · corrodedREMOVED EXISTING T-CAP REPAIR, FWD AND AFT SPLICE ANGLES, 1 VERTICAL STIFFENER AND 1 FLOORBOARD SUPPORT. REMOVED EXISTING T-CAP FROM C/L TO RBL 52. BEGAN DRILLING NEW T-CAP. COMPLETED FABRICATION OF REPAIR PER SRM 53-10-8 PG 56-57. INSTALLED T-CAP BEAM SPLMay 14, 1998 · N2809W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W980068Engine · bird strikeAIRCRAFT FLEW THROUGH FLOCK OF GEESE. NR 1 AND 2 ENGINES WILL BE REPLACED. NR 3 WILL BE BORESCOPED. NR 6 SLAT WILL BE REPLACED. RADOME AND RADAR ANTENNA WILL BE REPLACED.Jan 9, 1998 · N2809W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W971480Trunnion Ftg · corrosionTHE TRUNNION ATTACH FITTING OUTBOARD CLEVIS AND MATING TEE ATTACH FLANGE HAD CORROSION IN THE BORE. IN ADDITION, THE COUTER SINK THROUGH THE ATTACH FITTING LUG WAS FOUND TO EXTEND ALMOST COMPLETELY THROUGH THE LUG FLANGE. THIS DAMAGE WAS REMOVED BY OVERSIZEDJul 23, 1997 · N2809W · Boeing 727247 · Wing, Landing Gear Attach FittingsSDR DL72W971452Spar Cap · damagedTHE SUBJECT AIRCRAFT EXPERIENCED A COLLAPSE OF THE RT MAIN LANDING GEAR DURING LANDING ROLLOUT. THIS RESULTED IN DAMAGE TO THE RT WING FRONT SPAR LOWER CAP ON THE OUTBOARD END. THE EXTENT OF THE DAMAGE REQUIRED THAT THE LOWER CAP TO BE CUT AT APPROX FS 770 AJul 15, 1997 · N2809W · Boeing 727247 · Wing SparSDR DL72W970760Battery Pack · dischargedLEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS OK.Apr 24, 1997 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W970759Light · inoperativeAFT STAIRS EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CHECKS OK.Apr 24, 1997 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W970638Skin · crackedFOUND A 1.5 IN CRACK RT ELEV LOWER SKIN FWD OF TAB. REPAIRED PER SRM 55-20-3.Apr 9, 1997 · N2809W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W961468Skin · crackedTHE SKIN JUST FWD OF STA 700 BETWEEN STR 28L AND 28R NEAR BL 0 WAS FOUND CRACKED AND CORRODED. REPAIRED WITH A DOUBLER AND TRIPLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-9-57.May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961283Skin · crackedSKIN CORROSION AND CRACK JUST FWD OF STA 700 BETWEEN STRINGERS 28L AND 28R NEAR BL 0. CUTOUT MEASURED 7.5 BY 3.75 INCH. REPAIRED PER DAL ER/A 303637-14, REV A.May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961462Skin · corrosionSKIN CORROSION AT FS 720F AT STR 27R. REMOVED A 1.75 INCH BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730. ERA WILL INCORPORATE BOTH REPAIRS INTO ONE REPAIR.May 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961282Skin · corrodedSKIN CORROSION AT STA 720F AT STRINGER 27R. DAMAGE REMOVAL RESULTED IN A 1.75 BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730, ERA 213172. EXISTING REPAIR REQUIRED THE REMOVAL OF THE CORNER OF THE LWR SKIN AT STA 740 AND STRINGER 26R. REPAIRED PEMay 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961234Floor Beam · corrodedFOUND ON MV1 CK, CORROSION/RIVETS SHEARD AT CABIN FLOOR BEAM STA 1070 AT RT O/B GALLEY FLOOR TRACK. REPAIRED PER M/M 53-20-11 FIG 804.May 15, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W961171Floor Beam · corrodedFOUND CORROSION ON FLOOR BEAM UPPER ANGLE STA 400 RBL 55. REPAIRED PER M/M 53-20-11 PG 811 B.May 14, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W961047Light · inoperativeEMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES.Apr 28, 1996 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W960697Skin · crackedINNER SKIN CRACKED AT NUTPLATES, RIBS 10, 11, 12 AND 13. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W960696Rib · crackedDURING INSPECTION, FOUND NR 6 L/E SLAT WITH INTERNAL SUPPORT RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W960695Rib · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH INTERNAL SUPPORT RIB NR 11 CRACKED. REPAIRED PER MM 57-54-0.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W960592Attach Fitting · brokenLT MAIN LANDING GEAR DOOR OPENED IN FLIGHT. FOUND LANDING GEAR DOOR ACTUATOR ATTACH FITTING BROKEN, IPC 32-10-4 FIG 2 ITEM 250.Mar 16, 1996 · N2809W · Boeing 727247 · Landing Gear Door ActuatorSDR DL72W960321Skin · wornDURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. SPLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801.Feb 13, 1996 · N2809W · Boeing 727247 · AileronsSDR DL72W960320Web · crackedDURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 1.25 INCH CRACK AT STA 294.5, APPROXIMATELY AT WL 170. THE DAMAGED PORTION WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAPS WAS INSTALLED IN ACCORDANCE WITH B727-53-145.Feb 10, 1996 · N2809W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W960309Angle · crackedA 1.5 INCH CRACK AT NR 1 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57 20-21.Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge Slat Control SystemSDR DL72W960308Bracket · crackedFOUND AT LETTER CHECK, NR 6 L/E FLAP ACTUATOR MOUNT BOX CRACKED, I/B SIDE UPPER AND LWR CORNERS. REPAIRED PER MM 57-20-21.Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge Slat Control SystemSDR DL72W960307Stringer · crackedA 1 INCH CRACK THROUGH HORIZ LEG OF STR 18A AND STA 950. REPAIRED PER MM 53-12-0, FOUND AT LETTER CHECK.Feb 9, 1996 · N2809W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W960306Angle · crackedSLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER MM 57-54-0.Feb 9, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W953149Angle · crackedCRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA302097-14AD.Jul 8, 1995 · N2809W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W952850Skin · gougedDURING INSPECTION, FOUND TOOLING DAMAGE TO RT FUSELAGE NOSE AT FS 243.7, APPROXIMATELY HALFWAY UP THE SKIN PANEL. REPAIRED PER SRM 53-30-3 FIG 3.Jun 26, 1995 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W952861Rib · crackedDURING SHOP INSPECTION, NR 3 SLAT PANEL WAS FOUND WITH L/E RIB NR 17 CRACKED. REPAIRED PER MM 57-54-00 FIG 809.Jun 22, 1995 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W952853Bulkhead · mismfgDURING INSPECTION, LT FS 178 BULKHEAD HAD ACCESS HOLE. INSTALLED PER SRM 53-10-9 FIG 3.Jun 22, 1995 · N2809W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W952851Bulkhead · mismfgDURING INSPECTION, FS 178 RT BULKHEAD HAD AN ACCESS HOLE. INSTALLED PER SRM 53-10-0 FIG 3.Jun 22, 1995 · N2809W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W952782Rib · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 9 CRACKED. REPAIRED PER SRM 57-54-0 FIG 805.Jun 22, 1995 · N2809W · Boeing 727247 · Leading Edge Devices
Back to N2809W, cancelled Feb 29, 2000