N410DA, cancelled Jul 20, 2010

Service difficulty reports · 63

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 = 'N410DA' AND deregistration_id = 'N410DA-2010-07-20'
  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 DL72S030143Skin · damagedUPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD.Feb 11, 2003 · N410DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S011025Warning Light · false indicationR-2 DOOR IND ILLUM ON T/O ROLL. ABORTED T/O BELOW 100 KTS. INSPECTED DOOR, NO PROBLEM NOTED. DOOR OPS NORM. CYCLED NUMEROUS TIMES, UNABLE TO DUPLICATE.Jun 21, 2001 · N410DA · Boeing 727232 · Door Warning SystemSDR DL72S010516Angle · cracked1/2 INCH CRACK IN NR 8 L/E SLAT COVE SKIN ANGLE AT ANTI-ICE DUCT CUTOUT REPAIRED PER MM 57-54-000-8Mar 29, 2001 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K001734Sign · inoperativeFOUND AFT SERVICE DOORS OVERHEAD EXIT SIGN IN AFT GALLEY. REINSTALLED EXIT SIGN. LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY PACK AND BASE, NO HELP. FOUND WIRE BROKEN ON EXIT SIGN. REPAIRED WIRE. SIGN OPS NORMAL NOW.Sep 8, 2000 · N410DA · Boeing 727232 · Emergency LightingSDR DL72K001291Relay · failedAFTER TAKEOFF PRESSURIZATION AUTO FAILED TO STBY. ATTEMPTED OPERATION IN STBY AND MANUAL. CABIN DIDN''T PRESSURIZE. FOUND PACK VALVE C/B POPPED. LEVELED AT 8,000 FT, CABIN ALT 8,000. PSI DIF. ISOLATED POPPING C/B TO R23 RELAY. REPLACED BOTH R23 AND R22 RJul 7, 2000 · N410DA · Boeing 727232 · Cabin Pressure ControllerSDR DL72K000920Pump · damagedAS ENG POWER WAS ADVANCED FOR TAKEOFF NR 1 ENG FLAMED OUT. EPR ON NR 1 ENG REACHED 1.3 BEFORE ENGINE INST. ROLLED BACK, NO TAKEOFF WAS INITIATED. FOUND ENG FUEL PUMP SHEARED. REPLACED SAME AND ENG FUEL CONTROL.May 8, 2000 · N410DA · Boeing 727232 · Engine Fuel PumpSDR DL72K000769Sign · inoperativeAFT EMERGENCY EXIT SIGN INOP AT CENTER AISLE STA 1046. REPLACED BATTERY RACK, CKS NORMAL.Apr 20, 2000 · N410DA · Boeing 727232 · Emergency LightingSDR DL72K000728Frame · crackedA PREVIOUS REPAIR WAS FOUND ON THE FS 910 FRAME AT STR 18A ON THE RIGHT SIDE OF THE AIRCRAFT. THE REPAIR WAS REMOVED, INSPECTED AND A NEW REPAIR INSTALLED PER ERA 334253-14. THE DAMAGE WAS FOUND AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K000727Frame · corrodedCORROSION WAS FOUND ON THE FS 1142.7 CARGO DOOR OPENING FRAME ON THE FORWARD SIDE OF THE WEB. THE CORROSION WAS BLENDED AND A DOUBLER INSTALLED PER ERA 334273-14 AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K000723Skin · gougedA GOUGE WAS FOUND IN THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-2 DOOR AT FS 990. THE DAMAGE WAS LOCATED APPROX 1 INCH ABOVE STRINGER 24R. THE SKIN, DOUBLER AND TRIPLER WERE TRIMMED, INSPECTED AND TREATED PER ERA 334268-14. THE DAMAGE WAS FOUND AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000668Door Frame · crackedTHE RT FRAME OF THE AFT ENTRY DOOR WAS FOUND CRACKED IN THE FORWARD FLANGE AT WL 276. THE BEAM WAS CUT AND A NEW SECTION SPLICED IN PER ERA 334236-14. THE DAMAGE WAS FOUND AT HMV.Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K000667Frame · wornTHE FS 1148 FRAME INNER CHORD WAS WORN AT STRINGER 5R. THE DAMAGE WAS BLENDED SMOOTH AND A REPAIR WAS INSTALLED PER ERA334258-14. THE DAMAGE WAS FOUND AT HMV.Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K000656Stiffener · crackedCRACKS WERE FOUND ON BOTH THE LBL 8 AND RBL 8 STIFFENERS OF THE 1183 BULKHEAD AT WL 182. THE CRACKS ARE IN THE TYPICAL LOCATIONS AS THOSE DESCRIBED IN S/B 727-53-0175. THE S/B REPAIR WAS INSTALLED PER ERA 334276-14AD AT HMV.Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K000655Skin · crackedA CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK IS THROUGH THE SKIN, DOUBLER AND BEARSTRAP AND IS APPROXIMATELY 2 INCHES LONG. THE CRACK WAS CUT OUT AND REPAIRED PER ERA 334242-14 WITH AND EXTERNAL REPAIR DOUBLER AND TRIPLER. THE Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000654Skin · gougedA GOUGE WAS FOUND IN THE FUSELAGE SKIN AT FS 360 BETWEEN STRINGER 17L AND 18L JUST BELOW AND AFT OF THE L1 DOOR CUTOUT. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED AT HMV PER ERA 334256-14.Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000589Skin · crackedSEVERAL CRACKS WERE FOUND IN THE LAP JOINT OF THE FUSELAGE SKIN AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE LAP JOINT WAS REPLACED PER ERA 334230-14AD AT HMV.Mar 28, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000568Beam · corrodedDURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS AND WEAR AT THE FWD ATTACH LUGS AND TOGGLE DETENT HOLE. REPAIR PER ER/A 387256-14AD AND BF GOODRICH REPAIR NR 23-0592.Mar 24, 2000 · N410DA · Boeing 727232 · Wing, Attach FittingsSDR DL72K000753Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 3 PLACES. A SECTION OF THE ANGLE WAS REPLACED AND NEW SECTION SPLICED IN PER MM 5752-01, FIG 802.Mar 23, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K000638Skin · wornAT HMV THE 5 SLAT LEADING EDGE WAS FOUND WORN AT FENCE. DRILLED REPAIR DOUBLER PER MM 57-54-0. DYE PEN INSP AREA UNDER FENCE FOUND 2 CRACKS STOP DRILLED. INSTALLED DOUBLER PER MM 57-54-0 FIG 817.Mar 23, 2000 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K000585Rib · crackedNR 5 SLAT I/B RIB CRACKED. INSTALLED REPAIR DOUBLER PER B727 MM 57-54-0, FIG 814.Mar 23, 2000 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K001976Skin · damagedDURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B LOWER CORNER. THE SKIN WAS REPAIRED PER 727 M/M 57-52-0 FIG 803, BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND SKIN FILLER.Mar 22, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K000641Skin · wornAT HMV THE SKIN ON 4 L/E SLAT WAS WORN ON UPPER AND LWR SURFACES I/B TRACK. AREA BURNISHED REPAIR DOUBLER MANUF INSTALLED DOUBLER PER MM 57-54-0 FIG 813.Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K000640Rib · crackedAT HMV A RIB WAS FOUND CRACKED ON 4 L/E SLAT I/B END. REPAIRED PER 57-54-0 FIG 814.Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K000639Rib · crackedAT HMV 4 L/E SLAT RIB WAS FOUND CRACKED ON O/B END. REPLACED PER MM 57-54-0 FIG 814. DYE CHECKED, FOUND NO CRACKS.Mar 22, 2000 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K000756Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. A SECTION OF THE ANGLE WAS REPLACED AND SPLICED TO OLD SECTION PER MM 57-52-0, FIG 802.Mar 21, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K000755Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED. THE CHORD WAS REPAIRED PER MM 57-52-0, FIG 802.Mar 21, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K000744Rib · crackedDURING SHOP VISIT THE I/B AFT RIB WAS FOUND CRACKED IN THE LOWER RADIUS AT THE AFT END. THE CRACK WAS STOP DRILLED AND A DOUBLER INSTALLED PER 727 MM 57-52-0, FIG 808.Mar 20, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K000624Skin · crackedAT HMV THE VERT SKIN WAS CRACKED AT PANEL 9523 LT FWD SIDE OF VERT STAB. REPAIR WAS FABRICATED PER MM 54-30-0 FIG 903 AND REPAIR WAS INSTALLED.Mar 20, 2000 · N410DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72K000621Panel · damagedAT HMV A TEMP REPAIR WAS INSTALLED ON LT SIDE OF VERT STAB AT L/E STA 1298 JUST FWD OF L/E PNL 9525. TEMP REPAIR WAS REMOVED AND DAMAGE CUT OUT AND PERM REPAIR INSTALLED PER MM 54-30-0 FIG 802.Mar 20, 2000 · N410DA · Boeing 727232 · Vertical StabilizerSDR DL72K000580Flap Track · corrodedHMV- ATTACH LUG HOLE FORWARD FITTING MLG WING DOOR CORRODED. REPAIRED PER MM 57-43-01.Mar 20, 2000 · N410DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K991576Skin · crackedFUSELAGE SKIN FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 29 CRACKS ALONG Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K991575Skin · crackedFUSELAGE SKIN FS 480-500, STRG 4L, SKIN LAP SPLICE, CRACK REPAIR. HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A SINGLE CRACK BETWEEN FS 480 AND 500. THE CRACK WAS CUTOUT OF THE SKJul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K991574Skin · crackedFUSELAGE SKIN FS 700-720, STRG 4R, SKIN LAP SPLICE : CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEJul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K991573Skin · crackedFUSELAGE SKIN FS 720A-720B, STRG 4R SKIN LAP SPLICE CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 7Jul 11, 1999 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K991111Light · inoperativeL2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.May 19, 1999 · N410DA · Boeing 727232 · Emergency LightingSDR DL72K990966Angle · corrodedWHILE PERFORMING HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLES CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLES WITH ANGLES OF NEW MFG.Apr 30, 1999 · N410DA · Boeing 727232 · Engine Mount SectionSDR DL72K990740Angle · crackedA .25 INCH CRACK ON ANGLE FWD SIDE OF FS 910 RT ABOVE AND FWD OF H BRACKET. REPAIRED PER MM 53-11-0, TIME LIMITED REPAIR.Apr 5, 1999 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K990512Actuator · leakingON WALKAROUND INSPECTION, FOUND NR 14 SPOILER ACTUATOR LEAKING.Mar 11, 1999 · N410DA · Boeing 727232 · Drag Control ActuatorSDR DL72K981031Skin · damagedDURING BUYBACK OF N/R 218, FOUND NUT PLATE EMBEDDED AT RT ELEVATOR LOWER SKIN. SKIN HAS .3125 INCH IN HOLE REPAIRED PER SRM 55-20-3.May 12, 1998 · N410DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72K980992Stringer · crackedTHE OUTER CHORD OF THE STRINGER 17L CREASE BEAM WAS FOUND WITH A .5 CRACK AT STA 848.95. THE CRACK WAS IN THE HORIZONTAL FLANGE OF THE TEE WHERE THE FLANGE WAS MILLED AWAY TO PASS UNDER THE FRAME. THE CRACK WAS ROUTED OUT OF THE HORIZONTAL FLANGE AND STOP May 8, 1998 · N410DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72K981030Rear Spar · crackedAN .375 INCH CRACK RT ELEVATOR REAR SPAR AT 2ND FROM O/B TAB, HINGE. REPLACED REAR SPAR UNDER EO 4-70183-3AD ME 02 AND ME 03.May 4, 1998 · N410DA · Boeing 727232 · Elevator, Spar/RibSDR DL72K980894Bear Strap · crackedFUSELAGE/SKIN ASSY, R1 DOOR SURROUND DOUBLER, UPPER HINGE CUTOU. REPAIR FOR CRACK IN REINFORCING DOUBLER. THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN THE UPPER HINGE CUTOUT. THE CRACK WAS IDENTIFIED AS BEING IN RApr 26, 1998 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K980950Skin · crackedTHREE EACH .125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER MM 54-30-0.Apr 22, 1998 · N410DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72K980937Floorbeam · corrosionCORROSION FLOORBEAM STA 1030 BL 0. REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-20-11.Apr 21, 1998 · N410DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72K980914Bear Strap · crackedFOUND ON MV2 CORROSION VISIT, CRACK IN EDGE OF BEARSTRAP AT RT FWD SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REFERENCE SUPPLEMENTAL CARD FOR SI 4-72762-12 ME-02. REPAIRED PER ERA 364614-14 REV A.Apr 21, 1998 · N410DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K981029Bracket · crackedNR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812.Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge DevicesSDR DL72K980902Stringer · crackedFOUND ON MV2 CORROSION VISIT, 1 VISABLE CRACK STR 18A RT, AFT OF STA 940 FITTING UPPER AFT ATTACH BOLT. REPAIRED PER M/M 53-12-0.Apr 20, 1998 · N410DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72K980900Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21.Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72K980899Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72K980898Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21.Apr 20, 1998 · N410DA · Boeing 727232 · Leading Edge Slat Actuator
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