N531DA, cancelled Nov 8, 2006

Service difficulty reports · 59

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 = 'N531DA' AND deregistration_id = 'N531DA-2006-11-08'
  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 DL72S020493Wedge · delaminatedOUTBOARD MIDFLAP TRAILING EDGE DELAMINATION. REPAIRED PER ER/A 417248-14.Apr 29, 2002 · N531DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S020181Battery Pack · dischargedDURING L/O FOUND 1ST CLASS OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY.Feb 13, 2002 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S020149Battery · dischargedEMERGENCY LIGHT ABOVE SEAT 3B INOP. REPLACED BATTERY.Feb 7, 2002 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S011661Battery Pack · dischargedLT FWD O/W SLIDE LIGHT INOP. REPLCD BATT PACK. OPS CKS GOODOct 12, 2001 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S011659Compressor · stalledAT APPROX 80 KTS WITH POWER STABILIZED, AT45 (194/197/194) WINDS 170/17, AIRSPEED AT 90 KTS NR 2 ENG COMPRESSOR STALLED. EPR DROPPED TO APPROX 1.70 AND RECOVERED. PERFORMED BORESCOPE AND COMPRESSOR WASH, NO DAMAGE FOUND.Oct 12, 2001 · N531DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72S011522Module · damagedON LANDING ROLLOUT HYD SYS -A- PRESS AND QTY WENT TO ZERO. FOUND -A- SYS ELEV CONTROL MODULE DAMAGED. SOLENOID BLEW OUT OF THE TOP OF MODULE. REPLACED MODULE.Sep 9, 2001 · N531DA · Boeing 727232 · Elevator Control SystemSDR DL72S011513Filter · dirtySYSTEM A O-HEAT LIGHT CAME ON JUST PRIOR TO CRUISE. REPLACED A-SYSTEM RETURN FILTER MODULE.Sep 9, 2001 · N531DA · Boeing 727232 · Hydraulic Filter, MainSDR DL72S011061Battery · dischargedRIGHT EXT OVERWING EXIT LIGHT INOP. REPLACED BATTERY, OP CHECKS GOOD.Jun 25, 2001 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S010780Line · looseDURING CRUISE AND DESCENT NR 2 ENG OIL QTY SLOWLY DECREASED FROM 3.2 TO 0 GAL. OIL TEMP AND PRESS IN GREEN ARC. ON FINALOIL PRESS BEGAN TO FLUC AND DROPPED OUT OF GREEN W/LOW OIL PRESS LIGHT ILLUM. IN FLT SHUTDOWN CK COMPLETED. REPLACED MAIN OIL FILTER. IMay 16, 2001 · N531DA · Boeing 727232 · Turbine Engine Oil SystemSDR DL72S010551Indicator · stuckUPON FLAP RETRACTION OUTBOARD FLAPS REMAINED AT 5 DEG. INBOARD WENT TO 2 DEG. AND L/E FLAP LIGHT REMAINED AMBER. RAN CHECK LIST. REPLACED OTBD FLAP INDICATOR. RAN FLAPS SEVERAL TIMES OPERATION CKS OK.Apr 3, 2001 · N531DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S001694Wire · shortedAFTER TAKEOFF INBOARD FLAPS FROZE AT 15. ACCOMPLISHED T/E FLAP ABNORMAL PROCEDURE. THE INBOARD RIGHT NEEDLE GRADUALLY SPLIT AND WENT DOWN TO 38 DEGREES. AIRTURN BACK TO DFW. FOUND INBOARD FLAP POSITION INDICATION CIRCUIT BREAKER TRIPPED. LOCATED SHORT IN Sep 1, 2000 · N531DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S001099Stringer · crackedTHE LEFT STRINGER 18A WAS FOUND CRACKED AT FS 940. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED AND AN HFEC WAS OF THE FUSELAGE SKIN WAS ACCOMPLISHED REVEALING A CRACK. THE CRACK IN THE SKIN WAS CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED. THEN A NEWJun 6, 2000 · N531DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S001053Flap Track · corrodedNR 4 I/B FLAP TRACK OF THE I/B FLAP WAS FOUND WITH CORROSION AND WEAR WHICH MEASURED BEYOND SRM AND OHM LIMITS. THE MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, THE SPOILER BEAM ATTACH BOLT HOLES, THE MLG DOOR FWD AND AFT HINGE FITTING HOLES, THE RADIUS BLOCK ATMay 30, 2000 · N531DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S001028Flap Track · corrodedINBOARD FLAP, NR 5 INBOARD TRACK CORROSION FOUND ON MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, THE SPACER BAR ATTACH BOLT HOLE, AND THE TOGGLE DETENT HOLE. REPAIR PER ER/A 387640-14AD AND BFGOOFRICH ENGINEERING REPAIR NR 23-0801.May 25, 2000 · N531DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S001031Web · crackedAT HMV2, CONTIN OF N/R 519. CHEM TREAT PER PIS 900-2-4-1 NR 2, PAINTED PER PS 900-3-6 NR 3, OK TO INSTALL LT & RT REPAIRS, INSTALLED LT & RT DOUBLERS PER SRM 53-10-4D FIG 802D.May 23, 2000 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001011Skin · crackedA CRACK WAS FOUND IN THE STR 4L LAP JOINT BETWEEN FS 460 AND FS 480 AT HMV. THE CRACK WAS REPAIRED SIMILIARLY TO THAT OF SRM 53-30-3, FIG 5 PER ERA 334481-14AD.May 23, 2000 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S001010Skin · crackedSEVERAL CRACKS WERE FOUND IN THE STR 4R LAP JOINT BETWEEN FS 700 AN DFS 720. THE DAMAGE WAS REPAIRED SIMILIARLY TO THAT OF SRM 53-30-3, FIG 5 PER ERA 334480-14AD AT HMV.May 23, 2000 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S001009Skin · crackedMULTIPLE CRACK LOCATIONS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 481 AND 681. THE LAP JOINT WAS REPLACED PER ERA 334469-14AD AT HMV.May 23, 2000 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S001019Flange · gougedAT HMV, THE NR 2 FIREWALL AFT FLANGE WAS FOUND TO BE WORN/GOUGED AT THE 6 O''CLOCK POS. IT WAS CHEMICALLY TREATED PER PS 900-2-4-1 NR 2 AND REPAIRED PER MM 53-11-0 PG 801.May 16, 2000 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S001020Cowling · wornAT HMV, THE NR 2 FIREWALL COWL LANDING WAS FOUND TO BE WORN. IT WAS REPAIRED PER MM 53-11-0 PG 801.May 15, 2000 · N531DA · Boeing 727232 · Engine Cowling SystemSDR DL72S001061Frame · crackedAT HMV STRINGER 14RT STA 920 FRAME WAS FOUND TO BE CRACKED. REMOVED DAMAGED SECTION FORMED ANGLE PER SRM 53-10-4 FIG 806D. CHEM TREATED PER PS 900-2-4-1. INSTALLED REPAIR IAW SRM 53-10-4 FIG 806D.May 12, 2000 · N531DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S001057Shear Tie · corrodedAT HMV2 FOUND AFT B/B SHEAR TIE CORRODED AT FS 1166 FROM STR 28L TO 28R. REMOVED FASTENERS TO GAIN ACCESS TO CORRODED AREA, CORROSION ON SHEAR TIE FROM STR 29-28 OUT OF LIMITS AND FRAME WEB BELOW FAIL-SAFE CHORD OUT OF LIMITS AS PER SRM 53-10-1 FIG 1. REMOVEMay 12, 2000 · N531DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S001001Spar · crackedSPAR CRACKED. NR 8 L/E SLAT, FWD SPAR AT TAI DUCT. REPAIRED SLAT PER MM.May 10, 2000 · N531DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992367Angle · crackedNR 8 SLAT ACTUATOR O/B ATTACH ANGLE WAS CRACKED. REPAIRED PER MM 57-20-21.Oct 25, 1999 · N531DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S992366Bracket · crackedTPA LTR CHK F-2, 1 VISIBLE CRACK O/B ATTACH BRACKET NR 1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21.Oct 25, 1999 · N531DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S991985Rod · brokeAFTER T/O, DURING GEAR RETRACTION, GOT A LOUD SNAP WITH A VIBRATION AND A RED GEAR DOOR ON FWD PANEL AND NLG DOOR LIGHT ON S/O PNL. REPLACED NOSE GEAR ACT ROD. SWUNG NOSE GEAR GEAR AND DOORS OPERATE NORMAL.Sep 7, 1999 · N531DA · Boeing 727232 · Landing Gear Door Retract SectionSDR DL72S991854Accessory Unit · malfunctionedON SHORT FINAL, THE LANDING GEAR WARNING HORN SOUNDED AS FLAPS WERE SET TO 30 DEG. GEAR DOWN AND INDICATION NORMAL. SPEED BRAKE STOWED. HORN STOPPED DURING GO-AROUND AS FLAPS WERE RETRACTED PAST 30 DEG. REPLACED LANDING GEAR ACCESS UNIT PER M/M 32-09-121. Aug 18, 1999 · N531DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S990667Clamp · brokenAFTER PUSHBACK, HEARD LOUD BANG AND EXPERIENCED SMOKE IN CABIN. FOUND CLAMP OFF DUCT IN AREA OF FLOW MULT REF IPC 21-10-0-4 ONLY AFFECTS AIR FROM APU. PUT APU AIR TO MCO AND PLACARD.Mar 26, 1999 · N531DA · Boeing 727232 · Pneumatic Distribution SystemSDR DL72S990577Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON THE S26L LAP JOINT, CRACK INDICATIONS WERE NOTED BETWEEN BS 480 AND BS 681. HFEC INSPECTIONS CONFIRMED 4 CRACK INDICATIONS. ADDITIONALLY, A 2.5 INCH CRACK RUNNING FWD/AFT WAS NOTED AT S25L AT BS 540Mar 16, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990552Rib · crackedTHE UPPER CHORD ANGLE OF THE LEFT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED AT A FASTENER HOLE ON THE HORIZONTAL FLANGE OF THE CHORD ANGLE UNDER S16. REPAIRED PER ERA 332872-14, REV B.Mar 16, 1999 · N531DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72S990529Skin · corrodedCORROSION WAS FOUND UNDER S28L AT BS 1010 AT THE SKIN BUTT JOINT. REPAIRED PER ERA 332920-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990528Stringer · crackedFUSELAGE STRINGER 29R WAS FOUND CRACKED 2 FWD OF BS 950E. ADDITIONALLY, CORROSION WAS NOTED 2 AFT OF BS 950D. A SECTION OF STRINGER FROM BS 950D+10 TO BS 950E+10 WILL BE CUT OUT AND REPLACED. REPAIRED PER ERA 332882-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S990527Frame · wornSTATION 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE AT S22L DUE TO CONTACT WITH A HYD LINE. REPAIRED PER ERA 332918-14.Mar 12, 1999 · N531DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990485Skin · wornTHE UPPER SKIN OF THE S19R LAP SPLICE WAS FOUND TORN AT BS 720E-5 DUE TO MISALIGNMENT OF THE WING TO BODY FAIRING UPON INSTALLATION. REPAIRED PER ERA 332901-14AD, REV A.Mar 9, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990451Beam · crackedCRACK IN L-1 LOWER BEAM AFT CORNER HFEC TO CONFIRM CRACK MARK ENDS. FABRICATED REPAIR DOUBLER PER M/M 52-11-01 FIG 803. STOP DRILLED CRACK AT MARKED ENDS. INSTALLED PER M/M 52-11-01 FIG 803. COMPLETED INST PER M/M 52-11-01 FIG 803.Feb 26, 1999 · N531DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S990448Stringer · crackedRT WING STR-TO-RIB INSP AT WS 686.5 STRINGER 8 SHOWS CRACK INDICATION, MARKED (AFT UPPER STR). LOOSENED FUEL DUMP LINE FOR ACCESS, BEGAN DRILLING UP REPAIR PER M/M 57-13-0 FIG 802. STOP DRILLED CRACK REPAIR PER M/M 57-13-0 FIG 802. INSTALLED REPAIR PER M/M Feb 26, 1999 · N531DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S990446Stringer · crackedLT WING UPPER STR-TO-RIB HOLE INSP, SHOWS CRACK INDICATION WS 686.5 STRINGER 11. CUT ACCESS HOLE IN STRINGER, BEGAN DRILLING UP RADIUS BLOCKS. STOP DRILLED CRACK, REMOVED FUEL VENT TUBE FWD OF STRINGER 12 AT WS 686.5 TO FOM, REMOVED FUEL PROBE HARNESS STANDOFeb 26, 1999 · N531DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S990044Wire · shortedFOUND DURING L/O CHECK, EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 19 AND 26 INOP. REPAIRED WIRING.Jan 8, 1999 · N531DA · Boeing 727232 · Light System WiringSDR DL72S982627Bulb · failed5 LIGHTS BAD AT AFT STAIR CASE, RELAMPED.Dec 25, 1998 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S972726Battery · dischargedEMERG LIGHT ABOVE AFT AIRSTAIRS INOP. REPLACED BATTS AND CKS GOOD.Dec 24, 1997 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S972587Beam · crackedTHE AFT GUSSET AND HORIZONTAL BEAM AT FS 1273 ON THE VENTRAL STAIRWAY TORQUE BOX WERE FOUND CRACKED PER INSPECTIONS OF S/B 53-0129 AS MANDATED BY AD 94-07-08. THE CRACKED PARTS WERE REPLACED PER S/B 53-0129 AS DOCUMENTED IN ER/A 363353-14AD.Dec 4, 1997 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971788Battery Pack · dischargedEMERGENCY EXIT LIGHT MOUNTED ON CEILING OF CABIN IN BETWEEN OVERWING EMERGENCY EXITS BLINKS INTERMITTENTLY DURING TEST. REPLACED BATTERY PACK.Sep 12, 1997 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S970883Web · crackedFOUND ON D2 LETTER CHECK, .25 INCH CRACK RT LOWER TORQUE BOX WEB AT A LIGHTING HOLE STA 1246. REPAIRED PER MM 53-11-0.May 8, 1997 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961988Wire · chafedON SERVICE CHECK, FOUND MID-FRONT EMERGENCY TRACK LIGHTS AND ALL FOUR OVERWING EMERGENCY EXIT IDENT LIGHTS INOPERATIVE. FOUND WIRE SHORTED AT SIDEWALL WHERE TRACK LIGHT WIRES PASS THROUGH. REPAIRED SAME. LIGHTS NOW TEST OK.Aug 10, 1996 · N531DA · Boeing 727232 · Light System WiringSDR DL72S961579Angle · crackedTHERE IS A ONE INCH CRACK IN THE ANGLE OF THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THE REPAIR REPLACES THE DAMAGED PARTS IN ACCORDANCE WITH S/B 53-0129.Mar 7, 1996 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960508Angle · crackedFOUND DURING C-2 LETTER CHECK - 2 INCH CRACK NR 4 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.Mar 6, 1996 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960311Identifier · inoperativeDURING LAYOVER CHECK, AFT CABIN DOOR EMERGENCY EXIT IDENTIFIER INOP ON TEST. REPLACED AFT CABIN DOOR IDENTIFIER AND REPAIRED BROKEN WIRE AT D9069P.Feb 9, 1996 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S960310Battery Pack · inoperativeDURING LAYOVER CHECK, FOUND FWD AND AFT BULLNOSE EMERGENCY LIGHTS WOULD NOT TEST. REPLACED BATTERY PACK AT FWD 1088 AND REPLACED BATTERY PACK AT AFT 1089, NOW CHECKS OK.Feb 9, 1996 · N531DA · Boeing 727232 · Emergency LightingSDR DL72S960021Skin · corrosionTHE FUSELAGE SKIN AT STA 500 STR 28R WAS DAMAGED BY CORROSION AND A 13.5 INCH BY 3.5 INCH SECTION WAS CUTOUT. A SKIN REPAIR WAS ACCOMPLISHED PER B727 SRM 53-30-3 FIG 3, EXCEPT THE DOUBLER WAS EXTENDED FORWARD TO STA 480 BUTT JOINT. REPAIRS ACCOMPLISHED PER DDec 20, 1995 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954731Rib · crackedFOUND ON CV2 CHECK TRANSFERRRED FROM N/R 33 ITEM NR 2, .4375 INCH CRACK AT NR 6 SLAT NOSE RIB INBD SIDE OF ACTUATOR. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.Dec 12, 1995 · N531DA · Boeing 727232 · Leading Edge Devices
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