N511DA, cancelled Jun 13, 2012

Service difficulty reports · 46

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 = 'N511DA' AND deregistration_id = 'N511DA-2012-06-13'
  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 DL72L011164Power Supply · dischargedON STBY POWER FIRST CLASS EMERGENCY EXIT LIGHT INOP. REPLACED PWR SUPPLY.Jul 13, 2001 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L010930Skin · crackedA 0.5 INCH CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN ON THE LT SIDE, AT S-11. CRACK RUNS FROM A FASTENER HOLE AT S-11 AND EXTENDS FWD FOR APPROXIMATELY 0.5 INCH. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER INSTALLED.Jun 8, 2001 · N511DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L010914Bracket · brokenON DEPARTURE HEARD THUMP SOUND ACCOMPANIED BY SHUDDER. SHORTLY AFTER OUTBOARD FLAP STUCK IN 5 DEG RANGE WITH FLAP HANDLE AT 2 DEG. RETURNED TO CVG. FOUND CABLE ATTACH BRACKET BROKEN ON LEFT I/B FLAP O/B TRACK. REPLACED CABLE ATTACH BRACKET AND CABLE DRUM Jun 3, 2001 · N511DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72L010507Battery · dischargedON LAYOVER FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT AT ROW 25 INOP - REPLACED BATTERIESMar 27, 2001 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L010300Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 & 740 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED SEVERAL CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. THE ENTIRE SKIN LAP WAS CUTOUT TO REMOVE ALL CRACKED HOLES. THE JOIFeb 19, 2001 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L010299Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTIONS CONFIRMED 7 CRACKS ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN. THE SKIN LAP WAS CUTOUT TO REMOVE ALL HOLES. THE JOINT WAS REPAIRED WITHFeb 17, 2001 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002118Angle · crackedA 1.25 INCH VISIBLE CRACK ON NR 3 SLAT AT O/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.Oct 26, 2000 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002117Rib · crackedA .75 INCH CRACK IN L/E NOSE RIB OF NR 7 SLAT AT O/B SIDE OF ACTUATOR ATTACH FITTING. REPAIR PER M/M 57-54-0.Oct 26, 2000 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L001629Actuator · leakingA SYS HYD LOSS ON TAKEOFF, FOUND NR 7 LEADING EDGE SLAT ACTUATOR LEAKING FROM AFT SIDE. REPLACED NR 7 LEADING EDGE ACTUATOR.Aug 22, 2000 · N511DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L001438Battery · dischargedCABIN EMERGENCY LIGHTS INOP AFT OF ROW 26. REPLACED BATTERY PACK, CKS GOOD.Jul 30, 2000 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L001343Coffeemaker · odorF/A REPORTED ELECTRICAL SMELL IN AFT GALLEY. FOUND COFFEEMAKER AT FAULT. REPLACED SAME.Jul 17, 2000 · N511DA · Boeing 727232 · Buffet/GalleysSDR DL72L992724Angle · corrodedON HUSH-KIT MOD, FOUND LT NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT AFT MOUNT SUPPORT CHORD ANGLE WITH ONE OF NEW MFG.Dec 13, 1999 · N511DA · Boeing 727232 · Engine Mount SectionSDR DL72L992725Angle · corrodedON HUSH-KIT MOD, FOUND RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH ONE OF NEW MFG.Dec 10, 1999 · N511DA · Boeing 727232 · Engine Mount SectionSDR DL72L992540Antiskid Module · splitWHILE STOPPED ON THE TAXI WAY DURING TAXI OUT WITH BRAKES SET. A/C STARTED TO ROLL. S/O NOTED 'B' SYSTEM PRESSURE DROPPING TO ZERO WITH BOTH HYD B LIGHTS ON. FOUND RT ANTI-SKID MODULE CASE BROKEN IN TWO AT FILTER CASE. REPLACED MODULE.Nov 16, 1999 · N511DA · Boeing 727232 · Hydraulic System, MainSDR DL72L992084Skin · damagedUPPER RUDDER DAMAGED TORN 2 INCHES BY 7 INCHES AT L/E RUDDER STA 180 TO 187. DRILLED UP REPAIR PER SRM 55-20-3 FIG 1. INSTALLED REPAIR PER SRM 55-20-3.Sep 16, 1999 · N511DA · Boeing 727232 · Rudder, Plate/SkinSDR DL72L992085Skin · corrodedTHE LOWER SKIN OF THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH A 5 INCH LONG AREA OF CORROSION OVER THE UPPER TWO FASTENER ROWS. THE CORRODED AREA WAS CUT AWAY AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 368232-14, REV A.Sep 15, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L992055Rib · crackedFOUND ON MV2 CK, .375 INCH CRACK ON NR 2 L/E SLAT RIB O/B OF ACTUATOR ATTACH BOLT. REPAIRED PER MM 57-54-0.Sep 15, 1999 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L992054Stiffner · crackedFOUND ON MV2 CK, L/E WING SPAR STIFFENER CRACKED AT THE NUMBER 7 SLAT O/B TRACK O/B SIDE. REPAIRED PER MM 57-20-21.Sep 15, 1999 · N511DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L992053Stiffner · crackedFOUND ON MV2 CK INBD AND OUTBD SPAR STIFFENERS CRACKED AT THE NUMBER 7 SLAT I/B TRACK ON THE FWD WING SPAR. REPAIRED PER MM 57-20-21.Sep 15, 1999 · N511DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L991967Web · crackedFOUND ON MV-2 CK, 1 INCH CRACK STA 1303 WEB WL 270 RBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.Sep 4, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991966Web · crackedFOUND ON MV-2 CK, 1 INCH CRACK IN STA 1303 WEB WL 270 LBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.Sep 4, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L992087Frame · corrodedFOUND DURING MV2 CORROSION VISIT NRC 226, CORROSION AT SUPPORT FRAME FOR ACCESS PANEL 3455R AT LWR SURFACE I/B OF FWD HINGE. REPAIRED PER M/M 53-30-1 FIG 804.Sep 1, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991982Stringer · crackedFOUND DURING MV2 CORROSION VISIT NRC 196, DURING UPPER WING INSPECTION OPERATION 5621, FOUND 1.5 INCH VISIBLE CRACK AT STR 18 A RT AT STA 936, IN LOWER FLANGE OF STR 18 A. REPAIRED PER M/M 53-12-0.Sep 1, 1999 · N511DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L990494Skin · crackedLFEC INSPECTION REVEALED A CRACK INDICATION NEAR THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SPLICE NEAR FS 442. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE AT FS 442. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTEDMar 7, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990493Skin · crackedLFEC INSPECTION INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R SKIN LAP SPLICE NEAR FS 405. HFEC INTERNAL INSPECTION OF THE SKIN LAP CONFIRMED A CRACK AT FS 405. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENMar 7, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990433Light · inopR1 OVER DOOR EMER LIGHT INOP. REPLACED LIGHT, CKS GOOD.Mar 2, 1999 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L990353Light · inopL2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.Feb 22, 1999 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L981601Hose · leakingAFTER T/O, LOST A-SYS HYD FLUID. RETURNED TO MSY. FOUND LEAKING SUPPLY LINE AT LEFT ELEVATOR PCU. REPLACED LINE.Aug 4, 1998 · N511DA · Boeing 727232 · Hydraulic System, MainSDR DL72L981248Web · crackedFOUND AT D-1 LETTER CHECK, WEB CRACKED RT FWD LOWER AFT AIRSTAIR AREA. REPAIRED PER M/M 53-11-0.Jun 12, 1998 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L972289Skin · crackedFOUND ON C2 LETTER CK, R-1 DOOR OUTER SKIN CRACKED 1 INCH UPPER FWD CORNER JUST BELOW GATE. REPAIRED PER MM 52-11-01.Nov 7, 1997 · N511DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72L972287Rib · crackedA 1.5 INCH CRACK IN DOUBLER NR 3 SLAT I/B NOSE RIB AT ACTUATOR ROD END ATTACH. REPAIRED PER M/M 57-54-0.Nov 7, 1997 · N511DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72L972042Wire · cutON L/O 2 CK, FOUND EMERGENCY TRACK LIGHTING INOP NEAR L1 DOOR. REPAIR SPLICED WIRES, OPN CKS GOOD PER M/M.Oct 11, 1997 · N511DA · Boeing 727232 · Light System WiringSDR DL72L971978Heat Manifold · blownNR 2 ENG DETECTOR ILLUM AFTER POSITIONING TO A AND TESTING LIGHT STAYED ON AND FOLLOWED BY NR 2 FIRE WARNING LIGHT. THROTTLE TO IDLE ALL INDICATIONS NORMAL AND ALL TESTS NORMAL, THROTTLE IN IDLE FOR DURATION. REPLACED NR 2 ENG FUEL HEAT MANIFOLD.Oct 6, 1997 · N511DA · Boeing 727232 · Fuel HeaterSDR DL72L970546Track Light · brokenEMERGENCY TRACK LIGHTING AT 22 RIGHT SIDE IS MISSING PARTS OF PLASTIC STRIP, RED COVER WILL NOT STAY IN. REPLACING TRACK PIECE, ALL LIGHTS SECURE AND TEST GOOD.Mar 20, 1997 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L960524Accessory Unit · malfunctionedON GEAR RETRACTION, THE RIGHT GEAR RED LANDING GEAR DISAGREEMENT LIGHT REMAINED ILLUMINATED AND REMAINED ILLUMINATED UNTIL GEAR EXTENDED FOR LANDING. PERFORMED OPERATION TEST OF UPLOCK SENSORS PER MM 32-61-811, REPLACED LANDING GEAR ACCESSSORY UNIT PER 32-09-Mar 6, 1996 · N511DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72L960390Skin · crackedDURING INSPECTION, LEFT WING O/B AILERON WAS FOUND WITH LOWER OUTBOARD SKIN CRACKED. REPAIRED PER MM 57-51-0 PG 801.Feb 20, 1996 · N511DA · Boeing 727232 · AileronsSDR DL72L960332Stiffener · crackedFOUND DURING B-1 LETTER CHECK - 1 INCH CRACK LWR END SPAR STIFFENER AT NR 6 L/E SLAT I/B TRACK I/B ANGLE. REPLACED PER MM 57-20-21.Feb 13, 1996 · N511DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L960331Angle · crackedFOUND DURING B-1 LETTER CHECK - .50 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTATCH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.Feb 13, 1996 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L960330Angle · crackedATTACH ANGLE BROKEN NR 1 L.E. FLAP ACTUATOR BOX. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21.Feb 13, 1996 · N511DA · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72L960134Skin · corrodedDURING INSPECTION, THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO HAVE CORROSION ON THE ATTACH FLANGE IN THE LT AFT CORNER. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 1-17-96, THE DAMAGE HAS BEEN BLENDED TO 0.59 MINIMUM FLANGE THICKNESS.Jan 17, 1996 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L960115Skin · corrodedBELLY SKIN WAS CORRODED REQUIRING A 1 INCH BY 4 INCH CUTOUT OF THE SKIN. THE STA 1009 BUTT SPLICE IS AFT OF THE CUTOUT AND FORWARD OF AN EXISTING REPAIR. REPAIRED PER SRM 53-30-3 FIG 3A.Jan 16, 1996 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L954349Eel Harness · damageCENTER CARGO EMERGENCY LIGHT INOP. REPLACED RACK AND REPAIRED DAMAGED WIRE HARNESS, OPERATION NORMAL.Nov 12, 1995 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L953924Eel Pwr Supply · failedDURING DEPARTURE CHECK, EMERGENCY TRACK LIGHT IN FWD CABIN DO NOT TEST. REPLACED BATTERY PACK M9026, OPERATION NORMAL.Oct 3, 1995 · N511DA · Boeing 727232 · Emergency LightingSDR DL72L953065Angle · crackedFOUND DURING A-2 LETTER CHECK, CRACK IN ANGLE BL 8 LEFT STATION 1183 ON I/B RADIUS AT BOTTOM OF BULKHEAD SUPPORT ANGLE. REPAIRED PER MM 53-11-0.Jul 13, 1995 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L953064Rib · crackedFOUND DURING A-2 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT ACT ATTACH I/B RIB. REPAIRED PER MM 57-54-0.Jul 13, 1995 · N511DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72L953063Angle · crackedFOUND DURING A-2 LETTER CHECK, 1 INCH CRACK NR 11 SPOILER ACTUATOR SUPPORT FITTING I/B ATTACH ANGLE BELOW SUPPORT FITTING MOUNT BOLT. REPAIRED PER SRM 57-50-6 FIG 7.Jul 13, 1995 · N511DA · Boeing 727232 · Wing Miscellaneous Structure
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