N536DA, cancelled Jul 20, 2010

Service difficulty reports · 37

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 = 'N536DA' AND deregistration_id = 'N536DA-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 DL72S010865Sign · inoperativeEMERGENCY EXIT SIGN INOP ACROSS FROM ROW 32. RELAMPED EMERGENCY EXIT SIGN.May 29, 2001 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S010260Engine · intermittentNR 1 ENG FILTER BY PASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT 100 KTS. RETURNED TO BLOCKS. INSP AND REPLACED NR 1 ENG MAIN OIL SCREEN. FWD FILTER BY PASS LIGHT TO MCO AND PLACARD PER MEL 79-00-02.Feb 14, 2001 · N536DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S001547Spar · crackedTHE RT ELEVATOR WAS FOUND WITH A .25 INCH CRACK IN THE REAR SPAR EMANATING FROM THE EDGE OF A SHEAR PLATE. THE CRACK IS TYPICAL OF BAC S/B 727-55-0089. HOWEVER, THE TERMINATING ACTION OF THE S/B HAD BEEN ACCOMPLISHED. THE CRACK WAS STOP DRILLED AND ALLOWED Aug 11, 2000 · N536DA · Boeing 727232 · Elevator StructureSDR DL72S001383Light · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT STA 680. REPLACED LIGHT ASSY, OPS NORMAL.Jul 21, 2000 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S000966Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC CONFIRMED CRACKS IN TWO FRAME BAYS. BECAUSE OF THE CRACKS AND EXISTING PREVIOUS REPAIRS THE ENTIRE LAP JOINT May 15, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000842Power Supply · inoperativeDURING CHECK OF THE EMERGENCY LIGHT SYSTEM, ROWS AFT OF 26 AND THE LT, RT AND AFT DOOR WERE INOP. FOUND AFT POWER SUPPLY BAD. REPLACED THE POWER SUPPLY, OPS CHECK GOOD.Apr 28, 2000 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S000644Panel · missingFWD BLOW OUT PANEL ON RT SIDE OF NR 2 ENG COWL MISSING. REPLACED BLOW OUT PANEL, NO DUCT LEAKS NOTED ON ENG RUN.Apr 5, 2000 · N536DA · Boeing 727232 · Engine Cowling SystemSDR DL72S000187Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION CONFIRMED THREE CRACKS BETWEEN FS 520 & FS 540. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXJan 25, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991416Track · corrosionCORROSION WAS DISCOVERED IN THE TWO BOLT HOLES WHERE THE I/B FLAP O/B FLAP TRACK ATTACHES TO THE SPOILER SUPPORT LWR CHORD. REWORKED PER ERA 333256-14, REV A.Jun 23, 1999 · N536DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S991415Fitting · corrodedRHS BOLT HOLES FOR THE VERT FIN FITTING ATTACH TO TENSION TIE RIB WAS FOUND WITH CORROSION. REWORKED PER ERA 333260-14, REV B.Jun 23, 1999 · N536DA · Boeing 727232 · Vertical StabilizerSDR DL72S991407Frame · crackedDURING ACCOMPLISHMENT OF INSPECTIONS OF THE OVERWING EXIT FRAMES, UNIDENTIFIED REPAIRS WERE NOTED. THE SUBJECT ERA WILL EVALUATE THE REPAIRS AND ENSURE COMPLIANCE / DOCUMENTATION. REWORKED PER ERA 333213-14AD, REV A.Jun 21, 1999 · N536DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S991360Frame · crackedFRAME AT BS 620 WAS FOUND CRACKED REMOVAL OF THE CRACK REQUIRED REMOVAL OF APPROX 5 OF THE UPPER FLANGE FROM THE PRODUCTION SPLICE AT RBL 11 INBD TO RBL 6. REPAIRED PER ERA 333235-14.Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S991359Skin · gougedGOUGE FOUND IN FUSELAGE SKIN AT AFT EDGE OF THE C2 DOOR AT BS 990. DAMAGE AREA IS LOCATED AT S24R PLUS 5 AND IN THE SKIN ONLY. REPAIRED PER ERA 333244-14, REV A.Jun 16, 1999 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990745Skin · crackedLFEC INSPECTION OF THE STINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGApr 3, 1999 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990408Light · inopL1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NOW OK.Feb 26, 1999 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S982252Coffeemaker · failedINDICATION OF SMOKE OBSERVED BY FLT ATTEND IN AFT GALLEY AND AFT CABIN. REPLACED COFFEEMAKER AND CANNON PLUG.Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/GalleysSDR DL72S982241Connector · shortedSMOKE IN AFT CABIN. FOUND THE CANNON PLUG FOR THE NR 3 COFFEEMAKER IN THE AFT GALLY SHORTED. PULLED AND COLLARD C/B, DISCONNECTED CANNON PLUG FROM COFFEEMAKER.Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/GalleysSDR DL72S981541Wire · brokenTHE FWD EMER EXIT SIGN IN THE COACH CABIN INOP. FOUND BROKEN GRD WIRE AT C/P FOR LIGHT ON LIGHT SIDE. REPAIRED WIRE, EMER LIGHTS CK OK.Jul 20, 1998 · N536DA · Boeing 727232 · Light System WiringSDR DL72S980690Bracket · crackedFOUND ON D1 LETTER CK, NR 2 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER RADIUS. REPAIRED PER MM 57-20-21.Mar 30, 1998 · N536DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S980689Web · crackedFOUND ON D1 LETTER CK, LT VERT TORQUE BOX WEB CRACKED AT UPPER END AT STA 1237 LT. REPAIRED PER MM 53-11-0.Mar 30, 1998 · N536DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980673Indicator · shortedAT FL 310 HAD STRONG ELECT SMELL LIKE PLASTIC BURNING. INDICATOR LTS MASTER SECT 1 C/B POPPED. ODOR SLOWLY SUBSIDED, FOUND COCKPIT INDICATOR SHORTING TO GROUND. REPOSITIONED TERMINALS, CKS OK.Mar 27, 1998 · N536DA · Boeing 727232 · Flight Compartment LightingSDR DL72S972645Structure · damagedFUSELAGE, SKIN, FRAME, AND STRINGER FS228-252, S24R. REPAIR FOR DENTED AND CRACKED SKIN, STRINGERS, AND FRAMES. THE FUSELAGE SKIN BETWEEN FS 228 AND 252 AT S-24R WAS DAMAGED BY GROUND EQUIPMENT. THE SKIN DAMAGE WAS CUTOUT AND A DOUBLER REPAIR INSTALLED. THDec 10, 1997 · N536DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S971692Stringer · cracked1.25 INCH CRACK IN VERT STAB S-9R AND SECOND BULKHEAD ABOVE CRAWL WAY OPENING. REPAIRED PER MM 55-30-0 PG 803.Aug 28, 1997 · N536DA · Boeing 727232 · Vertical StabilizerSDR DL72S970112Frame · crackedA .375 INCH VISIBLE CRACK IN MLG UPLOCK FRAME OUTB'D FLANGE STA 913.5 UPPER END OF RADIUS BLOCK. INSTALLED REPAIR PER MM 53-11-0 PG 834.Jan 20, 1997 · N536DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S970110Skin · crackedFOUND DURING C-1 LETTER CHECK, 4.5 INCH CRACK LEFT ELEVATOR LWR SKIN AT O/B END. REPAIRED PER SRM 55-20-3.Jan 20, 1997 · N536DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S961515Web · crackedA 1.25 IN CRACK IN TORQUE BOX WEB UPPER RT CORNER AT STA 1213 AT UPPER CORD. INSTALLED DOUBLER PER MM 53-11-0 PG 832.Jun 24, 1996 · N536DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960174Spar · crackedDURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A.Jan 24, 1996 · N536DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960173Ballast · failedCEILING POWER FWD C/B ON P18-3 PNL POPPED FOLLOWED BY AN ACRID ELECTRICAL SMELL IN THE FWD PART OF THE AIRCRAFT. PULLED AND COLLARED FWD CONT C/B AND FWD CEILING PWR C/B. PULLED C/P ON CEILING LIGHT AT RT ROW 24 AND LT 17. FOUND BURNED BALLAST, REPLACED BALJan 23, 1996 · N536DA · Boeing 727232 · Passenger Compartment LightingSDR DL72S954668Mask · popped indicatorDURING INSPECTION, FOUND FWD CABIN PBE WITH POPPED INDICATOR. REPLACED PBE.Dec 7, 1995 · N536DA · Boeing 727232 · Portable Oxygen SystemSDR DL72S954476Angle · crackedFOUND DURING B-1 LETTER CHECK, NR 5 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.Nov 22, 1995 · N536DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954475Actuator Mount · crackedFOUND DURING B-1 LETTER CHECK, NR 7 L/E SLAT ACTUATOR MOUNT FITTING CRACKED 1 INCH AT LWR I/B MOUNT BOLT. REPAIRED PER M/M 57-42-0 PAR 5.Nov 22, 1995 · N536DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S954473Spar Stiffener · crackedFOUND ON B1 LETTER CK, LE SPAR STIFFENER CRACKED OUTBD TRACK NUMBER 3 SLAT INBD ANGLE. REPAIRED PER MM 57-20-21.Nov 22, 1995 · N536DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S954343Bolt · missingON DEPARTURE, NR 2 SLAT FAILED TO RETRACT, AIL WAS DISPLACED 30 UNITS, NR 2 SLAT SHOWED GREEN ON S/O PANEL, NR 2 SLAT FINALLY STOWED WITH SPEED REDUCTION. FOUND NR 2 SLAT LWR INBRD BOLT MISSING FROM TRUNNION BRACKET, INTERMITTENTLY BINDING SLAT RETRACTION REPNov 11, 1995 · N536DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S953920Angle · crackedTHE NR 5 L/E SLAT, LOWER T/E ATTACH ANGLE CRACKED AT RIB NR 9. REPAIRED PER M/M 57-54-0 PAGE 807A.Sep 25, 1995 · N536DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S953394Eel Battery Pack · dischargedDURING LAYOVER, FOUND EMERGENCY LIGHTS ABOVE AFT AIRSTAIR INOP. REPLACED BATTERY OPERATION NORMAL.Aug 14, 1995 · N536DA · Boeing 727232 · Emergency LightingSDR DL72S952133Angle · crackedDOUBLER CRACKED FOR FLANGE UNDER ANTI ICE DUCT FOR NR 2 SLAT. FOUND DURING A-2 LTR CK. REPAIRED PER MM 57-54-0.May 15, 1995 · N536DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952132Rib · crackedONE-HALF INCH CRACK NR 2 SLAT NOSE RIB ANGLE O/B OF ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. FOUND AT A-2 LETTER CHECK.May 15, 1995 · N536DA · Boeing 727232 · Leading Edge Devices
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