N543DA, cancelled Jul 20, 2010

Service difficulty reports · 80

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 = 'N543DA' AND deregistration_id = 'N543DA-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 DL72S020607Compressor · damagedNR 3 ENG WOULD NOT ACCELERATE ON ADDING T/O POWER. ABORTED T/O AT ABOUT 30 KTS. BORESCOPE INSPECTED 3 ENG 6 AND 7 STG COMP. FOUND 7 STG COMP BLD DAMAGE BEYOND M/M LIMITS. FULL LENGTH OF BLD. ALL BBLDS DAMAGED (361774). REPLACED 3 ENG PER CARD DECK 4T203May 29, 2002 · N543DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72S020344Outflow Valve · malfunctionedDURING CLIMBOUT FROM ATL, CABIN ALT CONT TO CLIMB AT 400 FT / MIN TO APPROX 9800 FT. A DESCENT WAS INITIATED AT 27000 FT TO AN ALTITUDE OF 16000 FT WHERE PRESSURIZATION COULD BE MAINTAINED. CARGO VALVE INDICATOR CLOSED THE ENTIRE FLIGHT. CHANGES TO BLEED SOMar 20, 2002 · N543DA · Boeing 727232 · Pressure Regulator/Outflow ValveSDR DL72S020213Frame · crackedFOUND ON F-2 LETTER CK 3/4 IN CRACK MLG UPLOCK FRAME SUPPORTSTRUCTURE AT STA 913 RIGHT W/W. REPAIRED PER MM 53-11-000-8.Feb 20, 2002 · N543DA · Boeing 727232 · Fuselage Structure (General)SDR DL72S011790Door Frame · crackedTHE FWD FRAME OF THE C1 DOOR OPENING AT FS 560 WAS FOUND WITH TWO WEB CRACKS AT EXISTING FASTENER LOCATIONS BELOW THE UPPER DOOR SILL. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0219 AND AD 99-23-13. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH A TITANNov 11, 2001 · N543DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S011722Slat · crackedMULTIPLE RIBS CRACKED,REPAIRED PER AMM 57-54-000-8 FIG 814Oct 16, 2001 · N543DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S011236Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #3 SLAT __REPAIRED PER MM 57-54-000-8Jul 25, 2001 · N543DA · Boeing 727232 · Wing StructureSDR DL72S011235Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #2 SLAT __REPAIRED PER MM 57-54-000-8Jul 25, 2001 · N543DA · Boeing 727232 · Wing StructureSDR DL72S011234Bracket · cracked3 INCH CRACK AT #1 SLAT ACT. ATTACH I/B AND O/B BRACKET __REPAIRED PER M/M 57-20-021-8Jul 25, 2001 · N543DA · Boeing 727232 · Wing StructureSDR DL72S011232Stiffener · crackedFOUND ON F-1 CK 1 INCH CRACK L/E WING VERTICAL SPAR STIFFENER O/B SIDE OF NUMBER 6 SLAT O/B TRACK.Jul 25, 2001 · N543DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S011231Angle · crackedFOUND ON F1 LETTER CK NUMBER 8 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED . REPAIRED PER MM 57-20-021-8.Jul 25, 2001 · N543DA · Boeing 727232 · Wing StructureSDR DL72S010876Indicator · faultyAFTER TAKEOFF RETRACTING FLAPS TO 5 DEGS INBD FLAPS REMAINED AT 15 DEGS. INBOARD FLAPS REMAINED AT 15 DEGS AFTER POM PROCEDURES. PILOT DECLARED EMERGENCY. REPLACED INBD FLAP POSITION IND AND INBD FLAP ASSY LOCK OUTRELAY R-187.May 31, 2001 · N543DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S010210Battery · inoperativeL2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS GOOD.Feb 6, 2001 · N543DA · Boeing 727232 · Emergency LightingSDR DL72S010177Engine · missingNR 3 OIL QTY DECREASE TO ZERO. DURING CRUISE FOLLOWED BY FLUCUATING OIL PRESS, SHUT DOWN NR 3 ENGINE PER POM. COMPLETED ENGINE FLAME OUT / LOSS OF THRUST SHUTDOWN FORM. ENGINE SHUTDOWN TIME 30 MIN / OIL PRESS WINDMILL 25 PSI / OIL QTY 0. FOUND 3 STUDS ON GJan 31, 2001 · N543DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S000998Frame · crackedA .5 INCH CRACK WAS FOUND IN THE WEB OF THE C1 DOOR OPENING AFT FRAME (FS 620) JUST BELOW THE NR 6 DOOR STOP. THE CRACK WAS COMMON TO A FASTENER HOLE ATTACHING THE WEB TO THE OUTER FRAME CHORD. THE WEB WAS LOCALLY TRIMMED AWAY TO REMOVE THE CRACK AND REPAIRMay 19, 2000 · N543DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S000938Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT FS 560 OVER STRINGER 28L. THE CORROSION WAS REMOVED WITH A 14 X 1.5 CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 377271-14.May 10, 2000 · N543DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000637Line · chafedA SYSTEM FAILURE. FOUND LINE TO NR 2 LEAKING. REPLACED WITH TEMP/APPROVED LINE. LEAK AND OPS CKS GOOD. HYD FLUID AT 3 GAL.Apr 4, 2000 · N543DA · Boeing 727232 · Hydraulic System, MainSDR DL72S000520Battery · dischargedAFT CABIN DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS NOW OK.Mar 16, 2000 · N543DA · Boeing 727232 · Emergency LightingSDR DL72S000519Battery · dischargedMID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK.Mar 16, 2000 · N543DA · Boeing 727232 · Emergency LightingSDR DL72S000249Door · failedRIGHT PACK TRIP FOLLOWED BY SMOKE IN CABIN. FOUND RT COOLING DOOR NOT OPENING WHEN PACK SELECTED. REPLACED RT COOLING DOOR ACTUATOR RELAY.Feb 2, 2000 · N543DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S992390Battery · dischargedAFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPS CK OK.Oct 28, 1999 · N543DA · Boeing 727232 · Emergency LightingSDR DL72S992266Web · crackedFOUND ON D2 LETTER CK, .25 INCH CRACK LEFT VERTICAL TORQUE BOX WEB LIGHTENING HOLE STA 1323.. ALSO, RT VERTICAL TORQUE BOX WEB AT LIGHTENING HOLE AT STA 1233 CRACKED .25 INCH. REPAIRED PER MM 53-11-0.Oct 12, 1999 · N543DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991635Flap · brokeON APPROACH, RIGHT O/B TRAILING EDGE FOREFLAP BROKE IN HALF. DID NOT LEAVE AIRCRAFT. DID GO-AROUND. A/C LANDED WITHOUT INCIDENT.Jul 20, 1999 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990531Web · crackedRT SIDE TORQUE BOX WEB HAS .125 INCH CRACK PROTRUDING PAST. ROUTE OUT REPAIR AT STA 1283 LOWER HOLE M/M 53-11-0 PG 832.Mar 12, 1999 · N543DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990248Gearbox · leakingON APPROACH INTO CVG PASSING THROUGH APPROX 9000 AGL, NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL QTY WAS AND NOW OBSERVED TO DECREASE, OIL TEMP NORMAL, INCREASED ABOVE 105 DEG C. ENGINE SHUT DOWN PER POM PROCEDURES. FOUND NR 2 ENG GEARBOX LEAKING AT 6 O'CLOCFeb 5, 1999 · N543DA · Boeing 727232 · Turbine Engine Accessory DriveSDR DL72S981650Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH CRACK AT RBL 25 AND WL 169. THE CRACK WAS REPAIRED WITH A TITANIUM REPAIR DOUBLER ON A TEMPORARY BASIS WITH REPETITIVE INSPECTIONS. THE PERMANENT REPAIR WILL ACCOMPLISH A WEB MODIFICATION PER BAC S/B 727-53-02Aug 8, 1998 · N543DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S980397Skin · corrodedA 24 X 17.5 AREA OF SKIN WAS TRIMMED AWAY BETWEEN FS 480 AND FS 500, AND BETWEEN STRINGERS 27L AND 27R. THE SKIN CUTOUT WAS REPAIRED WITH A DOUBLER AND TRIPLER INSTALLED PERER/A 364006-14, REV A.Feb 13, 1998 · N543DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S980320Floorbeam · corrosionCORROSION ON FLOORBEAM STA 1030 AT BOLT HOLES AT BL 0, LBL 9 AND RBL 10.5. CORROSION WITHIN LIMITS AT BL 0 AND RBL 10.5. CORROSION OUT OF LIMIT AT STA LB 9 PER SRM 53-10-1. INSTALLED REPAIR PER M/M 53-20-11.Feb 3, 1998 · N543DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S980319Floorbeam · cracked.75 INCH CRACK ON FLOORBEAM STA 344 AT LBL 30 AT FLOOR PANEL FASTENER HOLE. DRILLED UP REPLACEMENT SECTION PER SRM 53-10-8.Feb 3, 1998 · N543DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S971858Bulb · failedONE WHITE EMERGENCY PATH LIGHT INOP. REPLACED BULB.Sep 23, 1997 · N543DA · Boeing 727232 · Emergency LightingSDR DL72S961759Pack Fan · inoperativeREJECTED TAKEOFF AT DFW 18L DUE TO RT PACK TRIPPING OFF AND FILLING THE CABIN WITH SMOKE. REPLACED RIGHT PACK FAN. OPS CHECK NORMAL.Jul 23, 1996 · N543DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S960806Skin · crackedFOUND ON A2 LETTER CHECK, 1 INCH VISIBLE CRACK ON NR 7 SLAT COVE SKIN SUPPORT ANGLE. REPAIRED PER MM 57-54-0.Apr 8, 1996 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960805Skin · crackedFOUND ON A2 LETTER CHECK, L1 DOOR UPPER AND LOWER HINGE CUTOUTS CRACKED, UPPER .5 INCH LOWER .875 INCH. REPAIRED PER MM 53-30-0.Apr 8, 1996 · N543DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960370Hprsov · malfunctionedON DECENT AT ABOUT 9K, STRONG DUSTY ELEC SMELL IN AFT ENTRY AREA. THE WING AND ENGINE HEAT OFF. DEACTIVATED GALLEY POWER AND LAV FLUSH MOTORS AS PRECAUTION. INSPECTED AND OPERATED SYSTEMS, UNABLE TO DUPLICATE. SUBSEQUENT OCCURENCE ISOLATED PROBLEM TO HIGHFeb 18, 1996 · N543DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S960369Air Distr · odorDURING FINAL APPROACH, FLT ATTN NOTICED BURNING SMELL LIKE FIREWORKS, AROUND LT AFT LAV AREA. MTC POWERED A/C, TURNED ON ALL GALLEY AND LAV EQUIPMENT AND WAS UNABLE TO REPRODUCE ANY NOTICEABLE SMELL.Feb 18, 1996 · N543DA · Boeing 727232 · Air Distribution SystemSDR DL72S960200Baffle · crackedDURING ROUTINE SHOP INSPECTION, A CRACK WAS FOUND IN THE ANTI-ICE BAFFLE BETWEEN THE 11TH AND 12TH RIB FROM THE I/B END. BAFFLE WAS REPAIRED AS PER MM 57-57-0 FIG 8103A FOR NR 2 L/E SLAT.Dec 9, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S953614Angle · crackedFOUND ON A-1 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0.Sep 5, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951679Nose Cowl · crackedOUTER FRAME AND BULKHEAD DAMAGED UNDER TEMP. REPAIR AT 3 O'CLOCK POSITION. DAMAGE WAS REPAIRED PER B-727 SRM 54-10-3 FIG 3 FOR NR 3 ENGINE NOSE COWL, DURING SHOP INSPECTION.Mar 22, 1995 · N543DA · Boeing 727232 · Engine Cowling SystemSDR DL72S950946Skin · dentedDURING SHOP VISIT, FOUND THE NR 1 MIDFLAP LEADING EDGE SKIN DENTED I/B OF F/F TRACK CUTOUT 98 INCHES FROM I/B END. CUT OUT DAMAGE AND INSTALLED DOUBLER PER MM 57-50-0 FIG 803 PG 808.Feb 25, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951319Nose Cowl · damagedDURING SHOP INSPECTION, FOUND AFT BULKHEAD TORN AND BENT AT STATION 99.25, OF NOSE COWL. REPAIRED DAMAGE PER SRM 54-10-3 FIG NR 3.Feb 22, 1995 · N543DA · Boeing 727232 · Engine Cowling SystemSDR DL72S950660Te Panel · delaminatedDURING SHOP INSPECTION, FOUND RIGHT WING SPOILER PANEL TRAILING EDGE DELAMINATED. REPAIRED PER SRM 57-50-6.Feb 17, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950644Panel · delaminatedDURING HMV, FOUND NR 12 SPOILER PANEL DELAMINATED AT THE TRAILING EDGE, REPAIRED PER B-727 SRM 51-40-6.Feb 16, 1995 · N543DA · Boeing 727232 · SpoilersSDR DL72S950718Support Bracket · crackedAT HMV, FOUND NR 5 KRGR FLAP ACT SUPPORT BRACKET CRACKED AT LWR OB LEG. FABRICATED AND INSTALLED NEW DOUBLER PER M/M 57-20-21.Feb 15, 1995 · N543DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950648Bracket · crackedAT HMV, NR 6 LEADING EDGE FLAP ACTUATOR SUPPORT BRACKETS WERE FOUND CRACKED. REPAIRED THE BRACKETS PER MAINTENANCE MANUAL 57-20-21.Feb 15, 1995 · N543DA · Boeing 727232 · Leading Edge Slat Control SystemSDR DL72S954267Flap Track · corrosionTHE LEFT SIDE INBOARD TRACK FOR THE INBOARD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE, FORWARD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBOARD AND OUTBOARD SIDES OF THE TRACK. THE HOLES WERE BOTH OVERSIZED TO Feb 14, 1995 · N543DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S951435Rear Spar · crackedAT SHOP INSP, NR 3 MID FLAP WAS FOUND WITH BOTTOM REAR SPAR CRACKED AT 40 INCHES FROM I/B END. REPAIRED PER MM 57-52-0 PG 807.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951434Spar · crackedBOTTOM REAR SPAR CHORD CRACKED 54 INCHES FROM I/B END OF NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0. FOUND DURING SHOP INSPECTION.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951433Angle · crackedCHORD ANGLE REPAIR CRACKED AT I/B PUSH ROD CUTOUT NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951432Angle · crackedAT SHOP INSPECTION, NR 3 MID FLAP WAS FOUND WITH CHORD ANGLE CRACKED AT I/B AFT FLAP TRACK CUTOUT. REPLACED CHORD PER SRM 57-52-0.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S951431Fitting · wornAT SHOP INSPECTION, NR 3 MID FLAP CARRIAGE SUPPORT FITTING INBOARD THRUST BEARING RETAINER BOLT HOLES ARE CORRODED. REAMED HOLE TO .312 TO REMOVE CORROSION HFEC, TREATED AND BUSH PER SRM 57-50-4.Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950708Skin · delaminatedAT HMV, FOUND NR 14 SPOILER DELAMINATED. REPAIRED PER SRM 57-50-6.Feb 14, 1995 · N543DA · Boeing 727232 · Spoilers
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