N544DA, cancelled Nov 8, 2006
Service difficulty reports · 67
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 = 'N544DA' AND deregistration_id = 'N544DA-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.
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 = 'N544DA' AND deregistration_id = 'N544DA-2006-11-08' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL72S030141Battery Pack · dischargedRT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.SDR DL72S021479Engine · malfunctionedNR 3 ENGINE EGT LIMITED IN CLIMB POWER, EGT 590-595 AT 20 TAT CLIMB THRUST (ON T/O USING ALT 40 TAT CLIMB NR 3 EGT 610). AT 20 TAT CLIMB EPR = 1.88 HAD TO PULL NR 3 THROTTLE BACK TO 1.76 EPR TO KEEP EGT AT / BELOW 580. REPLACED NR 3 ENGINE PER 4T203AD.SDR DL72S020370Charger · failedLEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY, OPERATION NORMAL.SDR DL72S020290Charger · failedLEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER.SDR DL72S011797Light · unserviceableEXIT SIGN ABOVE 1L DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TESTED. REPLACED LIGHT ASSYSDR DL72S011191Seal · tornON CLIMBOUT A LOUD SQUEAL DEVELOPED FROM FORWARD LEFT DOOR. NOISE WAS TOO LOUD TO CONTINUE FLIGHT. DECENDED TO 10,000 FTAND CHANGED CABIN TO 2.0 PSID. NOISE STOPPED. CA RPD L1 DOOR SEAL.SDR DL72S011178Web · crackedFOUND ON E2 LETTER CK R/H INBD VERT TORQUE BOX WEB CRACKED AT UPPER END STA 1214 R/H. REPAIRED PER MM 53-11-000-8.SDR DL72S011177Clip · crackedFOUND ON E2 LETTER CK SKIN CLIP CRACKED FWD STA 1263 ABOVE STR 12R. REPAIRED PER B727 DAL DRD 53-10-4D FIG 803D.SDR DL72S010591Light · inoperativeEMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED LIGHT RACKSDR DL72S010580Battery Pack · dischargedLT OVERWING EMERGENCY EXIT LIGHT FLASHING. REMOVED AND REPLACED BATTERY PACK.SDR DL72S010168Light · inoperativeON L/O FOUND C-2 DOOR EMERGENCY FLOOD LIGHT INOP. REPLACED SAME.SDR DL72S010163Battery · dischargedDURING STBY PWR CK LT SIDE OVERWING EXIT LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK. ALL CHECKS NORMAL.SDR DL72S002471Stringer · corrodedFUSELAGE / STRINGER / FS 440 / STRG. 27L : SPLICE REPAIR. STRINGER 27L WAS FOUND CORRODED AT FS 440. THE CORRODED SECTION OF STRINGER WAS CUT AWAY TO REMOVE ALL DAMAGED. THE DAMAGED SECTION WAS REPAIRED WITH TWO (2) ALUMINUM REPAIR ANGLES INSTALLED SDR DL72S000968Skin · crackedNR 3 KRUEGER FLAP CRACKED AT O/B LIP HINGE CUTOUT. TPA D-2 LTR CHK. INSTALLED DOUBLER PER M/M 57-53-0, NR 2A.SDR DL72S000923Engine · leakingOIL QUANTITY DECREASED RAPIDLY ON NR 3 ENG. RATE WAS APPROX 1 GAL PER 5 MIN UNTIL REACHING ZERO. ENG CHANGE IN PROGRESS.SDR DL72S000765Flap Track · corrodedTYPICAL CORROSION WAS FOUND ON THE LOWER SURFACE OF THE NR 4 AND NR 5 FLAP TRACKS AND ON THE UPPER SURFACE OF THE MLG AT THE INTERFACE OF THE FLAP TRACK AND THE MLG SUPPORT BEAM. THE CORROSION WAS MACHINED OR SPOTFACED FOR REMOVAL PER THE GUIDANCE OF BSDR DL72S000334Wire · disconnectedEMERGENCY EXIT LIGHT OVERRIDE SWITCH AT AFT FLIGHT ATTENDANT STATION INOP. FOUND ONE WIRE DISCONNECTED FROM AFT ATTENDANT EMERGENCY LIGHT SWITCH. RESECURED WIRE TO SWITCH, OPERATION NOW NORMAL.SDR DL72S992243Engine · malfunctionedON CLIMB-OUT, NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. S/D ENG PER POM. OIL FILTER FOUND CLEAN. REPLACED SAME, ENGINE RUN CHECKS GOOD.SDR DL72S992221Casting · crackedFOUND ON D1 LETTER CK, NR 4 SLAT ACTUATOR I/B MOUNT CASTING CRACKED. REPLACED CASTING.SDR DL72S992220Stiffner · crackedFOUND ON D1 LETTER CK, NR 4 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S992219Rib · crackedFOUND ON D1 LETTER CK, NR 1 SLAT L/E NOSE RIB CRACKED 1.5 INCH AT I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0.SDR DL72S991632Skin · crackLOWER SKIN CUT TO FACILITATE MAINTENANCE. REPAIRED PER M/M 57-54-0 FIG 801.SDR DL72S991631Rib · crackedRIB CRACKED. REPAIRED RIB PER M/M 57-54-0.SDR DL72S990467Battery · dischargedFLASHLIGHT HAD NO CHARGE. REPLACED BATTERY, OPS CK GOOD.SDR DL72S990465Battery Pack · dischargedOVERWING RT SIDE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND OPS CK GOOD.SDR DL72S990457Angle · crackedFOUND ON C2 LETTER CK, RT KEEL BEAM SUPPORT ANGLE CRACKED AT STA 870. REPLACED ANGLE PER SRM 53-10-9.SDR DL72S982075Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183 LBL 18 VERTICAL BEAM, REPAIR FOR CRACK. A .75 INCH TYPICAL CRACK WAS FOUND IN RADIUS OF THE LBL 18 VERTICAL BEAM LOWER END ON THE FS 1183 BULKHEAD. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 727-53-0202. THE REPAIR WAS DOCUMENTED PESDR DL72S980659Fuel Control · failedNR 3 ENG DID NOT RESPOND TO THROTTLE MOVEMENT DURING DESCENT, FLAMEOUT, FUEL FLOW WAS ZERO. EGT AND EPR WERE ZERO AND NOT RESPONDING. N1 AND N2 DISPLAYED WINDMILLING INDICATION, THIS LASTED FOR 2 TO 3 MINUTES. PRIOR TO COMMENCING THE ENG FAILURE FOLLOW UP CSDR DL72S971773Door · crackedAT FL 350 CABIN STARTED CLIMBING AT 650 FPM. CARGO HEAT OUTFLOW AND MAIN OUTFLOW VLV'S CLOSED. LT PACK WENT TO FULL CLOSED AND WOULD NOT CHANGE. NO DUCT OVERHEAT OR PACK TRIP OFF LIGHT, ALSO NO PRESS FAILURE LIGHTS. FOUND C-3 CARGO DOOR FWD LWR CORNER CRACSDR DL72S960814Angle · crackedFOUND ON A-1 LETTER CHECK, 1.5 INCH CRACK IN NR 3 L/E SLAT LWR COVE SKIN ANGLE. REPAIRED PER M/M 57-54-0.SDR DL72S960626Bulb · failedAFT GALLEY DOOR EXIT LIGHT INOP. RELAMPED, OPERATION NORMAL.SDR DL72S954253Chord · crackedDURING SHOP VISIT, A CRACK AND TEMPORARY REPAIR DOUBLER WAS FOUND ON AFT CHORD OF NR 2 MIDFLAP. INSTALLED PERMANENT REPAIR PER MM 57-53-0.SDR DL72S954254Chord · crackedDURING SHOP VISIT, A CRACK WAS DISCOVERED ON AFT CHORD AT I/B DRIVE ROD CUTOUT, OF NR 2 MIDFLAP. REPAIRED PER MM 57-52-0.SDR DL72S953941Le Skin · wornDURING SHOP INSP, NR 3 MIDFLAP WAS FOUND WITH I/B L/E SKIN WORN. REPAIRED LEADING EDGE PER MM 57520, BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.SDR DL72S953942Skin · wornDURING SHOP INSP, NR 4 MIDFLAP L/E SKIN WORN AT O/B END OF FLAP. REPAIRED PER MM 57520 BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.SDR DL72S953818Cowling · crackedDURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL.SDR DL72S953879Frame · misdrilledDURING THE ACCOMPLISHMENT OF DAL EO 4-58560-3AD, IT WAS NOTICED BY MAINTENANCE THAT THE FRAME REINFORCEMENT STRAP ON THE OUTER CHORD OF STA 760.95 FRAM, WAS DOUBLE DRILLED AT THREE LOCATIONS PRIOR TO THIS HEAVY MAINTENANCE VISIT. MAINTENANCE OVERSIZED THE HOLSDR DL72S954036Skin · corrodedBELLY SKIN, CORROSION AT STA 700 TO 720, O/B OF S-28L AD 91-09-09, 94-05-04. SKIN CORROSION AT STA 700 TO 720, O/B OF S-28L HAS PROMPTED REQUEST FOR AN EXTENSION OF AN EXISTING DOUBLER IN THAT AREA TO COVER THE ADDED DAMAGE REMOVAL, APPROXIMATLY 2 BY 2 INCHESSDR DL72S953779Rib · crackedDURING HMV, FOUND ON VERTICAL FIN 4TH RIB DOWN FROM ACCESS HOLE STA 6.372 RIB NR 6 CHORD ANGLE CRACKED AT STR 7 LEFT. REPAIRED PER M/M 55-30-0 PG 802.SDR DL72S953778Rib · crackedDURING HMV, FOUND NR 8 SLAT, RIB NR 13 WAS CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S953777Rib · crackedDURING HMV, FOUND NR 4 SLAT HAS CRACK AT ACTUATOR ATTACH O/B RIB. REPAIRED PER MM 57-54-0 FIG 804.SDR DL72S953776Rib · crackedDURING HMV, FOUND NR 3 SLAT HAS CRACK IN LOWER SURFACE OF NR 3 RIB FROM I/B END. REPAIRED PER MM 57-54-0 FIG 805.SDR DL72S953748Angle · crackedFOUND DURING HMV - NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED PER M/M 57-54-0, FIG 812.SDR DL72S953730Actuator Mount · crackedFOUND AT HMV, NR 4 SLAT MAIN ACTUATOR MOUNT CRACKED AT PREVIOUSLY REPAIRED AREA. REPAIRED PER M/M 57-54-0, FIG 804A.SDR DL72S953729Rib · crackedFOUND ON HMV RIB WEB AT TAI, TUBE CRACKED AT NR 6 SLAT INBOARD WEB. REPAIRED RIB PER M/M 57-54-0, FIG 805.SDR DL72S953878Frame · oversized holesDURING ACCOMPLISHMENT OF EO 4-61904-3AD, SEVERAL HOLES IN THE INBOARD FRAME FLANGE AT FS 760.95, BOTH RT AND LT SIDES WERE OVERSIZED THROUGH THE STRAP, FRAME, AND MODIFICATION ANGLE. ONE HOLE ON THE LEFT HAND SIDE HAS BEEN OVERSIZED TO 0.403 DIA AND REQUIRES SDR DL72S953775Beam · crackedDURING HMV, FOUND FWD ENTRY DOOR LOWER HORIZONTAL BEAM CRACKED AT AFT CORNER. REPAIRED PER M/M 52-11-01 PG 805.SDR DL72S953695Bracket · crackedDURING HMV, FOUND NR 6 KRUEGER FLAP ACTUATOR BRACKET IS CRACKED AT I/B LOWER FWD CORNER. REPAIRED PER M/M 57-20-21.SDR DL72S953774Skin · crackedDURING HMV, FOUND LT ELEVATOR SKIN CRACKED APPROX 1.5 INCH CRACK IN UPPER SKIN I/B END NEAR LEADING EDGE. REPAIRED PER SRM 55-20-3.SDR DL72S953880Rib · crackDURING THE ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DETECTED IN A FASTENER HOLE IN THE VERTICAL FLANGE OF THE RIB CHORD AT BS 760.95. REMOVAL OF THE CRACK IN THE RIB CHORD RESULTED IN THE INADVERTENT OVERSIZING OF THE FUSELAGE SKIN AT THIS LOCATION, AS W
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