N522DA, cancelled Apr 2, 2013
Service difficulty reports · 63
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 = 'N522DA' AND deregistration_id = 'N522DA-2013-04-02' 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 = 'N522DA' AND deregistration_id = 'N522DA-2013-04-02' 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 DL72S020595Ram Air Door · stuckAT GATE WITH APU POWER,TURNED PACKS ON AND CABIN FILLED WITH SMOKE. FOUND RT PACK RAM AIR SCOOP CK VALVE STUCK OPEN. FREED DOOR, RAN PACKS, RAN ENGINES 1 AND 3. PACK OPERATING, NO FURTHER SMOKE OR FUMES IN CABIN. OK FOR SERVICE.SDR DL72S020588Skin · crackedA CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEARSTRAP OF THE LOWER HINGE CUTOUT OF THE L1 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE BEARSTRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383225-14,SDR DL72S020585Skin · corrodedFUSELAGE / SKIN / FS 1067 / STRG. 28R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 1067 NEAR STRINGER 28R. THE CORROSION WAS REMOVED WITH A 5.75" X 2" CUTOUT SDR DL72S020584Skin · crackedFOUND ON E1 LETTER CK 1/2 CRACK VISIBLE VERTICAL STAB AT LWR END SKIN AT AFT SPAR R/H SIDE REPAIRED PER M/M 55-30-000-8 FIG 801SDR DL72S020583Skin · crackedFOUND ON E1 LETTER CK, LT ELEVATOR BONDED BEADED SKIN CRACKED AT STA 100 TO STA 103 FWD OF TAB. REPAIRED PER SRM 55-20-3D FIG 3.SDR DL72S020582Skin · crackedFOUND ON E1 LETTER CK 2 INCH CRACK L/H ELEVATOR LOWER SKIN FWD OF TAB WRITEN ON CARD 79 REPAIRED PER SRM 55-20-3D FIG 5SDR DL72S020581Angle · crackedFOUND ON E1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED BELOW #2 SLAT TAI DUCT. REPAIRED PER MM 57-54-000-8SDR DL72S020580Web · crackedFOUND ON E1 LETTER CK I/B MOUNT WEB CRACKED #1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21-8.SDR DL72S020338Valve · malfunctionedPACKS OVERHEATED ON TAXI OUT. RETURNED TO GATE. HAZE IN CABIN. FOUND RIGHT PACK FREEZING UP, REPLACED 35 DEGREE CONTROLLER AND VALVE.SDR DL72S011682Angle · crackedLWR COVE SKIN ANGLE IS CRACKED AT #7 SLAT I/B UPSTOP PAD. SLAT SER # BN324. REPAIRED PER M/M 57-54-000-8SDR DL72S011110Charger · faultyRIGHT AFT LOWER FUSELAGE EMERGENCY LIGHT INOP. REPLACED CHARGER, CKS OK.SDR DL72S002499Switch · unserviceableNR 5 KRUGER FLAP SHOWED AMBER AFTER RETRACTION. CORRECTION: REPLACED NO. 5 KRUGER FLAP POS. SWITCHSDR DL72S002304Skin Panel · damagedDURING ACCOMPLISHMENT OF PREVENTIVE MOD. PER E.O. 4-70183-3 THE UPPER AND LOWER SKIN PANELS WERE FOUND WORN FROM REPETITIVE DISASSIMBLY. MANY ATTACHMENT HOLES WERE OVERSIZED. REPAIR PER ER/A 397029-14ADSDR DL72S002288Frame · corrodedFUSELAGE / C3 DOOR CUTOUT SURROUND STRUCTURE / AFT FRAME : CORROSION REPAIR. THE AFT FRAME OF THE C3 DOOR CUTOUT (FS 1142) WAS FOUND WITH CORROSION IN THE SKIN FLANGE BETWEEN STRINGER 28R AND 29R. THE CORRODED FLANGE WAS TRIMMED AWAY. THE DAMAGE WAS REPAIRSDR DL72S002284Frame · crackedFUSELAGE / C1 DOOR OPENING SURROUND STRUCTURE / AFT FRAME / FS 620 : WEB CRACK AND CHORD GOUGE REPAIR NSPECTIONS OF THE AFT DOOR FRAME OF THE C1 DOOR OPENING AT FS 620 REVEALED A .5 INCH CRACK IN THE FRAME WEB JUST BELOW THE #6 DOOR STOP. THE INNER FRAME CHOSDR DL72S002277Skin · wornTHE HORIZONTAL STABILIZER ELEVATOR SKINS WERE FOUND WITH WORN, WITH ELONGATED FASTENER HOLES. THE FASTENER HOLES ARE COMMON TO THE UPPER AND LOWER SKINS AND THE REAR SPAR. REPAIR PER ER/A 396929-14ADSDR DL72S002282Frame · crackedFUSELAGE / C1 CARGO DOOR CUTOUT SURROUND STRUCTURE / FWD FRAME / FS 560 : WEB CRACK REPAIR THE FWD FRAME OF THE C1 CARGO DOOR CUTOUT (FS 560) WAS FOUNDWITH A CRACK IN THE FRAME WEB. THE CRACK WA REMOVED WITH A .75" DIA HOLE THROUGHT THE WEB. THE FRAME WASSDR DL72S001650Oxygen Mask · brokenMICROPHONE JACK FOR O2 MASK IS BROKEN. REPLACED JUMPSEAT O2 MASK ASSY.SDR DL72S001443Casting · crackedON C2 LETTER CK, NR 3 SPOILER O/B ATTACH CASTING CRACKED. REPLACED ANGLE PER MM 57-42-0.SDR DL72S001256Battery Pack · dischargedFOUND EMERGENCY EXIT LIGHT ABOVE L-2 DOOR HAS DEAD BATTERY . R & R EMERGENCY EXIT LIGHT ASSY ABOVE L-2 DOOR OPS CK NORMAL.SDR DL72S992817Stiffener · crackedNR 2 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813.SDR DL72S992816Stringer · crackedSTR 18A CRACKED AT STA 940 AFT SIDE OF RADIUS BLOCK AT AFT LOWER BOLT. REPAIRED PER M/M 53-12-0 PG 816, LEVEL II TIME LIMITED REPAIR.SDR DL72S991813Battery Pack · dischargedLEFT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CK OK.SDR DL72S991177Frame · crackedA .5 INCH CRACK IN R-1 DOOR FWD FRAME EXTENDING FROM LOWER FWD STOP FITTING. REPAIRED PER MM 52-12-0.SDR DL72S990431Pump · damagedAFTER T/O ON INIT CLMB, BOTH HYD SYS B PUMPS LOW PRESS LIGHTS ILLUM. HYD QTY IN A SYS DROPPED TO 2.5 GALS, B QTY APPEARED NORMAL. PRESS THEN DROPPED TO NEAR ZERO, TURNED PUMPS OFF IAW POM 1 TO 2 MINS AFTER ILLUMINATION. FOUND O-RING ON NR 1 B SYS HYD PUMP CSDR DL72S982433Battery Pack · dischargedEMERG LIGHT OVERWING FWD POSITION LT WING INOP. REPLACED BATTERY PACK.SDR DL72S982375Light · inopEMER AREA LIGHT AT WING EXITS IN CABIN INOP. FOUND THAT LAMP AT EXTERIOR WING EXIT SHORTING CIRCUIT. REPLACED LAMP AND BATTERY PACK AND RACK FUSES, OPERATION CHECK GOOD.SDR DL72S980617Frame · corrodedSKIN ATTACH FLANGE AT FS 1166 FRAME WAS CORRODED BETWEEN S28 AND 29 ON THE LT SIDE. REPAIR WILL REQUIRE REACOMMPLISHMENT OF AD92-12-03. REPAIRED PER ERA 331479-14AD.SDR DL72S980616Bulkhead Ftg · damagedTHE BORE OF FS 870 BLKHD LT TERMINAL FITTING WAS O/S TO 4.605 DIAMETER TO REMOVE TOOLING DAMAGE. REWORKED PER ERA 331517-14.SDR DL72S980541Stiffener · crackedA CRACK WAS FOUND IN THE RBL 36.83 VERT STIFFENER ON THE FWD SIDE FO THE FS 1183 BLKHD. THE CRACK WAS LOCATED AT APPROX WL 238 AND WAS APPROX 2. REPAIRED PER ERA 331448-14AD.SDR DL72S980592Fitting · corrodedCORROSION ON BORE OF BODY FITTING LT AFT BTL PIN. ALSO, SOME CORROSION ON EDGE OF FITTING BETWEEN WING AND BODY FITTING. REMOVED CORROSION PER 53-40-1 FIG 4. REWORKED NR 1214 BORE, REPAIRED ON NR 1214 AS PER ERA 331517-14.SDR DL72S980667Angle · crackedDURING SHOP INSPECTION, THE FLAP REAR CHORD ANGLE WAS FOUND CRACKED 32 AND 37 FROM THE IB END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.SDR DL72S980666Angle · crackedDURING SHOP INSPECTION, THE FLAP WAS FOUND WITH A CRACKED REAR CHORD ANGLE. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.SDR DL72S980518Web · crackedINSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED ON LT SIDE. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DRILLED CRACK AND DYE CHECK PER SRM 53-10-4. OK TO INSTALL DOUBLER. INSTALLED DOUBLER.SDR DL72S980517Web · crackedDUPLICATE ORIGINAL SOILED. INSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED AT 2 LOC ON RT SIDE. REMOVED SECTION OF ANTI-ICE DUCT AND X BRACE FOR ACCESS. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DRILLED CRACK AND DYE CHECKED PER SRM 53-10-4. SDR DL72S980557Frame · crackedITEM: FRAME CRACKED STA 930 ABOVE 14 LT MARKED. REPAIRED PER SRM 53-10-4 FIG 25.SDR DL72S980613Bulkhead Skin · crackedAT HMV, FOUND APU BLEED AIR CUTOUT FWD BLKHD RT W/W SKIN CRACKED. REPAIRED PER SRM 53-10-9 FIG 5.SDR DL72S980612Frame · crackedITEM: AT HMV TEMPORARY REPAIR LMLG UPLOCK FITTING SUPPORT FRAME AFT WEB. REPAIRED PER MM 53-11-0 FIG 814.SDR DL72S980750Angle · damagedAFT LOWER CHORD ANGLE IS DAMAGED 29 FROM O/B END OF NR 2 MIDFLAP. REPAIRED PER M/M 57-52-0 FIG 802, INSTALLED DOULBER.SDR DL72S971267Hydraulic Line · rupturedSYSTEM A HYDRAULICS TOTAL FAILURE 10 MIN INTO FLIGHT. BY POM ELECTRICALLY OPERATED FLAPS AND CRANKED NOSE GEAR DOWN. MAIN GEAR DOWN BY ALTERNATE METHOD. ALL HAPPENED AT 10,000 FT AND 250 KTS. REPLACED LOWER RUDDER POWER CONTROL UNIT PRESSURE LINE, SERVICEDSDR DL72S970491Rudder · deflectionON TAKEOFF ROLL 10 KNOTS BEFORE V1, RUDDER KICKED HARD LEFT TWICE IN RAPID SUCCESSION CAUSING ABRUPT NOSE DEFLECTION. TAKEOFF WAS CONTINUED DUE TO HIGH WEIGHT AND HIGH SPEED.SDR DL72S962690Web · crackedFOUND DURING F-2 LETTER CHECK, 3 EA .5 INCH CRACKS LWR TORQUE BOX WEB STA 1219 TO 1224 LEFT SIDE. REPAIRED PER M/M 53-11-0.SDR DL72S962689Angle · corrodedFOUND DURING F-2 LETTER CHECK, CORROSION AT FUSELAGE BELLY PANEL 3348L FWD HINGE SUPPORT. REPAIRED PER M/M 53-30-01.SDR DL72S961397Frame · crackedFOUND CRACKS AT THE LT AND RT FRAMES AT STA 784. REPAIRED BOTH CRACKS PER BAC S/B 727-53-0197, REV 2.SDR DL72S961396Skin · corrosionFOUND CORROSION SLIGHTLY AFT OF C-3 DOOR OPENING BEAR STRAP. REPAIRED PER ER/A 303676-14.SDR DL72S961358Torque Box · crackedAT MID-VISIT, THE AFT STAIRWELL RT TORQUE BOX WAS FOUND CRACKED AT THE UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0.SDR DL72S961469Blkhd Stiffener · crackedCRACKS WERE FOUND EMANATING FROM THE BOTTOM OF THE FLANGE ON THE VERTICAL STIFFENERS LOCATED AT THE BOTH LBL AND RBL 8. REPAIRED PER B727 S/B 727-53-0175, REV 2.SDR DL72S961284Bulkhead · crackedCRACKS EMANATING FROM VERTICAL STIFFENERS AT LBL AND RBL 8 ON STA 1183 BULKHEAD. REPAIRED PER EO 4-59275-3AD.SDR DL72S961300Trunnion Ftg · corrodedAT MID VISIT, THE NLG TRUNNION FITTING WAS FOUND TO BE CORRODED. REPAIRED PER MM 53-40-0.SDR DL72S961299Trunnion Ftg · corrodedAT MID VISIT, BORE OF NLG FITTING WAS FOUND TO BE PITTED. AREA SPOTFACED, BORED DYE CHECKED, ROTOPEENED AND BUSHING INSTALLED PER M/M 53-40-0.
Back to N522DA, cancelled Apr 2, 2013