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 aircraft_model_key = '72725' 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 aircraft_model_key = '72725' 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 07FDEA01038Floor Support · corrodedCABIN FLOOR SUPPORT (BEAM ) HAS CORROSION FS 620, LBL 35. FABRICATED REPAIR ANGLES PER DWG SR27-53-033 AND MAE TRAVELER T7/669736 CUT OUT DAMAGED AREA IAW DWG SR27-53-033. TREATED AND PRIMED CUT OUT DAMAGE IAW SRM 51-10- 2. FABRICATED FILLER FROM 7075-T6 .SDR 02FDEA00565Door Frame · crackedAFT FRAME OF FWD CARGO DOOR CUT OUT CRACK AT THE TIP DOOR STOP FITTING BETWEEN STR 19R - 20R. REMOVED AND REPLACED ANGLE & FILLER ON AFT FRAME PER EA 7-5310-65859.SDR 02FDEA00567Skin · damagedNUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 580 & 600, STR 23R TO STR 26R.SDR DHL2002708009Button · brokenSMOKE DETECTION SYSTEM NR 2 TEST BUTTON BROKE OFF DURING TEST. REPAIRED TEST BUTTON COVER IAW BMM 20-60-01.SDR DHL2002708008Fire Loop · out of positionNR 1 FIRE PROTECTION DETECTOR LIGHT ON. REPOSITIONED FIRE LOOP NR 1 ENG, OPS CHECKED GOOD IAW M/M 26-11-00.SDR DHL2002708007Fire Loop · out of positionENG NR 1 FIRE DETECTION GROUND FAULT LIGHT FLASHES IN FLIGHT. REPOSITIONED ENG NR 1 FIRE LOOP AND REMOVED AND REPLACED NR 1 GROUND FAULT LENS COVER WITH NEW LENS COVER. NO FAULTS DETECTED, OPS CHECKS GOOD IAW MM 26-11-000.SDR DHL2002708006Windshield Wiper · out of adjustCAPTAIN'S SIDE WINDSHIELD WIPER DOES NOT FUNCTION IN THE LOW POSITION THE WIPER DOES NOT HAVE ADEQUATE RANGE OF MOTION TO KEEP THE UPPER PORTION OF THE WINDSHIELD CLEAR. RECLOCKED AND TESTED CAPT'S WINDSHIELD WIPER IAW MM 30-42-01. OPS CHECK NORMAL.SDR DHL2002708005Power Supply · not seatedAPU FIRE DETECT SYS WILL NOT TEST. RESEATED APU FIRE WARNING POWER SUPPLY. OPS GOOD IAW MM 26-15-0.SDR DHL2002708004Light · inoperativeCOCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE IN TEST. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CK NORMAL IAW B727 MM 33-50-1.SDR DHL2002708003Transmission · failedCAPTAIN WINDSHIELD WIPER IS INOP. REMOVED AND REPLACED WINDSHIELD WIPER TRANSMISSION IAW B-M/M 30-42-11, OPS CHECK GOOD.SDR DHL2002708002Light · inoperativeFWD ENTRY EMERGENCY EXIT LIGHT INOP IN TEST POSITION (ON POSITION). REMOVED AND REPLACED FWD ENTRY WAY EMERGENCY EXIT LIGHT ASSY IAW M/M 33-5-00. OPS CHECK SERVICEABLE.SDR DHL2002708001Glare Shield · out of positionF/O'S SLIDING WINDOW IS BINDING AGAINST GLARE SHIELD WHEN TRYING TO OPEN WINDOW. REPOSITIONED GLARE SHIELD AT F/O'S SLIDING WINDOW. OPS CHECK SERVICEABLE PER B727 M/M 56-12-11.SDR DHL2001708016Windshield Wiper · out of adjF/O WINDSHIELD WIPER DOES NOT WORK ON HALF SPEED. RUNS SLOW ON 3/4 SPEED.ADJUSTED WIPER TENSION PER 727 MM CHAPTER 30-42-01, OPS CK SATISFACTORY.SDR DHL2001708014Fire Loop · out of positionNR 2 ENGINE GROUND DET LIGHT ON DIM. OPENED COWLING, CLEARED FIRE LOOP FROM COWLING, CLOSED COWLING AND OP TEST NORMAL PER MM 26-00.SDR DHL2001708015Skin · crackedLEFT WING INBOARD AILERON UPPER SURFACE HAS 2 CRACKS 5.5 INCHES APART. OUTBOARD CRACK APPROX 2.25 INCHES LONG, INBOARD APPROX 2 INCHES. REMOVED EXISTING I/B AILERON SKIN LT SIDE IAW B727 SRM 57-30-2 (UPPER) REPLACED SKIN IAW B727 SRM 57-10-02. INSTALLED UPPSDR 01FDEA00931Hydraulic System · leakingA-SYS QUANTITY DECREASING. SERVICED A-HYD SYS, NO LEAKS NOTED. OK FOR SERVICE.SDR DHL2001708013Fire Loop · out of position1) NR 1 GROUND DETECTOR CIRCUIT ILLUMINATED IN FLIGHT.2) REPOSITIONED NR 1 ENGINE LOOP-NO FAULTS NOTED.OPS CK SATISFACTORILY PER MM 26-11-000.THIS CLEARS DMI 7284.STATUS: CLOSEDSDR DHL2001708012Control Valve · failedLT MAIN GEAR BRAKE DRAGGING ON TAXI OUT. TAXI BACK TO GATE PER PHONE PATCH. MX FLT CONT CVG LT MAIN BRAKE FIRE THERMAL DISCHARGED TIRE 1 TIRE 2 FIRE LAST OVER 45 MIN, FIRE REFLARED UP 3 TIMES IN 45 MIN. CHECKED/INSP SERVICE OF LT MAIN SHOCK STRUT / STRUT ISSDR DHL2001708010Fire Loop · groundedNR 1 FIRE PROTECTION DET CIRCUIT GRD LIGHT ILLUMINATED IN FLT. FOUND ON ENG NR 1 FIRE PROTECTION LOOP WAS GROUNDING ON ENGINE COWLING, REPOSITIONED LOOP IAW B727 M/M 26-11-000 OPS CHECK SERVICEABLE.SDR DHL2001708009Fire Loop · out of positionENGINE NR 1 DETECTOR CIRCUIT GRD WAS ILLUMINATED ON TAXI OUT FROM MCO. FOUND NR 1 ENG LOOP TOUCHING A BRACKET. REPOSITIONED LOOP. SYS NOW OPS CHECK NORMAL PER M/M 26-11-0.SDR DHL2001708008ActuatorIN WINGS LEVEL DESCENT @ 280 KNOTS IAS SPEED BRAKE DEPLOYMENT CAUSES AIRCRAFT TO ROLL TO THE RIGHT. STOWING SPEED BRAKE CAUSES AIRCRAFT TO ROLL ABRUPTLY LEFT 15 DEGREES OPPOSITE DIRECTION YOKE DISPLACEMENT REQUIRED TO COUNTERACT ROLLING MOMENT. PROBLEM STILL PSDR DHL2001708007Controller · malfunctionedWHEN DEPLOYING FLIGHT SPOILERS AIRCRAFT ROLLS RT, WHEN STOWING FLIGHT SPOILERS AIRCRAFT ROLLS ABRUPTLY TO THE RT. INSPECTED ALL SPOILERS FOR DELAM, NONE NOTED. NO ACTUATORS BYPASSING AND LIFT OFF NORMAL. PICK UP NORMAL A&B SYS PER MM 2700.SDR DHL2001708006Computer · faultyDURING CRUISE FLT ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. ELEVATOR FEEL DIFF PRESSURE LIGHT STAYED ILLUMINATED. REPLACED ELEVATOR FEEL COMPUTER PER MM REF 27-30-111. OPS CK GOOD.SDR DHL2001708005Receiver · unserviceableRADAR PAINTS GROUND CLUTTER AT 6 DEG TILT UP, WHEN TURNING PAINTS GROUND.CORRECTIVE ACTION - R&R RADAR RT PER M/M 34-41-01 OPS CK NORMAL. STATUS-CLOSED.SDR DHL2001708003Stud · missingPRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL. SHUTDOWN WHEN OIL PRESSURE STARTED TO DECREASE. ENGINE OIL PRESS/TEMP GOOD UNTIL TOUCHDOWN. PERFORMED ABNORMAL PROCEDURES. N1 & N2 ROTATION GOOD UNTIL TOUCHDOWN. ENGINE NR 1. FOUND GEARBOX THRU STUD FELL SDR DHL2001708004Engine · unserviceableREMOVED AND REPLACED ENG FOR EXCESSIVE OIL CONSUMPTION. REF W/O 600003170. REMOVED NR 1 ENG AND REPLACED PER DHL 727 TASK MANUAL MANUAL 71-01-03 THRU 71-01-18.SDR DHL2001708002Gearbox · leakingNR 1 ENGINE LOST OIL QUANTITY AND PRESSURE IN FLIGHT. COMMENCED ENGINE SHUTDOWN AT INDICATION OF LOW OIL PRESSURE. T/S SYSTEM. REMOVED AND REPLACED N2 GEARBOX IAW P&W MM 72-60. NO LEAKS NOTED ON ENGINE RUN. TESTED OK IAW P&W MM72-00 AND DHL JRH.SDR 01FDEA00106Light · inoperativeNR 3 ENG REVERSER LIGHT ILLUM. REMOVED AND REPLACED REVERSER ACTUATOR COVERS. NEED SOCKET MPN 04-1011-003. ALL CKS GOOD. ALL PNLS REINSTALLED. AC OK FOR SERVICE.SDR DHL2001708001Altimeter · unserviceableALTIMETER SPLIT BETWEEN CAPT AND F/O'S POSITION BY 70 FEET.INSTALLED SERVO-PNUMATIC ALTIMITER IN CAPTS POSITION PER M/M 34-11-0,OPS CHK GOOD.SDR DHL2000708027Sensor · damagedAFTER T/O NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED,ABNORMAL PROCEDURES COMPLIED WITH. PLACED NR 3 ENGINE MODULATING VALVE ON DEFERRAL PER DHL MEL 36-11, DMI 3633.THIS SDR IS STILL OPEN. REMOVED AND REPLACED NR 3 ENGINE MOD VALVE SENSE LINE PER M/M 36-12-4SDR 00FDEA00888Switch · failed00-367 LEFT MAIN GEAR IND UNSAFE LEFT MAIN GEAR DOOR CAME ON AND WENT OUT. R&R LH MLG DOWN LOCK POSITION SWITCH PER MM 32-61-21. OPS CK PER MM 32-61-21.SDR CA001122010Restrictor Valve · failed(CAN) ON DESCENT INTO YEG THE NR 1 ENGINE OIL PRESSURE BEGAN FLUCTUATING BETWEEN 0-35 PSI. IMMEDIATELY FOLLOWING THIS INDICATION THE LOW OIL PRESSURE BYPASS LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN. TROUBLE SHOOTING REVEALED RESTRICTOR GOING TO OIL PRESSURE INDSDR CA001019010Rib · cracked(CAN) DURING A ROUTINE A CHECK IT WAS NOTICED THAT THE NR 8 SLAT ACTUATOR MOUNT WAS CRACKED AT THE ROD END ATTACH POINT. SLAT WAS REMOVED AND MOUNT BRACKETS AND RIB FOUND TO BE BROKEN. SLAT WAS REPLACED AND AIRCRAFT RELEASED. REPLACEMENT PER BOEING M.M. 27-81-SDR DHL200070806CPanel · crackedVERT STAB RT LWR SLIDING SEAL TRACK AREA LWR FIX PANEL HAS 2 CRACKS. REMOVED AND REPLACED PANEL PER SRM 55-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070812CPanel · crackedPANEL NR 3429 I/B LARGE PANEL RADIOUS CORNER CRACK PROGRESSIVE BEYOND STOP DRILL HOLE. CUT OUT DAMAGED AREA AT PANEL PER SRM 51-40-1. INSTALLED DOUBLER REPAIR PER SRM 51-40-2. ALODINE AND PRIMED PER SRM 51-10-2.SDR DHL2000708020Panel · crackedPANEL 5512 MOUNT HOLE CRACK. REPLACED PANEL 12 X 25 INCH PER SRM 51-30-2.SDR DHL200070809CFlange · crackedNR 9 L/E SLAT I/B TRACK O/B MOUNT AFT FLANGE IS CRACKED. ROUTED OUT CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-3. TREATED AND PRIMED PER SRM 51-10-3.SDR DHL2000708012Structure · damagedOUTBOARD FLAP T/E HONEYCOMB DETERIORATING. REPAIRED PER SRM 51-40-1. SIZE OF REPAIR 10 X 3 INCH.SDR DHL2000708005Rib · crackedLEFT WING LEADING EDGE SLAT RIB AFT FLANGE IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-50-3. SIZE OF REPAIR 8 X 2 INCH.SDR DHL200070802CStringer · corrodedEVIDENCE OF CORROSION AT S 23R BETWEEN BS 480 AND 500. REMOVED FASTENERS AND CUT OUT SECTION OF STR 23RT BETWEEN STA 480 AND 500 PER SRM 53-10-3. INSTALLED STR REPAIR PER SRM 53-10-3.SDR DHL200070808CRib · crackedRT WING NR 4 6 L/E SLAT O/B TRACK I/B MOUNT RIB AFT FLANGE IS CRACKED AT HORIZ NUT PLATE STRAP UPPER ANGLE. REMOVED FASTENERS AT NR 6 SLAT O/B TRACK I/B RIB PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. INSP CRACK AT STOP DRILL PER NDT MAN 51-00-00. SDR DHL200070807CFitting · damagedFWD CARGO COMPT RT SIDE BS 480 STATIC PORT FITTINGS PROTECTOR PANEL HAS BROKEN LUG AND MISSING FASTENER. INSTALLED NEW COVER PROTECTOR PER SRM 53-10-2. ALODINED AND PAINTED PER SRM 51-10-2. INSTALLED NEW PLACARD PER MM 20-10-1.SDR DHL200070805CStringer Clip · corrodedFWD BAGGAGE COMPT S-20L AT BS 500 WHERE CLIP ATTACHED TO STRINGER HAS A PIN HOLE AND SUSPECTED CORROSION. CUT OUT DAMAGED AREA PER SRM 53-10-3. TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-3.SDR DHL2000708024Latch · crackedFWD CARGO DOOR UP LOCK LATCH BRACKET LATCH CRACK. REPLACED LATCH PER SRM 51-10-2. MATERIAL USED 10 X 20 INCH.SDR DHL2000708021Angle · shearedSKIN BULGING, FASTENERS SHEARED ANGLE CORRODED AT TAIL SKID RIGHT SIDE STATION 1203. REPAIR PER B727 SRM 51-40-3, 51-30-2, 53-30-2. SIZE OF REPAIR 20 X 10 INCH.SDR DHL2000708006Web · crackedSTA 294.5 STR 15L HORIZONTAL WEB HAS CRACK GOING BEYOND STOP DRILL. REPLACED HORIZONTAL WEB PER SRM 53-10-1.SDR DHL2000708019Pressure Panel · crackedNOSE WHEEL WELL CEILING WEB PANEL SHOW CRACKS RUNNING FROM BS 268.5 AND LBL 20. INSTALLED 13 X 19 INCH DOUBLER PER B727 SRM 51-30-2.SDR DHL2000708007Angle · crackedFUSELAGE LOWER EXTERIOR BS 610 RT SIDE FAIRING PANEL ANGLE SUPPORT SHOWS CRACKS. INSTALL ANGLE SUPPORT. SIZE OF REPAIR 35 X 1 X 4 INCH.SDR DHL200070813CWeb · crackedMCD INTERNAL UPPER ROW OF LIGHTENING HOLES LOWER ROW NR 11 HOLE HAS A CRACK. TRIMMED OUT CRACK PER SRM 51-40-2. INSTALLED DOUBLER PER SRM 51-40-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070810CAngle · crackedMAIN CARGO DOOR FWD EDGE LWR SECTION, SMALL SECTION OF LINING CRACKED. INSTALLED NEW ATTCH ANGLE AT MCD FWD EDGE LWR SECTION PER SRM 51-10-1. TREATED AND PRIMED PER SRM 51-10-2.
Back to Boeing 727-25