Boeing 727-277
Service difficulty reports · 627
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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 = '727277' 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 = '727277' 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 MZZA98220Skin · delaminatedTNN - DURING HALF CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP UPPER SKIN EXISTING REPAIRED AT WBS 177. THE DAMAGED EXISTING REPAIR DOUBLER (5.125 INCH BY 3 INCH IN SIZE) WAS REMOVED AND REPAIRED PER B727 SDR MZZA98219Skin · delaminatedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS ON LEFT WING T/E INBOARD AFT FLAP LOWER SKIN WBL 205. THE DAMAGED SKIN 2.625 INCH DIAMETER WS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR MZZA98218Skin · delaminatedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP LOWER SURFACE EXISTING REPAIRED DOUBLER AT WBL 105. THE DAMAGED EXISTING REPAIRED DOUBLER (14.3125 INCH BY 5 INCH IN SIZE) WAS REMOVED AND RSDR 98ZZZM933Skin · delaminatedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 18.5 INCHES BY 6 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR 98ZZZM932Skin · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON RIGHT WING INBOARD FORE FLAP LOWER SKIN AT WBL 97. THE DAMAGED SKIN 1.5 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-6. (M)SDR MZZA98215Web · oil cannedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1233 AND BS 1253. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER SDR MZZA98214Web · cannedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1323 AND BS 1333. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PSDR MZZA98213Web · canningTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1303 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER SDR MZZA98212Web · oil cannedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1323 AND BS 1333. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PESDR 98ZZZM930Web · oil cannedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1303 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER SDR MZZA98211Battery · dischargedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PASSENGER CABIN EMERGENCY LIGHT BATTERIES WERE FOUND INOPERATIVE. THE BATTERIES, P/N S106, WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL TEST FOUND SATISFACTORY. (M)SDR EISA98242Sensor · malfunctionedCAUTION LIGHT ILLUMINATED ON F/E PANEL FOR MAIN CARGO DOOR DURING FLIGHT. AIR TURN BACK TO BSL. INSPECTED CARGO DOOR PER PEMCO MM 52-32-23. FOUND ALL OPS INDICATORS NORMAL. (M)SDR CA980908028Rim · failed(CAN) FOUND NR 4 MAIN WHEEL RIM MISSING OUTER RIM 90 PERCENT OF CIRCUMFERENCE. TIRE STILL HOLDING PRESSURE. PIECE FOUND ON RUNWAY. REPLACED. PART TC: 182.SDR EISA98204Skin · crackedDURING ACCOMPLISHMENT OF CPCP CARD C53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO 1183. DETECTED ROW OF RIVETS RIGHT SIDE AT STRINGER 25 STATION 680 TO 660 SKIN BULGED AND STRINGER CRACKED WITH CORROSION. REPLACED STRINGER 25 PER SRM 53-10-3 FIG 1 HEAVSDR EISA98184Stringer · crackedDURING ACCOMPLISHMENT OF CPCP CARD C 53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO BS 1183, DETECTED ROW OF RIVETS RIGHT-HAND SIDE AT S25 STA 680 TO STA 660, SKIN BULGED AND STG CRACKED WITH CORROSION. CORRECTIVE ACTION: REPLACED STG 25 PER SRH 53-10-0SDR EISA98183Connector · looseRETURNED TO BRU DUE TO PRESSURIZATION INOPERATIVE. GENERATED FROM PILOT REPORT. CORRECTIVE ACTION: TROUBLESHOT AND FOUND CONNECTOR TO OUTFLOW VALVE LOOSE. RESECURED CONNECTOR SYSTEM. CHECKS GOOD. MM CHAPTER 21. (X)SDR MZZA9818Starter · damagedMNL - FLT CS879 - L/P 7911528 - AIRCRAFT GATE RETURNED DUE TO HEAVY VIBRATIONS ON NR 1 ENGINE DURING START CYCLE. FOUND STARTER TURBINE WHEEL MISSING OUTER PORTION OF ALL BLADES. REMOVED AND REPLACED NR 1 ENGINE PNEU STARTER PER MM 80-11-31. GROUND ENGINE RSDR MZZA98184Valve · failedMNL - FLT CS879 - L/P 7910614 - DURING TAKEOFF ROLL IMMEDIATELY AFTER AN ESPECIALLY HARD JOLT, THE NR 3 FUEL HEAT VALVE LIGHT CAME ON AND OIL TEMPERATURE STARTED RISING. VALVE WAS SELECTED CLOSED AND CYCLING SWITCH WOULD NOT GO FULLY CLOSED. SUBMITTER SUSPECSDR 98FDEA00262Engine · sparksATA: 05-50 98-0098, AFTER TAKEOFF FROM PHL 9L- TOWER REPORTED THAT SEVERAL AIRCRAFT SAW SPARKS FROM RIGHT SIDE OF AIRCRAFT. RETURNED TO PHL FOR INSPECTION. ALL AIRCRAFT SYSTEMS NORMAL, ENGINE PARAMETERS NORMAL, NO PRESSURE PROBLEMS. INSPECTED ALL 3 ENGINE SDR 98FDEA00255Accessory Unit · failedLANDING GEAR LEVER FAILED TO RELEASE AFTER TAKEOFF. AIRCRAFT STUCK IN GROUND FLIGHT MODE. REMOVED AND REPLACED R92. COOLING FAN WORKED BUT LEVER LATCH WOULD NOT PULL. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER 32-09-122, OPERATIONAL CHECK NORMAL.SDR 98FDEA00253Oil Temp Bulb · inoperativeNR 3 OIL TEMPERATURE GAUGE INOPERATIVE. NEEDLE HANGS STRAIGHT DOWN TWITCHES OCCASIONALLY. REMOVED AND REPLACED NR 3 OIL TEMPERATURE BULB PER MAINTENANCE MANUAL 79-32-01.SDR 98FDEA00224Axle · shearedDURING WALKAROUND INSPECTION, FOUND THE NR 1 WHEEL ASSEMBLY AXLE TO BE SHEARED AT THE AXLE NUT. TIRE AND WHEEL REMAINED INTACT ON AXLE. *S/D* REMOVED AND REPLACED MAIN LANDING GEAR INNER STRUT, NR 1 AND NR 2 TIRES AND BRAKES, NR 2 ANTI-SKID DETECTOR. SERVSDR EISA98066Vhf Com · intermittentAFTER TAKEOFF FROM BRU, NR 1 COM WORKED INTERMITTENTLY. AIR TURN BACK TO BRU. PERFORMED NR 1 VHF ANTENNA BONDING CHECK PER MM 23. NO DEFECTS FOUND. ANTENNA COAX AND ANTENNA RESISTANCE NORMAL. REMOVED AND REPLACED NR 1 VHF. (M)SDR 98FDEA00167Fire Warn Light · malfunctionBOTH MASTER FIRE WARNING LIGHTS ILLUMINATE INTERMITTENTLY. ALL FIRE WARNING LIGHTS OFF PRIOR TO TAKEOFF. ONCE AIRBORNE APU FIRE LIGHT CAME ON STEADY. MASTER FIRE WARNING LIGHTS STARTED FLICKERING. REPLACED APU FIRE BOTTLE. FOUND CORROSION ON PLUG D-4858P SDR 98FDEA00116Fire Light · malfunctionedRED LIGHT ON IN AUXILIARY POWER UNIT FIRE HANDLE IN FLIGHT. TOOK OFF AT 0334Z AND NOTICED THE AUXILIARY POWER UNIT RED LIGHT ON AT 0400Z, FLIGHT LEVEL 310. PULLED THE HANDLE AND DISCHARGED THE AGENT. RED LIGHT REMAINED ON BUT WITH VARIATION OF INTENSITY. LSDR 97FDEA00885Fuel Control · malfunctionINFLIGHT, NUMBER 2 THROTTLE BINDING. PERFORMED NR 2 ENG THROT PULL CK, CKS GOOD. REMOVED AND REPLACED NR 2 ENG FUEL CNTRL AND FUEL DIFF PRESS SWITCH LEAK AND OPER CK GOOD PER M/M 73-21-0 AND JET RUN HDBK 6-39. PULL CK PER 76-11-0. INSP CABLE AND PULLEY IN SDR EISA97227Connector · looseON CLIMB-OUT AT BGY F/OS AIRSPEED INDICATOR DECREASED TO ZERO, ON APPROACH INDICATOR BEGAN TO CLIMB BUT NEVER REACHED NORMAL INDICATION. FOUND PITOT CONNECTION LOOSE ON F/O AIRSPEED INDICATOR. RESECURED CONNECTION. PITOT LEAK CHECK GOOD MM 34-11-0. (M)SDR CA971104008Brake · sheared(CAN) NR 3 BRAKE WAS FOUND WITH RIVETS THAT ATTACH THE LINING TO THE TORQUE TUBE SHEARED AND BROKEN METAL PARTS OF LINING DAMAGED. BRAKE REPLACED.SDR 97FDEA00774Duct · broken97-0210 MTY NR 3 ENGINE FIRE WARNING CAME ON APPROXIMATELY 1 MINUTE AFTER SELECTING CLIMB POWER. ALL ENGINE INSTRUMENTS WERE NORMAL. FIRE LIGHT WENT OUT BEFORE RETARDING NR 3 THROTTLE. FIRE WARNING SYSTEM TESTED GOOD. FOUND 8TH STAGE SADDLE DUCT BROKEN AT SDR 97FDEA00470Retract Mech · malfunctionedDURING DESCENT WITH SPOILER DEPLOYMENT, JET WANTED TO ROLL LT. TOOK FULL AILERON INPUT TO THE RT ABOVE 300-350 KTS. NOT AS PRONOUNCED BELOW 250 KTS. ON LANDING, LT WING WANTED TO DROP WHEN SPOILERS DEPLOYED. HAPPENED BOTH AUTO-PILOT ENGAGED OR DISENGAGED, SDR 97FDEA00382Bolt · jammedBEFORE TAKEOFF CHECK, ELEVATOR JAMMED PULLING AFT ON YOKE. OPENED ACCESS PANELS 9115, 9118, BOUND BOLT AT FORWARD END OF FORWARD TAB ROD ON LEFT HAND ELEVATOR POWER CONTROL UNIT WORKED LOOSE. INSTALLED BOLT, WASHERS, NUT AND SAFETY PER MAINTENANCE MANUAL 27-SDR 97FDEA00358Hyd Motor · failed'A' SYSTEM HYDRAULIC FAILURE. INITIALLY WHEN AT FLIGHT LEVEL 270 THE INBOARD TRAILING EDGE FLAP INDICATOR WENT TO 5' WITH NO LEADING EDGE DEVICES OR ANNUNCIATOR LIGHTS. WHILE RAISING FLAPS WITH ALTERNATE FLAPS SWITCH THE 'A' SYSTEM WENT TO ZERO. FOUND INBOASDR EISA97142Fire Loop · inoperativeNR 3 FIRE WARNING WOULD NOT TEST. REMOVED AND REPLACED FIRE LOOP, REPAIRED WIRING TO CONNECTOR. (M)SDR AU971128Adc · faulty(AUS) NO2 AIR DATA COMPUTER (ADC) FAILED. INVESTIGATION FOUND A DRY SOLDER JOINT ON A PIN CONNECTION AND THE HEAT SINK COMPOUND BETWEEN THE POWER DIODES AND THEIR INTERFACE WITH THE MODULE CIRCUIT CARD HAD DETERIORATED.SDR 97FDEA00264Switch · inoperativeON GEAR RETRACTION ENGINEERS PANEL DID NOT INDICATE AN AMBER RIGHT GEAR DOOR LIGHT DURING SEQUENCE. LANDING GEAR FRONT PANEL SHOWED CORRECT LIGHT SEQUENCE AND EXTINGUISHED RED LIGHT GEAR DOOR LIGHT. MAKING SURE RIGHT GEAR DOORS WERE UP. THE LANDING GEAR WAS SDR AU970480Compressor Case · damaged(AUS) NO1 ENGINE INTERMEDIATE COMPRESSOR CASE HOLED AT THE 12 O'CLOCK POSITION BY THE ENGINE LIFTING BEAM FORWARD ATTACHMENT FITTINGPNO F72714-2 - ENGINE WAS LIFTED WITH ONLY THE UPPER FORWARD CONE BOLT ENGAGED ALLOWING THE ENGINE TO ROLL TO THE RIGHT AND CONTSDR 97FDEA00227Chord · corrodedNR 0302 005. CORROSION (C53-100-01(1)) ON MID LT NOSE CHORD BS 344-350, LBL 16, WL 170. REMOVED AND REPLACED MID LT NOSE CHORD PER BAC DWG 65-18415 AND FED-EX SRM 51-30-2.SDR 97FDEA00229Keel Beam · corrodedNR 0250 004, CORROSION (C53-113-01-1) ON KEEL BEAM AT BS 720F, RBL 7, WL 149. *S/D* REMOVED CORROSION, SPOT FACED, FLAP PEENED AND INSTALLED STRAP AT BS 720F, RBL 7, WL 149 IAW FED-EX EA 7-5310-32976.SDR 97FDEA00222Hinge Fitting · corrodedNR 0468 004, CORROSION ON RT WING O/B AILERON I/B HINGE ON AILERON, WBL 492.0, WSS 655.5. *S/D* REMOVED RT WING O/B AILERON, AND REMOVED I/B AILERON HINGE FITTING AND REPLACED. REINSTALLED AILERON AND FUNCTIONAL TESTED. ALL WORK IAW FED-EX M/M 27-10-31 ANDSDR AU970490Combustor · holed(AUS) NO1 ENGINE NO9 COMBUSTION CAN BURNT THROUGH AT FUEL NOZZLE NUTFACE. FOUND DURING BOROSCOPE INSPECTION. INVESTIGATION FOUND THAT THE PROBLEM WAS CAUSED BY DISCREPANCIES IN THE OVERHAUL OF THE FUEL NOZZLE ASSEMBLIES. PERSONNEL/MAINTENANCE ERROR.SDR AU970464Seal · leaking(AUS) NO1 ENGINE NO9 COMBUSTION CAN FUEL INJECTOR NOZZLE SEAL LEAKING. INVESTIGATION FOUND THAT THE PROBLEM WAS CAUSED BY IMPROPER MAINTENANCE ACTIVITIES DURING NOZZLE OVERHAUL.PERSONNEL/MAINTENANCE ERROR.SDR 97FDEA00230Gusset · crackedNR 0526 002. LEFT STA 783.95 FRAME GUSSET CRACKED AT 2ND FASTENER HOLE ABOVE FLOOR LINE, APPROXIMATELY WL 210, UPPER LOBE ON INBD CHORD OF FRAME. FASTENER HOLE ENLARGED 4/32 O.S. (MAX) PER E.O. 7-5310-7-3367, PT 3. HFEC INDICATES CRACK STILL PRESENT. REPASDR 97FDEA00211Foreflap · delaminatedNR 0349 003, LEFT WING I/B UPPER SURFACE STAINLESS STEEL RUB STRIP DISBONDED. *S/D* REMOVED, REPAIRED AND INSTALLED ON LEFT WING I/B FOREFLAP, I/B UPPER SURFACE STAINLESS STEEL RUB STRIP IAW FED-EX SRM 51-40-6. FUNCTIONAL TEST LEFT WING I/B FOREFLAP OK IAW SDR 97FDEA00208Frame · damageNR 0244 002, DENT IN FRAME AT BS 720A, RBL 15, WL 155. BLENDED OUT DENT AND REPAIRED FRAME BS 720A, RBL 15, WL 155. ALL WORK ACCOMPLISHED PER FED-EX 727 SRM 51-10-2, 51-10-6, 53-10-4. FABRICATED REPAIR PART PER FED-EX SRM 53-10-4.SDR 97FDEA00207Wedge · puncturedNR 0106 001, RIGHT WING I/B MIDFLAP TRAILING EDGE WEDGE PUNCTURED ON LOWER SURFACE 25 FROM INBOARD END. *S/D* REMOVED RIGHT WING I/B AFT FLAP, REPAIRED PUNCTURE ON RIGHT WING I/B MID FLAP T/E WEDGE, INSTALLED RIGHT WING I/B AFT FLAP, REPAIR PERFORMED IAW FEDSDR 97FDEA00206Keel Beam · corrodedNR 0170 002, CORROSION ON KEEL BEAM AT BS 720F TO 720F + 5, RBL 5, WL 148. *S/D* REPAIRED KEEL BEAM IAW FED-EX EA 7-5310-32963.SDR 97FDEA00205Keel Beam · corrodedNR 0169 001, CORROSION ON KEEL BEAM BS 720F TO 720F + 8, LBL 5, WL 148. *S/D* REPAIRED KEEL BEAM IAW FED-EX EA 7-5310-32963.SDR 97FDEA00204Skin · corrodedNR 0260 003, CORROSION UNDER PRESSURE NUT PLATES ON INTERIOR OF SKIN AT BS 704 TO BS 734, RBL 6 TO LBL 6, WL 149. *S/D* REMOVED CORROSION UNDER NUT PLATES ON SKIN, MATERIAL LOSS OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED SKIN BS 704 TO 734, RBL 6 TO LBSDR 97FDEA00188Floorbeam · corrodedNR 0300 004, CORROSION AT NUT PLATE HOLES BETWEEN BLOWOUT PANEL TRIM AND TENSION STRAPS AND BETWEEN BS 680 TO 700, RBL 25 AND 45 WL 200. *S/D* REMOVED DAMAGED TEAR STRAPS. FABRICATED NEW TEAR STRAPS AND INSTALLED AT RBL 25 AND RBL 45 BETWEEN BS 680 TO 700, SDR 97FDEA00189Shear Tie · corrodedNR 0609 005, CORROSION ON SHEAR TIE AT BS 700 IN BETWEEN STR 25 AND STR 26 RT, WL 155. *S/D* REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 700 BETWEEN STR 25 AND STR 26 RT, WL 155, IAW FED-EX SRM 51-302, 51-20-01, 51-10-02, M/M 51-20-151.
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