Boeing 727-227
Service difficulty reports · 5,082
Newest first. General aviation reporting is voluntary.
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 = '727227' 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 = '727227' 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 AALA980080Frame · crackedTUL - BELL FRAME CRACKED STA 277 AT STR 16 LEFT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980079Beam · corrodedTUL - SEVERAL AREAS OF CORROSION ON AFT EDGE OF RT HORIZONTAL REAR UPPER CHORD. REPLACED RT AFT HORIZONTAL BEAM. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980078Skin · corrodedTUL - CORROSION COMING OUT AROUND FASTENERS AND SKIN AND BETWEEN SKIN AND STRINGER. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980077Skin · corrodedTUL - CORROSION EMANATING FROM LONGITUDINAL SKIN LAP. INSTALLED EXTERNAL DOUBLER 11 INCHES BY 14 INCHES PER SRM 53-30-3 FIG 14 SHEETS 1 THROUGH 6. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980076Skin · corrodedTUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980075Skin · corrodedTUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980074Skin · corrodedTUL - CORROSION IN SEALANT AT STR 10R STA 990 - STA 1010 AT SKIN LAP. REPAIRED PER SRM 53-30-3 FIG 5 PER ESO 11697 DATED 12-8-97. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980073Skin · corrodedTUL - CORROSION UNDER STR 26R FROM STA 696 TO STA 715. REPAIRED PER SRM 53-30-3 FIG 14. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980072Skin · corrodedTUL - SKIN BULGED OUT AT THE REPAIR STA 552, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980071Skin · dentedTUL - 3 INCH DENT AND GOUGE BELOW STR 24R, STA 332. REPAIRED MINOR DENT IN SKIN PER SRM 53-30-3 PAGE 154 FIG 24 SHEET 4. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980070Skin · corrodedTUL - FUSELAGE SKIN BULGED STA 681 BETWEEN STR 28L AND STR 28R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980069Skin · corrodedTUL - SKIN BULGING AROUND FASTENER HOLE STA 708 OUTBOARD STR 26R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980068Skin · corrodedTUL - LOWER SKIN BULGED AT STR 27R STA 500. INSTALLED EXTERNAL DOUBLER AT STR 27R STA 500 PER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980067Skin · corrodedTUL - SKIN BULGED OUT AT THE FLUSH REPAIR STA 580, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980065Skin · corrodedTUL - SKIN BULGED OUT AND FRONT BROKEN IN SKIN LAP AND DOUBLER, STR 26R, STA 700. DAMAGED AREA REPAIRED PER SRM 53-30-3, FIG 4. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980064Stringer · corrodedTUL - CORROSION AT STR 23L STA 720E TO STA 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980063Stringer · corrodedTUL - STR 27L HAS CORROSION ON BOTTOM AT STA 552 TO STA 555. REPAIRED STR PER SRM 53-10-3 FIG 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980062Stringer · corrodedTUL - CORROSION AT STR 26L BETWEEN STA 680 AND STA 700 (MKD). REPAIRED STRINGER PER SRM 53-10-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980061Stringer · corrodedTUL - CORROSION UNDER STRINGER BETWEEN STA 680 - STA 700. REPAIRED DAMAGED AREA PER SRM 53-10-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980060Stringer · crackedTUL - STR 28L CRACKED, DAMAGED OUTBOARD LEG STA 580. REPAIRED STR PER SRM 53-10-3, FIG 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980058Stringer · crackedTUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER AT 720C. REPAIRED STA PER 53-10-3, FIG 5, SHEET 2. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980057Stringer · crackedTUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER STA 720B. REPAIRED STR PER SRM 53-10-3 FIG 5, SHEET 2. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980055Stringer · crackedTUL - STR 15R CHANNEL CRACKED STA 720B AT RIGHT ZEE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, FIG 5. TST: 67,236. CYCLES: 44,034. (X)SDR 98FDEA00006Fire Loop · leaksENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. FOUND FIRE LOOP NEAR TO AIRFRAME IN TWO PLACES UNDER 5401 PANEL. REARRANGED LOOP. RAN ENGINE TO CHECK FOR AIR LEAKS. FOUND NO AIR LEAKS. CLOSEDSDR AALA980021Light · inoperativeTUL - AFT AIRSTAIR EMERGENCY LIGHT ASSY INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. TST: 67,414.53 HOURS. CYCLES: 44,081. (X)SDR TAOA019801Generator · failedFLT 6041 - BOS-LGA - WHILE ON APPROACH FOR LANDING AT LAGUARDIA AIRCRAFT HAD AN UNDER VOLTAGE ON NR 1 GENERATOR. EXECUTED A GO-AROUND AND RAN CHECKLIST FOR ELECTRICAL FAILURE. REPLACED NR 1 GENERATOR, OPERATIONAL CHECK NORMAL IAW MM CHAPTER 24-20-1. (M)SDR 98FDEA00002Seal · leakingCLIMBOUT FL260 NOTICED THE HYD SYS-A QTY HAD DECREASE TOWARD THE 0 GAL IND WITH NORM SYS PRES OF 3000 PSI. THE FLUID QTY IND BRKR WAS PULL THE RESET. SYS PRESS AND QTY REMAIN SAME, THE HYD SYS-A PUMP LO PRESS LIGHT BOTH FLICKERED AND SYS-A PRESS DECREASE THESDR TAOA129709Lamp · failedNOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION, DOES NOT TEST OF PRESS TO TEST. REPLACED LIGHT BULBS AND FOLLOWED ABNORMAL PROCEDURES. FOUND CIRCUIT BREAKER C709 POPPED ON P-18 PANEL, FOUND SHORTED LAMP IN RUDDER 'A' LOW PRESSURE CAPSULE. RESDR 98ZZZX1961Frame · damagedDURING C-CHECK AT 31J, FOUND FRAME 460 BETWEEN STR 5R AND STR 6R WITH 12 HOLES DRILLED INTO FRAME. INSTALLED DOUBLER REPAIR ON FRAME. ACFT TT: 56,458 HOURS. ACFT TC: 23,698.SDR 98ZZZX1960Skin · crackedDURING C-CHECK, FOUND A 1.50 INCH CRACK ON L/E OF WING SKIN PANEL UNDERSIDE WS 135 AND WS 140. INSTALLED REPAIR PLATE AND ANGLE. ACFT TT: 56,458. ACFT TC: 23,698.SDR 98ZZZX1959Support · crackedDURING D-CHECK AT 31J, FOUND THE FLOOR SUPPORT CRACKED 2 INCHES AFT OF FLOORBEAM AT STA 294.5 RBL 32.5 AT THE THIRD FASTENER FROM THE FLOORBEAM. FABRICATED REPAIR DOUBLER AND INSTALLED. ACFT TT: 56,458 HOURS. ACFT TC: 23,698.SDR TAOA129708Transmission · failedFLT 6450 - DCA-LGA - INBOARD FLAPS SPLIT ON RETRACTION AFTER DEPARTURE, AIRCRAFT RETURNED TO DCA. FOUND NR 5 FLAP TRANSMISSION WITH SHEARED PIN IN FLAP DRIVE UNIT. REPLACED NR 5 FLAP TRANSMISSION. (M)SDR 97FDEA00904Clamp · looseNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. POWER ON NR 1 ENGINE WAS REDUCED AND LIGHT WENT OUT AT APPROXIMATELY 80 PERCENT AND REMAINED OUT. REPEAT WRITE-UP. REMOVED STUB WING PANELS AND INSPECTED PLUMBING. FOUND ONE CLAMP SLIGHTLY LOOSE. RSDR TAOA129707Chain · failedFLT 6140 - LGA-BOS - THE STABILIZER TRIM FAILED. A LOUD BANG WAS HEARD WHEN THE TRIM WAS ELECTRICALLY OPERATED. BICYCLE CHAIN THAT RUNS FROM THE MANUAL CONTROL WHEEL DOWN TO THE CABLE SPOOL HAD SEPARATED. A CLOSER INSPECTION REVEALED THE MASTER LINK ON THE SDR SCNA98020Coffeemaker · sparkingSPARKS NOTICED FROM FOWARD GALLEY COFFEEMAKER WHEN ACTIVATED. REMOVED AND REPLACED COFFEEMAKER AS A PRECAUTIONARY. FUNCTIONALLY CHECKED GOOD.SDR 97FDEA00898Duct · failed97-0255 - DURING TAKEOFF WITH CLIMB POWER SET NR 1 STRUT OVERHEAT LIGHT CAME ON. PULLED THRUST ON NR 1 BACK TO 80 PERCENT N1, NR 1 BLEED OPEN LEFT PACK ON LIGHT GOES OUT. FOUND 8TH STAGE DUCT LEAKING AT FLANGE WELD. REPLACED DUCT JUST OUT BOARD OF PYLON ON SDR 97FDEA00897Heat Valve · malfunction97-0254 - NR 1 ENGINE OIL TEMPERATURE IN YELLOW BAND DUE TO FUEL HEAT VALVE STUCK OPEN. SHUTDOWN ENGINE, AFTER 15 MINUTES TEMPERATURE AT 125C MAX TEMPERATURE 130C LESS THAN 5 MINUTES. WINDMILL 50 MINUTES. PULLED OIL FILTER, FOUND CLEAN. INSTALLED NEW FILTESDR AALA972510Generator · defectiveCCS - FLT 2143 - DURING CRUISE MIA/CCS, NR 3 GENERATOR BECAME INOPERATIVE IN-FLIGHT WITH NR 2 GENERATOR AND APU ALREADY PLACARDED AS INOPERATIVE. LANDED CCS WITHOUT INCIDENT. REPLACED NR 3 GENERATOR AND NR 2 GENERATOR VOLTAGE REGULATOR. SYSTEM GROUND CHECKEDSDR SCNA98019Coffeemaker · sparkingSPARKS NOTICED FROM FOWARD GALLEY COFFEEMAKER WHEN ACTIVATED. OPS CHECKED COFFEEMAKER IN FORWARD GALLEY PER MAINTENANCE MANUAL CHAPTER 253000. FUNCTIONALLY CHECKED GOOD.SDR AALA972390Bulkhead Web · corrodedTUL - BS 178 WL 195-197, CORROSION ON BULKHEAD WEB ABOVE HORIZONTAL ANGLE. INSTALLED DOUBLER PER SRM 53-10-9. (M)SDR AALA972484Indicator · defectiveDFW - FLT 713 - DURING FLIGHT, CREW OPERATED FLAPS ELECTRICALLY. CREW ACCOMPLISHED EMERGENCY CHECKLIST. AIRCRAFT MADE NORMAL LANDING AND WAS NOT OVERWEIGHT. REPLACED OUTBOARD FLAP POSITION INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 97FDEA00890Retract Ind · malfunctionLEADING EDGE DEVICE AMBER LIGHT ON AT 2 DURING FLAP RETRACTION NUMBER 3 AND 4 LEADING EDGE DEVICE INDICATOR LIGHTS SHOWED AMBER. RECYCLED 2 TIMES IN FLIGHT, NO CHANGE. LEADING EDGE DEVICES WERE OK AT 5/15/25/30 ON FLAP RETRACTION. CYCLED SLATS AND FLAPS FORSDR TAOA129702Light · shortedFLT 6541 - DCA - AFTER AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT BASE ASSEMBLY AND BATTERY. OPERATIONAL CHECK NORMAL. (M)SDR AALA972385Frame · dentedTUL - STATION 600, STRINGER 25L AND 24L, TOP FLANGE OF BELTFRAME DENTED, BULGING SIDE OF FRAME BETWEEN 24L AND 25L, DEEPLY DENTED OVER OUTBOARD EDGE OF 24L IN RADIUS OF BELTFRAME UPPER FLANGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED DOUBLER AND INSTALLED SDR TAOA129701Battery Pack · dischargedFLT 6053 - BOS-LGA - RIGHT FORWARD AND AFT ESCAPE HATCH EXIT SIGNS INOPERATIVE. REPLACED FORWARD AND AFT BATTERY PACK AT 18 AND 19 DEF SEAT LOCATIONS. OPERATIONAL CHECK NORMAL. (M)SDR AALA972388Keel Beam Web · crackedTUL - BS 870-874, RBL 6, WL 155-161, RIGHT KEEL BEAM WEB CRACKED AROUND NUMEROUS FASTENERS THROUGH 870 TO KEEL BEAM CHORD ANGLE REPAIR. REMOVED DOUBLER ON CHORD ANGLE FWD RIGHT SIDE OF APU AREA. MADE NEW DOUBLER INSTALLED WITH NEW FASTENERS PER SRM 51-40-4. SDR AALA972387Frame · dentedTUL - FOUND STATIONS 520, STRINGER 25R TO 21R, BELT FRAME HAS NUMEROUS DEEP DENTS, CREASED INTO RADIUS. FABRICATED AND INSTALLED REPAIR ON FRAME PER SRM 51-40-3. (M)SDR AALA972375Frame · corrosionTUL - FOUND CORROSION AT SCREW HOLES AND LOWER FLOORBEAM LOWER CAP. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 51-10-6 AND ESO 11697, DATED 11/11/97. (M)SDR AALA972389Frame · dentedTUL - STATION 520, STRINGER 23L, BELTFRAME DEEPLY DENTED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)SDR AALA972386Frame · dentedTUL - STATION 580, STRINGER 25L TO 23L, BELTFRAME UPPER FLANGE DENTED, DENT AT 23L HAS CREASED RADIUS, DENT AT 25L HAS DENTED DOUBLER AT SPLICE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)
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