Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 99ZZZX3439Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND RT INBOARD FOREFLAP GOUGED, INBOARD OF INBOARD TRACK. BURNISHED GOUGED, ALODINED AND PRIMED. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4.SDR 99ZZZX3438Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND LT OUTBOARD AILERON DELAMINATING ON UPPER OUTBOARD CORNER. REBONDED DELAMINATION PER SRM 51-40-5.SDR 99ZZZX3437Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, RIGHT INBOARD AFT FLAP SKIN CRACKED AT OUTBOARD ATTACH POINT. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-50-4.SDR 99ZZZX3436Strap · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND FLOOR SUPPORT CROSSMEMBER CORRODED AT BS 1030 LBL 45.50 AND LBL 24.75. REMOVED CORROSION PER SRM 51-10-6 AND FOUND OUT OF LIMITS. REMOVED CROSSMEMBER AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1SDR 99ZZZX3435Floorbeam · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND FLOORBEAM CORRODED AT BS 460 LBL 62 TO RBL 62. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR TO UPPER CHORD PER SRM 53-10-8.SDR 99ZZZX3434Floorbeam · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON FLOORBEAM AT BS 360 LBL 62 TO RBL 62. REMOVED FLOORBEAM UPPER CHORD PER SRM 51-30-2. FABRICATED AND INSTALLED NEW UPPER CHORD PER 53-10-8.SDR 99ZZZX3433Support · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON FLOOR SUPPORT AT BS 420 TO BS 460 RBL 62. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-10-8 FIG 6.SDR 99ZZZX3432Extrusion · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION AT UPPER LOBE BS 1030 BL ZERO. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4.SDR 99ZZZX3431Bracket · crackedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND MAIN ENTRY DOOR BRACKET CRACKED AT FORWARD LOWER CORNER. REMOVED DAMAGED BRACKET. FABRICATED AND INSTALLED NEW BRACKET PER SRM'S 51-10-1 AND 51-30-2.SDR 99ZZZX3430Skin · corrodedDURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION AT AFT LOWER CORNER OF LOW CARGO DOOR CUT-OUT, BS 620. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-10-2. FABRICATED AND INSTALLED NEW SUPPORT WEB PER SRM'S 51-10-1 AND 51-30-2.SDR 99ZZZX3424Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND RT OUTBOARD FOREFLAP GOUGED IN LEADING EDGE. BURNISHED GOUGE, ALODINED AND PRIMED, FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4.SDR SCNA99099Bulb · failedDURING LINE MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT LIGHT BULB WAS FOUND BROKEN. REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LENS AND BULB. OPERATIONALLY CHECKS GOOD.SDR DHL9974203CAngle · wornAT C CHECK, ANTI-ICE SUPPORT BRACKETS WORN AT VERTICAL FIN FRONT SPAR. REMOVED AND REPLACED BRACKETS PER SRM 51-30-2 9.25 BY 2 BY .75, N/R 4267.SDR DL72S991666Tr Unit · inopWEATHER RADAR INOP. REPLACED TRANSCVR.SDR SCNA99095Controller · failedUPON DESCENT CABIN BEGAN TO CLIMB AT 1200 FEET PER MINUTE, CLOSED CABIN OUTFLOW VALVE AND CLIMB DIDN'T CHANGE. WENT TO STANDBY MODE AND THEN MANUAL BUT COULD NOT CONTROL PRESSURIZATION. ALL PASSENGER SERVICE UNIT OXYGEN MASKS DROPPED. PRESSURIZED AIRCRAFT ASDR USAA020001Switch · out of adjustFLT 6161 - BOS-LGA - UPON GEAR RETRACTION, AURAL WARNING STEADY HORN SOUNDED. GEAR RETRACTED AND EXTENDED NORMALLY. AURAL WARNING WENT OUT AFTER AT 3 MINUTES AFTER 2ND GEAR RETRACTION. ALL RED LIGHTS REMAINED ILLUMINATED ON GEAR RETRACTION. TROUBLESHOT PROSDR 99ZZZX2824Track · corrodedLOG PAGE 25775. DURING INSPECTION OF AREA DUE TO REMOVAL OF FLAP FOR GROUND DAMAGE, FOUND SHIMS MIGRATED ON PAD A. REMOVED TRACK TO REPLACE. REMOVED AND REPLACED SHIMS AND NR 4 FLAP TRACK IAW BOEING SB 727-57-0178 REV 5. (X)SDR DL72S991590Skin · wornDURING SHOP INSPECTION, THE THE L/E SKIN WAS FOUND WORN ON THE I/B END OF THE FLAP, APP 6 LONG AREA. REPAIRED PER M/M.SDR DL72S991598Skin · bird strikeNR 3 L/E SLAT/UPPER SKIN / OSS 170 - 190 DENT REPAIR. AT SHOP VISIT, THE UPPER SKIN WAS FOUND WITH A LARGE DENT. UPPER SKIN CUTOUT RESULTED IN APPROX 20 X 20 CUTOUT. INCLUDING THE UPPER SKIN AFT OF THE NOSE BEAM AND THE L/E SKIN FWD OF THE NOSE BEAM. EXTESDR DL72S991547Angle · crackedANGLE CRACKED APPROX 3 INCHES AND FASTENERS SHEARED AT FWD SIDE OF NR 7 SPOILER ACTUATOR CASTING. REPAIRED ANGLE PER M/M 57-20-22 PG 809 PER ERA 367745-14 REF NR 64.SDR DL72S991571Floorbeam · corrodedDURING MV1 CORROSION VISIT, NRC 54 CORROSION ON TOP SURFACE OF FLOORBEAM STA 344 FROM LBL 24 TO RBL 12. REPAIRED PER SRM 53-10-8 FIG 11.SDR EISA99141Switch · out of adjustRIGHT MLG LIGHT (RED AND GREEN) CAME ON AT SAME TIME (FALSE INDICATOR) MLG UP AND LOCKED. ADJUSTED F/M MLG TARGET PLATE TO UPLOCK SWITCH. CYCLED UPLOCK MECHANISM. OPS CHECK GOOD. (M)SDR DL72S991482Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT AN EXISTING SKIN REPAIR AT FS 705 AND STRINGER 28R. THE SKIN REPAIR WAS REMOVED, THE CORROSION CUTOUT, AND A NEW ALUMINUM REPAIR DOUBLER INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 367664-14AD, REV A.SDR USAA069965Actuator · failedFLT 6051 - BOS-LGA - AIR RETURNED TO BOS ON TAKEOFF, INBOARD FLAP ASYMMETRY TRIP. NR 5 L/E SLAT LIGHT SHOWED AMBER. ACCOMP ASYMMETRICAL FLAP ABNORMAL CHECKLIST, RETURNED TO BOS. ALL FLAPS EXTENDED ON LANDING. FOUND RIGHT INBOARD FLAP TRANSMITTER STICKING OSDR USAA069964Tube · brokeSYSTEM 'A' SYSTEM HYDRAULIC FAILURE OCCURRED DURING FLAP RETRACTION. FOUND TWO BROKEN HYDRAULIC TUBES IN LEFT AFT STAIR WELL. IPC 29-15-01G, ITEMS NR 375 AND 270. REPLACED SAME AND PERFORMED HYDRAULIC SYSTEM 'A' TROUBLESHOOTING PER MM 29-11-0, PAGE 101. CHSDR 99ZZZM395Tube · brokeSYSTEM 'A' SYSTEM HYDRAULIC FAILURE OCCURRED DURING FLAP RETRACTION. FOUND TWO BROKEN HYDRAULIC TUBES IN LEFT AFT STAIR WELL. IPC 29-15-01G, ITEMS NR 375 AND 270. REPLACED SAME AND PERFORMED HYDRAULIC SYSTEM 'A' TROUBLESHOOTING PER MM 29-11-0, PAGE 101. CHSDR 9902272705Interconnect · leakingON CLIMBOUT OF MKE, CREW NOTICED BOTH HYDRAULIC SYSTEM LIGHTS ILLUMINATED. CREW DETERMINED THAT FLUID LOSS WAS IN 'B' SYSTEM AND CLOSED PUMP SWITCHES. FLIGHT LANDED AT DTW WITHOUT INCIDENT. DTW MAINTENANCE FOUND GROUND INNERCONNECT LEAKING AND REPLACED SAMESDR USAA069962Frame · crackedLEFT BS 870 FRAME HAS HFEC CRACK INDICATION AT STRINGER 18A ATTACH BOLT AFT HOLE IN LOWER ROW. ACCOMPLISHED REPAIR AT LEFT BS 870 FRAME DUE TO CRACK INDICATION AT STRINGER 18A ATTACH BOLT HOLE, AFT HOLE IN LOWER ROW, IAW BOEING TELEX TSI-MIA-99-0008RR. (M)SDR USAA069961Bulkhead · crackedAFT AIRSTAIR EXTERNAL ACCESS PANEL 3902, BS 1183 PRESSURE BULKHEAD CRACKED AT EDGE OF RADIUS BLOCK RBL 16, AT 8 INCHES UP FROM BOTTOM, AND FROM 10 INCH ABOVE BOTTOM TO 14 INCH ABOVE BOTTOM. INSTALLED DOUBLER REPAIR AT FS 1183 PRESSURE BULKHEAD AT EDGE OF RADISDR USAA069960Beam · crackedVERTICAL BEAM IS CRACKED IN BOTH RADIUS LOC AT BS 1183, RBL 36, WL 238. INSTALLED DOUBLER REPAIR ON THE VERTICAL BEAM, BS 1183 RBL 36.83 IAW SB 727-53-0192. MATERIAL USED, 7075-T6, .100 INCH, TWO ANGLES, 48 INCH BY 7 INCH. (M)SDR USAA069959Stringer · crackedSTRINGER 21L IS CRACKED AT OUTBOARD FRAME ATTACH POINT STATION 480. INSTALLED STRINGER REPAIR AT STATION 480, STRINGER 21L AT OUTBOARD FRAME ATTACH POINT. MATERIAL USED, PART NR BAC1498-139, 35 INCH LONG. REPAIR ACCOMPLISHED IAW SRM 53-10-3, FIG 1. (M)SDR USAA069958Stringer · crackedSTRINGER 25R IS CRACKED AT OUTBOARD FRAME ATTACH POINT STATION 460. INSTALLED STRINGER REPAIR AT STATIN 460, STRINGER 25L AT OUTBOARD FRAME ATTACH POINT. MATERIAL USED, PART NR BAC 1498-139, 33 INCHES LONG. REPAIR ACCOMPLISHED IAW SRM 53-10-3 PAGE 3. (M)SDR USAA069955Housing · crackedFORWARD ENTRY DOOR HANDLE MECHANISM HOUSING HAS BROKEN ACCESS HOLE EDGES WHERE PUSH ROD PASSES THROUGH CASTING TO TORQUE TUBE. ACCOMPLISHED FORWARD ENTRY DOOR MECHANISM HOUSING REPAIR IAW AVITAS ENGINEERING DRAWING 99AVHM.029D-1. (M)SDR USAA069954Skin · crackedLEFT ELEVATOR UPPER SURFACE SKIN GOUGED AND FASTENERS BROKEN, ELEV STATION 123.15 TO 132.15. INSTALLED DOUBLER REPAIR AT LEFT ELEVATOR UPPER SKIN, FROM ELEVATOR STATION 123.15 TO STATION 132.15. MATERIAL USED 2024-T3, .032 INCH, 10.5 INCH BY 7.5 INCH. REPAISDR USAA069953Stringer · crackedSTRINGER 21R IS CRACKED AT FRAME ATTACH POINTS STATION 460. INSTALLED STRINGER REPAIR AT STRINGER 21R AT FRAME ATTACH POINTS, STATION 460. MATERIAL USED, CHANNEL, PART NR BAC 1493-412, 10 INCHES LONG, ANGLE; PART NR BAC 1493-513, 10 INCH LONG, STRINGER; PARTSDR USAA069952Frame · crackedFORWARD E/E COMPARTMENT FUSELAGE CIRCUMFERENTIAL FRAME CRACKED AT ATTACHING FASTENERS TO NLG TORQUE BOX VERTICAL STIFFENER, LBL 18.6, AT BS 344 JUST ABOVE HORIZONTAL WALKWAY BEAM CHORD. INSTALLED DOUBLER REPAIR AT FORWARD E/E COMPARTMENT, FUSELAGE CIRCUMFERENSDR USAA069951Stringer · dentedSTRINGER 16L, BS 400 DAMAGED. REPAIRED STRINGER AT LEFT BS 400, STRINGER 16L IAW SRM 53-10-3. MATERIAL USED BAC 1498-140, 19 INCHES LONG, BAC 1498-131 TWO PIECES 12 INCHES LONG. REPAIR ACCOMPLISHED IAW SRM 51-10-3 FIGURE 1. (M)SDR USAA069950Skin · dentedFUSELAGE BS 400, STRIGNER 16L HAS DENT. INSTALLED DOUBLER REPAIR AT LEFT BS 400, MATERIAL USED, 7075-T6, .063 INCH, 21 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIGURE 1. (M)SDR USAA069949Frame · crackedAFT CARGO COMPARTMENT, BS 1010 FRAME IS CRACKED AT UPPER RADIUS LOCATED BETWEEN STRINGER 26L AND 27L. INSTALLED FRAME REPAIR AT AFT CARGO COMPARTMENT, BS 1010 FRAME AT UPPER RADIUS, BETWEEN STRINGER 26 AND 27 LEFT. MATERIAL USED, 7075-T6, .063 INCH, 11 INCH SDR USAA069948Skin · corrodedRIVET HEAD MISSING RIGHT SIDE BETWEEN STRINGER 25R AND 26R AT BS 348.2. INSTALLED DOUBLER REPAIR AT RIGHT BS 348.5, BETWEEN STRINGER 25 AND 26R. MATERIAL USED, 2024-T3, .071 INCH, 12 FT BY 14 INCHES. REPAIR ACCOMPLISHED IAW SRM 53-30-3, FIG 3. (M)SDR DL72S991600Skin · damagedON SHOP VISIT, DAMAGE WAS FOUND TO THE TOP HALF OF THE C1 DOOR, OUTER SKIN. THE SKIN WAS TRIMMED BETWEEN THE NR 3 AND NR 4 STOP BEAMS AND REMOVED TO THE UPPER EDGE. A NEW SECTION WAS FABRICATED AND SPLICE INSTALLED. THE SPLICE CONSISTED OF AN EXTERNAL DOUBLSDR USAA069947Hose · leakingFLT 6540 - DCA-LGA - HYDRAULIC SYSTEM 'A' FLUID DEPLETED TO ZERO. NORMAL LANDING. FOUND NR 1 ENGINE HYDRAULIC PUMP CASE DRAIN LINE FROM FIREWALL TO CASE DRAIN FILTER LEAKING. REPLACED LINE. REPLACED NR 1 AND NR 2 'A' SYSTEM CASE DRAIN FILTERS. (M)SDR SCNA99083Battery Pack · dischargedDURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKS GOOD.SDR SCNA99081Battery Pack · dischargedDURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT BATTERY PACK (M655). OPERATIONALLY CHECKS GOOD.SDR SCNA99082Battery Pack · dischargedDURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE RIGHT FORWARD EMERGENCY LIGHT BATTERY PACK (M1086). OPERATIONALLY CHECKS GOOD.SDR 99ZZZM381Lamp · disconnectedON PREFLIGHT TRANSIT, FOUND EPL TRACK LIGHTS BETWEEN ROW 17-18C INOPERATIVE. RECONNECTED EPL LIGHTS IAW 33-50-0. OPS CHECKED OK. (M)SDR SCNA99709Light · inoperativeDURING HEAVY MAINTENANCE CHECK, THE NO SMOKING SWITCH POPS THE DIM EMERGENCY LIGHT CIRCUIT BREAKER. REPLACED RIGHT HAND AFT OVERWING EMERGENCY LIGHT, OPERATIONS CHECK GOOD IAW B727 MM 335002.SDR SCNA99708Battery Pack · dischargedDURING HEAVY MAINTENANCE CHECK, L1 ENTRANCE WAY EMERGENCY EXIT BATTERY PACK FAILS TO HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW B727 MM 335002. OPERATIONS CHECK GOOD IAW 335000.SDR USAA059909Lamp · failedBOS/LGA - FLT 6181 - EPL LIGHT INOPERABLE, ROW 28. RELAMPED. (X)SDR USAA059908Battery · dischargedBOS/LGA - FLT 6181 - FORWARD SECTION OF EPL INOPERATIVE. REPLACED BATTERY PACK. (X)
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