Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72S011869Angle · crackedNBR 3 SLAT AFT ANGLE CRACKED AT ACTUATOR ROD END ATTACH REPAIR PER MM 57-54-000-8 FIG 807SDR DL72S011854Battery · dischargedEMERGENCY LIGHT ABOVE 1L DOOR INOP.___BATTERIES DEAD. _REPLACED BATTERIES IN LIGHT ASSY. OP CKS NML.SDR DL72S011849Light · inoperativeEMERGENCY EXIT LIGHT OVER CENTER AISLE BETWEEN 2L AND 2R DOORS INOP. RELAMPED LIGHT ASSY AND OPERATION NORMAL.SDR DL72L011847Transmitter · failedAFTER T/O RUDDER OSCILLATIONS FOLLOWED POM PROCEDURE. FOUND POSITION TRANSMITTER COIL OPEN REMOVED AND REPLACED POS XMTR PER MM ADJ/TEST OF YAW DAMP CHKS GOOD PER MM.SDR DL72L011845Coupler · intermittentON TAKEOFF SLIGHT RUDDER OSCILLATIONS WITH HIGH WIND. AFTER TAKEOFF EXCESSIVE RUDDER MOVEMENT. FOLLOWED YAW DAMP INOP POM PROC. NO HELP. REMOVED AND REPLACED UPPER AND LOWER YAW DAMP COUPLERS PER M/M. SYSTEM TEST NORMAL.SDR DL72S011829Power Supply · dischargedFIRST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED FIRST CLASS EMERGENCY LIGHT POWER SUPPLY/CHARGER.SDR DL72S011822Light · inoperativeL1 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.SDR DL72L011814Engine · shutdownNO 2 ENG SHUTDOWN INADVERTENTLY IN FLT AT FL270. RESTARTED ENGINE WITH ALL PARAMETERS NORMAL. OPERATED NORMALLY FOR DURATION OF FLIGHT. PERFORMED WINDMILL INSPECTION AND CHECKED CHIP DETECTORS AND OIL FILTER. ALL NORMAL, OK FOR SERVICE.SDR DL72S011803Battery · dischargedON LAYOVER FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY.SDR DL72S011801Battery · dischargedON L/O FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT TURN ON BRIGHT WHEN EMERGENCY LIGHTS TURNED ON. REPLACED BATTERIES AND LIGHT ASSY, OPS CHECKS OK.SDR DL72S011797Light · unserviceableEXIT SIGN ABOVE 1L DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TESTED. REPLACED LIGHT ASSYSDR DL72S011793Actuator · leakingLOST A SYSTEM HYDRAULICS ON CLIMBOUT FROM ABQ. LOST PRESSUREAND QUANTITY BOTH TO ZERO. _REPLD NBR 3 L/E FLAP ACTUATORSDR DL72S011790Door Frame · crackedTHE FWD FRAME OF THE C1 DOOR OPENING AT FS 560 WAS FOUND WITH TWO WEB CRACKS AT EXISTING FASTENER LOCATIONS BELOW THE UPPER DOOR SILL. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0219 AND AD 99-23-13. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH A TITANSDR DL72S011774Light · inoperativeBOTH AFT SERVICE DOOR SLIDE LIGHTS INOP. RELAMPED BOTH BULBS AND REPLACED BATTERY PACK FOR M983.SDR DL72S011770Light · inoperativeRIGHT AFT OVERWING AND LT FWD OVERWING EMERGENCY EXIT LIGHTS INOP ON EXTERIOR OF ACFT. REPLACED LAMPS, RACKS AND BATTERIES. ALL POSITIONS OPERATIONAL EXCEPT LT FORWARD POSITION. RECRIMPED SPLICE 2480 REF WDM 33-51-01. OPS CHECKS GOOD.SDR DL72S011765Battery · dischargedAFT AIRSTAIR EMERGENCY LIGHT VERY DIM. REPLACED BATTERIES.SDR DL72S011727Light · inoperativeFWD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.SDR DL72L011689Engine · power lossON TAKEOFF ROLL, N1 ROLLED BACK TO 80 PERCENT, EPR FOLLOWED. THROTTLE PUSHED BACK UP, ROLLED BACK AGAIN. INSPECTED FCU BURNER PRESSURE LINE, OK. SERVICED BELLOWS AND RAN PER PFHB, NO TROUBLE FOUND.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 DL72S011722Slat · crackedMULTIPLE RIBS CRACKED,REPAIRED PER AMM 57-54-000-8 FIG 814SDR DL72S011661Battery Pack · dischargedLT FWD O/W SLIDE LIGHT INOP. REPLCD BATT PACK. OPS CKS GOODSDR DL72S011659Compressor · stalledAT APPROX 80 KTS WITH POWER STABILIZED, AT45 (194/197/194) WINDS 170/17, AIRSPEED AT 90 KTS NR 2 ENG COMPRESSOR STALLED. EPR DROPPED TO APPROX 1.70 AND RECOVERED. PERFORMED BORESCOPE AND COMPRESSOR WASH, NO DAMAGE FOUND.SDR 01FDEA00881Transmitter · faultyNR 1 ENG OIL PRESS GAUGE IND 20 PSI PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED NR 1 OIL PRESS TRANSMITTER PER MM 79-33-001-2. OPS & LEAK CHECK GOOD.SDR DL72S011655Actuator · malfunctionedUPON FLAP RETRACTION FROM 2 TO 0, NR 7 L/E SLAT STAYED FULLY EXTENDED WITH FLAPS UP. VERIFIED AT S/O PANEL. APPROX 45 SECS LATER, NR 7 L/E SLAT RETRACTED ON ITS OWN. NO HYD PRESSURE OR QUANTITY FLUCTUATIONS NOTED. AIRCRAFT DID HAVE A ROLLING TENDENCY (ATLMSDR 01FDEA00818Sequence Valve · corroded01-327 AFT GEAR IN UP POSITION L/G DOOR LIGHT REMAIN ON. R/R NR 1 & 2 ENGINE DRIVEN HYD PUMPS PER MM 29-11-000-2. & LG LOCK OPERATING SEQ VALVE.SDR DL72S011548Battery Pack · dischargedRT OVERWING EXTERIOR AFT EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHT CKS OK.SDR DL72S011547Battery Pack · dischargedRT WING EXT OVERWING MID EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHTS CK OK.SDR DL72S011546Battery Pack · dischargedLT AND RT AFT SVC DOORS EXTERIOR EMERGENCY SLIDE LIGHTS INOP. RELAMPED, NO HELP. REPLACED BATTERY PACK. LIGHTS CK OK.SDR DL72S011531Web · crackedCRACK AT UPPER FASTNER VERTICAL WEB L/H SIDE STA 1223 REPAIRED PER M/M 57-11-000-8SDR DL72S011522Module · damagedON LANDING ROLLOUT HYD SYS -A- PRESS AND QTY WENT TO ZERO. FOUND -A- SYS ELEV CONTROL MODULE DAMAGED. SOLENOID BLEW OUT OF THE TOP OF MODULE. REPLACED MODULE.SDR DL72S011513Filter · dirtySYSTEM A O-HEAT LIGHT CAME ON JUST PRIOR TO CRUISE. REPLACED A-SYSTEM RETURN FILTER MODULE.SDR 01FDEA00831Line · looseNR 3 ENG STRUT O/H LIGHT ILLUM DURING CLIMBOUT. RAN ENG WITH BOTH PACKS AT HIG 5 MIN, NO O/H LIGHT. TIGHTENED LEAKING THRUST REVERSER FLEX LINE. OK FOR SERVICE.SDR 01FDEA00815Connector · dirtyON DEPARTURE NR 3 STRUT O/H LIGHT CAME ON. REMOVED, CLEANED NR 3 ENG LOOP CONNECTOR PER MM REF ATA 20. RESECURED STRUT PANELS.SDR DL72S011518Bulkhead · crackedFUSELAGE / BULKHEAD / FS 351.2 / LBL 5 : WEB CRACK REPAIR THE FS 351.2 BULKHEAD WEB WAS FOUND CRACKED AT LBL 5 AT A DAMAGED NLG UPLOCK FITTING ATTACH POINT. THE WEB AND LOCAL BULKHEAD CHORD WERE SDR DL72S011446Skin · corrodedFUSELAGE / SKIN / FS 1150 / STRG. 29R : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND WITH A SMALL AREA OF CORROSION JUST AFT OF THE FS 1150 FRAME AND JUST OUTBD OF STRINGER 29R. THE CORROSION SDR DL72S011445Sill · corrodedFUSELAGE C2 DOOR OPENING LOWER SILL OUTER CHORD WAS FOUND WITH AN AREA OF CORROSION ON THE OUTBD SKIN FLANGE NEAR FS 950E+10. THE CORROSION WAS MACHINED AWAY AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND STRAP PER ER/A 381581-14, REV A.SDR DL72S011444Skin · corrodedFUSELAGE / SKIN / FS 1070-1090 / STRG. 27R-29R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1070 & 1090 AND BETWEEN STRINGERS 27R & 29R. THE CORROSION WAS REMOVED WITH A 11.75" X 8" CSDR DL72S011441Reservoir · lowRETURNED TO DFW FOR LOW HYDRAULICS FLUID IN SYSTEM A. SERVICED A SYSTEM TO 4.4 GALLONS. INSPECTED ACFT FOR LEAKS, NONE FOUND.SDR DL72S011501Support · crackedON FINAL WHEN LDG GEAR EXTENDED -A-SYS HYD FAILURE-COMPLETE-GEAR DOWN AND LOCKED FLAPS 30DGS-RAISED FLAP ELEC. TO 15DGS AND LANDED A/C- FOUND NOSEGEAR UPLCKACT.BRACKET CRACKED AND ACT.LINES DAMAGED-RPLCD BRACKET ACTUATOR LINES AND C/W ERA REPAIR TO STA351.5 WESDR DL72S011422Actuator · leakingON LANDING COMPLETE A SYSTEM HYD FAILURE. FOUND OVER CENTER ACTUATOR BULKHEAD FITTING BROKEN AND ACTUATOR LEAKING. CA REPLACED SAME.SDR DL72L011417Bearing · scoredYOKE BINDING IN ROLL AXIS. CHECKS OK ON GROUND. FOUND CAPTS AILERON DISCONNECT CAM AND BEARING PLATE RATCHETING. REPLACED SAME. RIGGED SYS. CHKS NORMAL. REF IPC 27-10-00-07 ITEMS 445-420-410SDR DL72S011404Pressure Switch · intermittentLOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUM IN FLIGHT. OIL PRESSURE WAS NORMAL AND PRECAUTIONARY ENG SHUTDOWN WAS ACCOMPLISHED. REPLACED DIFF PRESS SWITCH AND LOP/FILTER BYPASS LIGHT MODULE ALONG WITH MASTER DIM AND TEST DIODE CARD. RAN ENGS AT HIGH POWER AND ISDR DL72S011416Frame · crackedFUSELAGE FRAME AT FS 970 STR 26L-27L. THE FS 970 FRAME INNER CHORD WAS FOUND CRACKED AT A FLOOR ATTACH LOCATION BETWEEN STRINGERS 26L AND 27L. THE CRACK IS TYPICAL OF BAC S/B 727-53A0195 AND AD 92-12-03.SDR DL72S011400Warning System · malfunctionedDURING CLIMBOUT NR 1 ENGINE LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED. RAN POM PROCEDURE ACCOMPLISHED INFLIGHT SHUTDOWN DUE TO SUSPECTED FILTER BYPASS. ALL OTHER OIL INDICATIONS NORMAL. CA REPLACED AND INSPECTED OIL FILTER. NO TROUBLE FOUND. LEAK CKSSDR DL72S011353Battery Pack · dischargedFWD EMER PATH/OVERHEAD LIGHTS INOP. CA REPLACED BATTERY PACK.SDR DL72S011339Frame · wornTHE INNER CHORD OF THE RH FS 1303 FRAME WAS FOUND WITH A 1INCH AREA OF WEAR ON THE INNER FLANGE JUST ABOVE THE VENTRAL STAIRWAY TORQUE BOX DUE TO CONTACT WITH A LOOSE HYDRAULIC LINE CLAMP. THE DAMAGED AREA OF FLANGE WAS TRIMMED OUT. THE CHORD WAS REPAIRED SDR DL72S011333Beam · crackedINSPECTION OF THE VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER BAC S/B 727-53-0129 AND AD 94-07-08 REVEALED TYPICAL CRACKS IN THE RT HORIZONTAL BEAM AT FS 1263 & 1273. THE CRACKED STRUCTURE WAS REMOVED AND REPLACED WITH NEW STRUCTURE PER ER/A 381539-14AD.SDR DL72S011307Actuator · leakingON FINAL APPROACH PRIOR TO GEAR EXT WITH FLAPS 5 DEG AND HAD INDICATION OF A LOSS OF A SYSTEM HYD. REPLACED A SYSTEM FILTERS. REPLACED LEADING EDGE FLAP ACTUATOR FOR LEAKINGSDR DL72S011304Skin · corrodedFUSELAGE / SKIN / FS 485-500 / STRG. 27R-28R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 485 & 500 AND BETWEEN STRINGERS 27R & 28R. THE CORROSION WAS REMOVED WITH A 13.5" X 8.25"SDR DL72S011300Door Frame · crackedFUSELAGE C1 DOOR OPENING FWD FRAME AT FS 560 CRACKED. INSPECTION OF THE C1 DOOR CUTOUT SURROUND FRAME WEBS PER AD 99-23-13 REVEALED A TYPICAL CRACK IN THE FWD FRAME WEB BELOW THE LIGHT SWITCH WEB CUTOUT ALONG THE OUTER CHORD ATTACHMENT LOCATIONS.
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