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 9510632708Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE SKIN BS 683, STR 26L-STR 28L. REPAIRED SKIN (P/N 65-54590-6) PER EA 27-98880.SDR TAOA079501Eel Battery Pack · dischargedFORWARD LEFT OVERWING EXIT LIGHT WILL NOT TEST. PRELACED BATTERY PACK, OPERATIONAL CHECK OK. (X)SDR 9510352709Door · out of rigDURING CLIMB MSP-GEG, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FURTHER INVESTIGATION REVEALED AN AIR LEAK AT THE MAIN CABIN DOOR. DOOR WARNING INDICATED THAT THE DOOR WAS CLOSED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THAT THE DOOR WAS OUT OFSDR 9510602708Frame · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE BS 1303 FRAME WEB BETWEEN STR 8L-9L AND BETWEEN STR 8R-9R. REPAIRED FRAME (P/N 65-17506) PER EA 27-99049.SDR 9510452705Tire · failedDURING TAKEOFF, THE LEFT MAIN GEAR OUTBOARD TIRE RECAP SEPARATED AND INGESTED IN NR 1 ENGINE. THE NR 1 ENGINE COMPRESSOR STALLED. REDUCED THE NR 1 THRUST TO IDLE, JETTISONED 11,000 POUNDS OF FUEL, AND RETURNED TO DEN WITHOUT FURTHER INCIDENT. MAINTENANCE REPSDR 9510322708Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE KEEL BEAM CHORD, STRINGER 29L AT BS 950D AND BS 970 TO 990. REPAIRED CHORD (P/N 65-56441-4) PER EA 27-99048.SDR SCNA95138Eel Battery Pack · dischargedFOUND THE RIGHT WING EMERGENCY EXIT LIGHTS INOPERATIVE IN CABIN. REPLACED BATTERY PACK FOR RIGHT WING EMERGENCY EXIT LIGHTS. LIGHTS OPS CHECKED GOOD.SDR 95ZZZX3958Duct Shims · failedON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON, THROTTLE BACK LIGHT WENT OUT. RETURNED TO MIA, FOUND AIR LEAK IN AREA OF 13TH STAGE SUPPLY DUCT MOUNT FLANGE. REPLACED SHIMS IN DUCT FLANGE. ENGINE RUN-UP TO TAKEOFF POWER AND LEAK CK FOUND OK.SDR 95FDEA00825Shear Tie · corrosionCORROSION ON SHEAR TIE AND FRAME AT BS 950 RBL 10 TO 15 WL 150. REPLACED AFTER CUT OUT, PER FEDEX SRM 53-10-4.SDR 95ZZZX3633Hose · deterioratedDURING STRUCTURAL INSPECTION, DISCOVERED FUEL SHROUD LEAK AT BS 900 - BS 910. UPON FURTHER INSPECTION, FOUND NR 2 ENGINE FUEL FEED LINE DETERIORATED AND SEEPING AT SLEEVE FITTING. HOSE AGE OVER 22 YEARS.SDR IXKA9500020Actuator · malfunctionedATL-MDW - FLT 79 - ON CLIMB-OUT, NR 8 LEADING EDGE SLAT SHOWS INTRANSIT WHEN FLAP ARE RAISED. AIRCRAFT RETURNED TO ATL. REMOVED AND REPLACED NR 8 LEADING EDGE SLAT ACTUATOR AS PER MM 27-31-32. OPS CHECK OK. (M)SDR 9509672706Engine · malfunctionedNR 1 ENGINE DID NOT REACH TARGET EPR ON TAKEOFF. THE CREW ELECTED TO COMPLETE THE TAKEOFF, JETTISON 5,000 LBS OF FUEL WHILE IN FLIGHT AND RETURNED TO MSP. SUBSEQUENT LANDING OCCURRED WITHOUT INCIDENT. MAINTENANCE TRIMMED AND TESTED THE ENGINE, PERFORMANCE WSDR SCNA95131Eel Battery Pack · dischargedFOUND THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND TRACK LIGHTING TESTED GOOD.SDR SCNA95130Eel Battery Pack · dischargedFOUND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, LIGHT OPS CHECKED NORMAL.SDR 9510932709Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE WING-TO-BODY RIB UPPER CHORD, BOTH UPPER AND LOWER FORWARD FASTENER HOLES BS 760, LBL 70.5. REPAIRED PER EA 27-98428.SDR 9509552709Frame · crackedDURING H-CHECK, FOUND TWO, 2 INCH CRACKS IN THE BS 1303 FRAME BETWEEN THE LEFT AND RIGHT TORQUE BOXES AT THE LOWER LEFT AND RIGHT CORNERS. REPAIRED THE FRAME (P/N 65-17506) PER EA 27-98457.SDR 9509302709Chord · corrodedDURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WELL LEFT SIDE PANEL CHORD FS 336. REPAIRED CHORD (P/N 65-19861-7) PER EA 27-98463.SDR 9509292709Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON STR 29L FROM FS 950B TO 1000. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98455.SDR 9509282709Longeron · crackedDURING H-CHECK, FOUND CORROSION AND CRACKS ON STR 29R FROM BS 950E TO 985. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98461.SDR 9509542709Rib · crackedDURING H-CHECK, FOUND CRACKS IN THE RIGHT WING-TO-BODY UPPER RIB CHORD BS 760 AT RBL 70.5. REPAIRED CHORD (P/N 65-18522-14) PER EA 27-98434.SDR 9509122709Mount · corrodedDURING 'H' CHECK, FOUND CORROSION IN THE NR 2 ENGINE AFT MOUNT FITTING, AFT FLANGE. REPLACED FITTING PER SRM 54-40-1, PG.1-2.SDR CALA950478Chord · corrodedDEN - INSPECTION FOUND CORROSION ON THE NLG CHORD AT STA 294L WL 148. A REPAIR WAS INSTALLED PER SRM 51-40-4. (W)SDR CAL950477Blkhd Doubler · corrodedDEN - INSPECTION FOUND CORROSION ON ANGLE DOUBLER AT STA 1183 PRESSURE BULKHEAD BEAM. A DOUBLER WAS FABRICATED AND INSTALLED PER BOEING DRAWING 69-60242. (W)SDR CAL950425Line · worn throughEWR - FLT 0376 - THE CREW REPORTED B-SYSTEM HYDRAULIC QUANTITY LOSS IN-FLIGHT. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF B-PUMP LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE TO B-SYSTEM MODULE IN THE HYDRAULIC BAY WORNSDR 95ZZZM83Door · not sealedRETURN FROM FLIGHT, A HISSING SOUND WAS HEARD JUST AFTER VR COMING FROM THE L-1 CABIN DOOR AREA. THE AIRCRAFT FAILED TO PRESSURIZE, CAPTAIN DECIDED TO RETURN TO MYR. AFTER LANDING MAINTENANCE INSPECTED THE DOOR AND FOUND EVERYTHING TO BE NORMAL, NO DISCREPANSDR SCNA95103Eel Power Supply · failedAFT AIRSTAIR OVERHEAD LIGHTS DID NOT TEST. REMOVED AND REPLACED POWER SUPPLY FOR AFT AIRSTAIR EMERGENCY LIGHTS IAW 33-50-61. LIGHTS CHECKED GOOD.SDR SCNA95102Eel Power Supply · failedAFT ENTRY EMERGENCY LIGHT DID NOT TEST. REMOVED AND REPLACED AFT ENTRY OVERHEAD POWER SUPPLY IN OVERHEAD LIGHT IAW MM 33-50-101.SDR IXKA9500021Fuel Pump · malfunctionedMCO-ATL - FLT NR 22 - DURING CLIMB-OUT, NR 2 ENGINE N1 ACCELERATED TOWARD RED LINE, THROTTLE RETARDED AND N1 STABILIZED AT 80 PERCENT. NO RESPONSE TO THROTTLE MOVEMENT. ENGINE SHUTDOWN NORMAL AFTER AIR RETURN TO MCO. REMOVED AND REPLACED FUEL PUMP AND FUEL SDR 95ZZZM206Fuel Control · malfunctionedMCO-ATL - FLT NR 22 - DURING CLIMB-OUT, NR 2 ENGINE N1 ACCELERATED TOWARD RED LINE, THROTTLE RETARDED AND N1 STABILIZED AT 80 PERCENT. NO RESPONSE TO THROTTLE MOVEMENT. ENGINE SHUTDOWN NORMAL AFTER AIR RETURN TO MCO. REMOVED AND REPLACED FUEL PUMP AND FUEL SDR 9508092704Brake · damagedAFTER DEPARTURE, TOWER NOTED TIRE CARCASS ON RUNWAY. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 4 MAIN LANDING GEAR TIRE AND BRAKE DAMAGED. IN ADDITION, DAMAGE WAS SUSTAINED TO FORE, MID, AND AFT TRAILING EDGE FLAP. DSDR 9508002708Actuator · failedDURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE UNSAFE INDICATION REMAINED ILLUMINATED. CAPTAIN REQUESTED CFR TO STANDBY AND RETURNED TO MKE WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED JUMPER ON NR 8 LEADING EDGE SLAT AND DEFERRED ACTUSDR TAOA059508Apu · leaking oilPRIOR TO BOARDING, APU FILLED CABIN WITH SMOKE. FOUND OIL ON GROUND AROUND APU AND APU COVERED WITH OIL. M841141 ASSIGNED PER MEL SEQ 49-1. MAINTENANCE LATER REPLACED APU ASSEMBLY. (W)SDR 9508282707Chord · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT INBOARD MID FLAP UPPER MID SPAR T-CHORD WBL 70.6. REPAIRED PER EA 27-098378.SDR 9508262707Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 29L BETWEEN FS 970 TO 1010. REPAIRED LONGERON P/N 65-56441-3, PER EA 27-98377.SDR SCNA95096Eel Assy · failedCOCKPIT EMERGENCY EXIT SIGN INOPERATIVE WITH EMERGENCY LIGHT SWITCH ON. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD.SDR 95ZZZX3397Bolt · shearedON POST FLT INSPECTION, FOUND NR 3 TIRE/WHEEL ASSEMBLY MISSING FROM AIRCRAFT. REPLACED NR 3 AXLE SLEEVE AFTER AXLE INSPECTION. REPLACED NR 3 AND NR 4 BRAKES. REPLACED THE NR 3 AND NR 4 TIRE/WHEEL ASSEMBLIES. ACCOMPLISHED TIRE BURST INSPECTION IAW MM 32-40-SDR 95ZZZX2858Mount · lug crackedDURING C-CHECK INSPECTION, FOUND NR 2 SLAT ACTUATOR INBOARD TRUNNION MOUNT LUG CRACKED.SDR 95ZZZX2857Skin · corrodedDURING C-CHECK INSPECTION AND C.P.C.P. INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CORRODED AT BS 500, STR 27L (APPROXIMATELY 3 INCH AREA). CORROSION OUT OF LIMITS.SDR 95ZZZX2856Floorbeam · corrodedDURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM AT BS 1090, B.L.O., CORRODED OUT OF LIMITS (4 INCH AREA).SDR 95ZZZX2855Intercostal · angle crackedDURING C-CHECK INSPECTION, FOUND INTERCOSTAL UPPER ATTACH ANGEL CRACKED FIVE PLACES BETWEEN FLOOR BEAM 950A AND 950B, B.L.O.SDR 95ZZZX2854Skin · crackedDURING C-CHECK AND C.P.C.P. INSPECTION, FOUND 5 INCH CRACK ON SKIN KEEL BEAM AREA BETWEEN STA 930 AND STA 940 RIGHT.SDR 95ZZZX2853Intercostal · corrodedDURING C-CHECK INSPECTION, FOUND INTERCOSTAL Z-CHANNEL CORRODED OUT OF LIMITS FORWARD AND AFT OF FLOOR BEAM AT BS 1050, BL 12L.SDR 95ZZZW716Actuator Switch · defectiveLEADING EDGE SLAT 'AMBER' LIGHT ON FORWARD INSTRUMENT PANEL 'ON' WITH FLAPS RETRACTED. INDICATION WAS CONFIRMED ON FLIGHT ENGINEER'S PANEL. NR 1 LE SLAT SHOWED INTRANSIT. RECYCLED FLAPS, NO HELP. AOM PROCEDURES FOLLOWED. ADVISED ATL ATC AND RETURNED TO CHSDR 9507582705Bypass Switches · malfunctionedEN ROUTE TO MEM, THE NR 2 ENGINE OIL FILTER BYPASS WARNING ILLUMINATED. THRUST WAS REDUCED TO IDLE. THE FLIGHT CONCLUDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL FILTER BYPASS AND LOW OIL PRESSURE SWITCHES. AN INSPECTION OF THE OIL FILTER REVEALED NOSDR 9507502703Actuator · failedDURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE SLAT REMAINED EXTENDED. FOLLOWED ASYMMETRICAL LEADING EDGE DEVICE PROCEDURE TO NO AVAIL. FLIGHT RETURNED TO BNA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 8 SLAT ACTUATOR. LEAK ASDR SCNA95095Eel Battery · dischargedFORWARD CEILING MOUNTED AREA EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SELF-CONTAINED BATTERY. OPS CHECK GOOD IAW MM 33-50-81.SDR 9507022703Longeron · crackedDURING PERIODIC CHECK, MAINTENANCE FOUND FUSELAGE BELLY SKIN AND SURROUNDING STRUCTURE STR 29R, FS 980 TO 1015 CORRODED AND CRACKED. REPAIRED PER NWA EA 27-096533 (MFG PART NUMBER 65C1391-1).SDR 9507012703Frame · crackedDURING PERIODIC CHECK AND SCHEDULED REMOVAL OF AFT LEFT GALLEY SERVICE DOOR, SHOP MAINTENANCE FOUND FORWARD FRAME CRACKED AT UPPER HINGE CUTOUT, LENGTH .5 INCH. REPAIRED PER NWA EA 27-096522 (MFG PART NUMBER 65-56992-3).SDR SCNA95107Floorbeam · corrodedDURING C-CHECK, FOUND THE MAIN FLOOR CABIN BEAM AT BS 340 TO 344 CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-10-08 FIGURE 3. ALODINED AND PRIMED PARTS IAW SRM 51-10-02 AND INSTALLED IAW SRM 53-10-08.SDR SCNA95106Actuator · failedDURING C-CHECK, THE NUMBER 1, 2, AND 12 SPOILERS FAILED THE HOLD DOWN TEST PER SUN COUNTRY WORK CARD 3295, STEP 6 - F. REMOVED AND REPLACED NUMBER 1, 2, AND 12 SPOILER ACTUATORS IAW MM 27-61-00.
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