Boeing 727-222
Service difficulty reports · 1,723
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 = '727222' 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 = '727222' 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 99UAL900537Stringer · corrodedCORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010 THAT WAS BEYOND ALLOWABLE LIMITS. UAL REPAIR PROCEDURES CUT OUT THE BELLY SKIN TO ALLOW ACCESS TO REPLACE STRINGER 29. DURING THE CUTTING OF THE SKIN THE EDGE MARGIN OF THE FASTENER ROW SDR 99UAL900536Power Supply · failedEEL STRIPS INOPERATIVE IN CENTER PORTION OF CABIN. ALSO, WALL MOUNTED EXIT SIGNS ON LOWER LEFT SIDEWALL BY THE OVERWING DOORS INOPERATIVE. *S/D* REPLACED POWER SUPPLY AND 2 LIGHT SEGMENTS.SDR 99UAL900533Wire · looseEMERGENCY LIGHT OUT ABOVE FORWARD GALLEY DOOR. *S/D* LOOSE GROUND CONNECTION. REPAIRED LOOSE GROUND GD352. WD 33-51-02. OPS CKS GOOD.SDR 99UAL900535Seat · looseAFTER TAKOFF FROM FLL SEAT ROW 14 DEF CAME OUT OF THE TRACK. MOVED PASSENGERS AND CREW WAS ABLE TO PUT ROW OF SEATS BACK INTO THE TRACK. SUPPLEMENTAL DATA UPDATE SECURED SEATS AT ATTACH POINTS.SDR 99UAL900534Unknown · odorUPON ROTATION EXPERIENCED HAZE IN THE COCKPIT ALONG WITH A BURNING RUBBER SMELL. SMELL WOULD GO AWAY AND COME BACK. RETURNED TO ORD AND DID A FLY-BY TO DETERMINE IF THERE WAS A PROBLEM WITH THE GEAR BEFORE MAKING A NORMAL LANDING. *S/D* MAINTENANCE SPECULSDR 99UAL900513Valve · crackedAFTER DEPARTURE FROM BDL, AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE. DIVERTED TO BOSTON. *S/D* FOUND RT MLG LOCK OPERATED DOOR SEQUENCE VALVE ASSY CRACKED. REPLACED VALVE. JACKED AIRCRAFT, ACP'D GEAR SWING FIVE COMPLETE CYCLES AND CYCLED ALL FLIGHT CONTROSDR 99UAL900512Tailskid · damagedPOSSIBLE TAIL STRIKE ON TAKEOFF FROM BDL. TAIL STRIKE ILLUMINATION LIGHT ON. OVER SYR UNABLE TO MAINTAIN PRESSURE. DIVERTED TO CLE. *S/D* REPLACED CYLINDER AND SKID STRIKE PAD, OPERATIONALLY CHECKED OK. ALSO, PERFORMED CABIN PRESSURIZATION SYSTEM CHECK, SDR 99UAL900515Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON BOTH THE RIGHT AND LEFT SIDES WERE FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREAS WERE BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPASDR 99UAL900509Frame · crackedA CRACK WAS FOUND IN THE BODY STATION 760.95 FRAME STUB WEB (P/N 65-16325-18) AT THE CORNER OF AN EXISTING ACCESS HOLE CUTOUT. THE CRACK WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DERSDR 99UAL900504Access Panel · loosePASSENGER REPORTED FUEL DRAINING FROM LEFT WING TIP. CREW REPORTED QUANTITY DECREASING. RETURNED TO ABQ. *S/D* TORQUED NR 15 LEFT HAND WING ACCESS PANEL.SDR 99ZZZM759Clamp · looseFLT 308 - EN ROUTE TO JFK, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. RAN CHECKLIST, LIGHT EXTINGUISHED WITH NR 1 BLEED PACK VALVE CLOSED. FOUND AIR LEAK AT CLAMP ON DUCTING BEHIND PANEL OF THE RIGHT KEEL BEAM IN THE RIGHT WHEEL WELL. SECURED SAME.SDR 99UAL900499Skin · crackedFUSELAGE SKIN AFT OF FORWARD LAVATORY SERVICE PANEL FOUND WITH CRACKS AROUND AREA FASTENERS DUE TO CORROSION. 2024-T3 O.O40 INCH FUSELAGE SKIN AT STATION 312 RT SIDE, BETWEEN STRINGERS S-19 AND S-21 CORRODED. UNDERLYING BEAR STRAP, FRAME AND STRINGERS NOT AFSDR 99UAL900493Battery · dischargedEMERGENCY LIGHT AT DOOR 2R INOPERATIVE. *S/D* REPLACED BATTERIES.SDR GAIA99144BStrut · leakingTOL- ATL - FLT 518 - DURING TAKEOFF, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS SELECTED UP. THE LIGHT ON THE FLIGHT ENGINEERS DOOR WARNING PANEL. THE CREW CARRIED OUT AOM PROCEDURES, AND RETURNED TO TOL MAKING A ROUTINE AND SAFE LANDINGSDR GAIA99142Light · inoperativeDURING ROUTINE INSPECTION, COCKPIT EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 99ZZZM760Bulb · failedFLT 215 - DAY - NR 6 SMOKE DETECTOR IS INOPERATIVE. RELAMPED BEACON LAMP ON NR 6 SMOKE DETECTOR. (M)SDR 99UAL900486Switch · out of adjustAFTER DEPARTURE FROM SYRACUSE, CREW RECEIVED AN AMBER LIGHT INDICATION ON THE AFT STAIR/DOOR. RETURNED TO SYR. ADJUSTED UPLOCK SWITCH. ACTUATED AIRSTAIR SEVERAL TIMES. GROUND CHECKS NORMAL.SDR GAIA99141Switch · out of adjustFLT 518 - TOL-ATL, AFTER TAKEOFF, THE CREW RETRACTED THE GEAR AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO TOL AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIES. ADJUSTED THE NOSE LANDING GEAR DOOR SWITCHES AND PERFORMED A RETSDR 99UAL900481Connector · failedGALLEY HOT PLATE SMOKING AND SPARKING. HOT PLATE CORD FRAYED AND EXPOSED. *S/D* REMOVED HOT PLATES, INSPECTED WIRING FROM GALLEY WALL TO PLATES AND NO DAMAGE, NO OPEN INSULATION, NO BRITTLENESS. INSTALLED NEW CONNECTORS, CLEANED AREA, RECONNECTED HOT PLATESDR 99UAL900480Light · inopEMERGENCY AISLE LIGHT AT STATION 680 IS INOPERATIVE.SDR 99ZZZM761Hose · pluggedFLT 319 - OMA - NR 2 ENGINE OIL PRESSURE EXCEEDED NORMAL LIMITS (61 PSI) AND WOULD NOT RETURN TO NORMAL PRESSURE RANGE, NR 2 ENGINE WAS SHUT DOWN IN ACCORDANCE PROCEDURES AND CHECKLISTS. REPLACED OIL PRESSURE RELIEF VALVE, REPLACED OIL PRESSURE TRANSMITTER. SDR 99UAL900474Spar · corrodedTHE VERTICAL STABLE MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS RSDR 99UAL900469Sill · corrodedCORROSION DAMAGE WAS FOUND ON THE OUTBOARD CHORD OF THE AFT CARGO DOOR LOWER SILL. THE DAMAGED AREA WAS CUT OUT AND REPAIRED WITH A STRIP AND ANGLE REPAIR PER TIMCO REO-06703 REPAIR INSTRUCTIONS. THE REPAIR WAS APPROVED BY FAA FORM 8110-3.SDR 99UAL900455Battery · dischargedEMERGENCY EXIT LIGHT IN CABIN TO OVERWING IS INOPERATIVE. REPLACED ROW 7 BATTERYS IN EMERGENCY LIGHT. OPERATIONALLY CHECKS GOOD.SDR 99UAL900454Air Dist · odorRETURNED TO GATE DUE TO ARCING ODOR IN COCKPIT. CLICKING STATIC ON RADIO. WINDSHEAR INOPERATIVE FAILURE LIGHT STARTED TO FLICKER. ON WAY BACK TO GATE SMOKE BEGAN TO COME FROM UNDER THE INSTRUMENT PANEL. RAN ENGINES WITH ALL SYSTEMS OPERATING, LOOKED BEHINDSDR 99UAL900440Floorbeam · corrodedCORROSION WAS DISCOVERED ON THE UPPER CHORD OF THE STATION 1070 FLOORBEAM (P/N 65-20821-21), CENTERED ABOUT RBL 26. THE DAMAGE COVERS A SPAN OF SIX (6) FASTENER ROWS LOCATED BETWEEN THE RBL 24.75 SEAT TRACK AND THE GALLEY RAIL INBOARD OF THIS LOCATION. A REPSDR 99UAL900439Floorbeam · misdrilledA .1562 INCH DIAMETER HOLE WAS MISDRILLED ON THE UPPER CHORD OF THE STATION 360 FLOORBEAM AT ABOUT RBL 54. THE HOLE GOES THROUGH THE HORIZONTAL FLANGE AND EXTENDS INTO THE VERTICAL WEB OF THE FLOORBEAM. THE DAMAGE WAS REPAIRED PER THE INSTRUCTIONS GIVEN IN TSDR 99UAL900438Keel Beam · misdrilledA DOUBLE DRILLED HOLE WAS FOUND ON THE LOWER FLANGE OF THE STRINGER 29 RIGHT KEEL BEAM CHORD AT STATION 950C. THE HOLE WAS TRIMMED OUT AND A REPAIR STRAP INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY FAA FORM 8110-3.SDR 99UAL900434Hook · failedNR 3 LEADING EDGE SLAT DID NOT RETRACT. VERIFIED BY VISUAL CHECK. *S/D* FOUND SLAT HOOK CRACKED. REPLACED SLAT.SDR 99UAL900430Stringer · corrodedCORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010. CORROSION WAS BEYOND ALLOWABLE LIMITS. THE ADJACENT STRINGER 29 RIGHT HAD BEEN REPLACED AT A PREVIOUS VISIT AND THE REPAIR TO THE SKIN FOR THAT REPLACEMENT ALSO INCORPORATED DAMAGE TO TSDR 99UAL900429Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THSDR 99UAL900428Elbow · crackedDURING CLIMB, FEEDING FUEL FROM NR 2 TANK, TANK NR 1 DROPPED 1,000 LBS. CONDITION CORRECTED WITH CROSSFEED. *S/D* FOUND CRACKED ELBOW OF THE NR 1 FUEL VENT SYSTEM. REPLACED ELBOW.SDR GAIA99136Overheat Light · illuminatedFLT 202 - TYS-DFW - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED PROCEDURE IN AOM AND LIGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER DIFFICULTY. RAN NR 3 ENGINE AT 80 PERCENT EPR AND COULD NOT DUPLICATESDR GAIA99135Overheat Light · illuminatedFLT 202 - DFW-SEA - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. ACCOMPLISHED PROCEDURE AS PER AOM VOL 1 AND LIGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED NR 3 ENGINE AND STRUT FIRE LOOPS SDR 99UAL900423Bulb · failedEMERGENCY EXIT LIGHT SIGN AT DOOR 2L INOPERATIVE. RELAMPED EXIT LIGHT, OPERATIONALLY CHECKED OK.SDR GAIA99134Overheat Light · illuminatedFLT 302 - DFW-TYS - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED KHA PROCEDURE AND CONTINUED OPERATION ON NR 2 BLEED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED ALL BLEED AIR PLUMBING, FITTINGS, OSDR 99UAL900416Sequence Valve · leakingON GEAR EXTENSION AIRCRAFT LOST HYDRAULIC SYSTEM A. BOTH PUMPS RAN TO ZERO HYDRAULIC FLUID QUANTITY. *S/D* REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND REPLACED LT MLG LOCK OPERATED SEQUENCE VLV PER MAINTENANCE MANUAL. PERFORMED NORMAL RETRACTISDR 99UAL900414Coffemaker · smokingLOWER COFFEEMAKER IN AFT GALLEY SMOKING AND SPARKING. *S/D* REPLACED COFFEEMAKER. INSPECTED WIRING, LEFT UNIT ON FOR SEVERAL HOURS, NO DEFECTS NOTED.SDR GAIA99115Hat Section · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE HAT SECTION AT STATION 344 TO 360, RBL 19 IS CORRODED. HAT SECTION REMOVED PER ATS DRAWING 2000-0373. FABRICATED A NEW FLOOR PANEL IAW B727 SRM 53-20-2. THIS SDR GAIA99114Skin · misinstalledDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT AT STATION 610 AND STRINGER 3L, A FASTENER IS INSTALLED ON TOP OF A BUCKTAIL. REPAIRED IAW ATS DRAWING 2000-0193. THIS DRAWING WAS DER RECOMMENDED AND ACO APPROVEDSDR GAIA99113Floorbeam · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE FLOORBEAM AT STATION 620 IS CORRODED BETWEEN LBL 24.75 AND RBL 24.75 SEAT TRACKS. REPAIRED IAW ATS DRAWING 2000-0276. THIS DRAWING WAS DER RECOMMENDED AND ACO SDR GAIA99112Keel Beam · corrodedDURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE KEEL BEAM (STRINGER 27R) AT STATION 950E HAD EXFOLIATED CORROSION. THIS IN THE AREA OF THE NR 2 LOWER CARGO DOOR FRAME. REPAIRED IAW DRAWINGS 53-99296-1 AND 53SDR 99ZZZM741Smoke Detector · looseFLT 307 - JFK - NR 5 CARGO COMPARTMENT SMOKE DETECTOR FAILS TO TEST. FOUND SOCKET LOOSE ON TEST BULB, RE-SECURED SOCKET OPERATIONAL CHECKS NORMAL. (M)SDR 99UAL900424Bulkhead Chord · corrodedTHE FORWARD EDGE OF THE CHORD AT STATION 1183 BULKHEAD LBL 24, WL 209 WAS CORRODED BEYOND THE SRM ALLOWABLE LIMIT. DAMAGE WAS TRIMMED OUT AND AREA WAS REPAIRED WITH STRAP AND FILLER PER TIMCO INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110SDR 99UAL900405Battery · dischargedMID CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY.SDR 99UAL900408Rib · crackedDURING INSPECTION AND INSTALLATION OF THE PREVENTIVE MOD PER SERVICE BULLETIN727-57-0012 AS MANDATED BY AD94-07-08 AND AD90-06-09 ON THE LBL 70.5 RIB CHORD AT STATION 760.5 TWO CRACKED FASTENER HOLES WERE FOUND. FATIGUE. C0RRECTION, BOTH HOLES WERE OVERSIZESDR 99UAL900406Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THISDR 99UAL900404Spar Web · misdrilledDURING ACCOMPLISHMENT OF THE CENTER WING BOX REAR SPAR WEB MODIFICATION AS MANDATED BY AD97-25-15, EIGHTY THREE HOLES WERE MISDRILLED COMMON TO THE REAR SPAR CENTER WEB ACCESS PLATE AND THE REAR SPAR WEB. OVERSIZED FASTENERS OF THE SAME TYPE WERE INSTALLED. SDR 99UAL900393Fire Loop · defectiveNR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO STRUT OVERHEAT. RETURNED TO DEN. *S/D* DEFLECTIVE FIRE LOOP AT STUB WING CAUSED THE STRUT OVERHEAT LIGHT TO ILLUMINATE. AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF FIRE LOOP AND ENGINE RUN UP VERIFICATION.SDR 99UAL900394Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. SHUT OFF BLEED AND ANTI-ICE. LIGHT WILL NOT GO OUT. DIVERTED TO CLE. *S/D* TIGHTENED LOOSE CLAMP ON THE 13TH STAGE VALVE AND ONE CLAMP ON THE CHECK VALVE. RAN ALL THREE ENGINES TO TAKEOFF POWER WITH NO STRUT OVER
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