Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 DHL2001745012Light · not seatedEXIT LIGHT ABOVE COCKPIT CABIN DOOR STAYS ILLUMINATED. SEATED EXIT LIGHT ASSY.AS PER B727-200 MM CHAP 33-50-11.OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.SDR DHL2001745011Battery · dischargedEMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW B727 MM 33-50-22 OPS CHECK GOOD.SDR DHL2001745009Seat · lack of lubeCAPTAINS SEAT DOES NOT ADJUST UP OR DOWN. LUBRICATED ALL MOVING PARTS AS PER B727-200 MM 25-10-41 OPS CHECK GOOD NO DEFECTS NOTED.SDR DHL2001746001Tab · delaminatedLT O/B AILERON LWR SURFACE 2 AREAS DELAMINATED. AREA OF DELAMINATION LT O/B AILERON TRIM TAB & NOT THE AILERON ITSELF. REMOVED AND REPLACED LT O/B AILERON BAL TAB. OPS CHECKED SERVICEABLE.SDR DHL2001745008Skin · corrodedLT OUTBD MIDFLAP HAS NUMEROUS AREAS OF SURFACE CORROSION ON UPPER LT OUTBD MIDFLAP HAS 2 FASTENERS HEADS MISSING AFT OF UPPER SURFACE.SDR DHL2001745007Skin · corrodedNR 8 SPOILER UPPER SURFACE HAS AREA OF CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6.SDR DHL2001745006Bracket · crackedCOVE PANEL BRACKETS BELOW OUTBD END OF NR 13 SPOILER CRACKED LT WING LEADING EDGE VENT PANEL OUTER SKIN MISSING COVE PANEL BRACKETS BELOW OUTBD END NR 12 SPOILER BROKEN OUT. REMOVED & REPLACED 1 EA T/E COVE PNL SUPPORT CHANNEL PER B727 SRM 51-10-1 & 51-30-2. SDR SCNA01704Warning System · false activationFALSE WINDSHEAR WARNING AT 500 FT AGL, GO-AROUND WINDSHEAR AHEAD. NO FAULTS NOTED.SDR DHL2001747542Skin · corrodedDURING LINE INSPECTION FOUND CORROSION AT LEFT WING FWD LOWER SKIN AT APPROXIMATELY WS 190. REMOVED CORROSION PER B727 SRM 57-10-6 FROM LEFT WING AT APPROXIMATELY WS 190 MATERIAL LOSS .103 INCHES WITHIN LIMITS PER BOEING TELEX DHL-CVG-01-00004H. HFEC INSP ACCOSDR DHL2001747004Fire Loop · out of positionENG NR 3 FIRE PROTECTION SYS DETECTOR GROUND LIGHT ILLUMINATED IN FLIGHT. ENG NR 3 RE-POSITIONED FIRE LOOP IAW B-727 MM 26-11-000.SDR DHL2001747003Fire Loop · out of positionENGINE NR 3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT HAS PREVIOUS WRITE UP ON 06/28/01. MEL 26-9-1 DMI 6209 ENG NR 3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT HAS PREVIOUSLY WRITE-UP OSDR DHL2001747001Switch · failedNR 2 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION. COMPLETED ABNORMAL PROCEDURES, PROBLEM STILL OCCURRED. RETURNED TO KTUS. REMOVED AND REPLACED SLAT SWITCH. OPS CHECK GOOD IAW 727 MM 27-81-00.SDR DHL2001747Switch · failedNR 2 SLAT WOULD NOT RETRACT DURING FLAP RETRACTION. COMPLETED ABNORMAL PROCEDURES, PROBLEM STILL OCCURRED. RETURNED TO KTUS. REMOVED AND REPLACED SLAT SWITCH. OPS CHECK GOOD IAW 727 MM 27-81-00.SDR DHL2001747002Fire Loop · out of positionFIRE PROTECTION SYSTEM DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ENG NR 3. REPOSITIONED FIRE LOOP REF B727 MM 26-11-12.SDR 2001F00095Relief Valve · failedFLT 523 - MIA-CCS - DURING CLIMB-OUT, CREW UNABLE TO CONTROL CABIN PRESSURE. OUTFLOW VALVE CLOSED DURING ENTIRE TIME. AIRCRAFT RETURNED TO MIAMI WITH NO EMERGENCY LANDING DECLARED. SWAPPED AIRCRAFT, FLIGHT DEPARTED TO ORIGINAL DESTINATION 3:45 MIN DELAY. TSDR SCNA01042Battery · dischargedDURING A MAINTENANCE LINE CHECK THE AFT ENTRY EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED TWO BATTERIES.SDR GAIA01240OPSwitch · dirtyFLT 2011 - PDX-MHR - DURING APPROACH, THE GEAR WAS SELECTED TO THE DOWN POSITION. ALL THREE GREEN LIGHTS ILLUMINATED AND THE NOSE GEAR LIGHT WENT OUT AND DID NOT COME BACK ON. THE FLIGHT CREW DECLARED EMERGENCY, VERIFIED NOSE GEAR POSITION THROUGH THE VIEWINSDR DHL2001745005Autopilot Sys · malfunctionedAUTOPILOT WILL NOT MAINTAIN LOCALIZER ON APPROACH BELOW 2000 FT ABOVE AIRPORT. PERFORMED OPS CHECK OF A/P NAV/LOC. CHECKS GOOD WITH COMPANY EQUIPMENT.SDR GAIA01238STLight · not seatedMAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LIGHT ASSEMBLY NOT SEATED IN CONNECTOR. REINSTALLED AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR DHL2001747536Slat · crackedD-CHECK, RT WING NR 5 SLAT L/E, INBOARD TRACK SEAL CUT OUT CRACKED. SEEN FROM TOP OF L/E. REMOVED RT WING NR 5 LEADING EDGE SLAT TO FOM PED 27-81-11. NDT REG FOR CRACK DIMENSION. CRACK DIMENSION CHECKED IAW NTM 727 51-06-00, PART 1 FROM THE EDGE 0.616" LENSDR GAIA01156OPHydraulic Line · leakingFLT 1850 - PDX-SEA - UPON LANDING GEAR EXTENSION, LOST A SYSTEM HYDRAULICS QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN SEA. INSPECTION OF AIRCRAFT FOUND LEAKING LEFT GEAR DOOR ACTUATOR RETURN HOSE. REMOVED AND LEFT ACTUATOR RETURN HOSE. REMSDR DHL2001745004Computer · malfunctionedAUTOPILOT ENGAGED/DISENGAGED PADDLE LEVERS WILL NOT MOVE TO THE ENGAGED POSITION IN BOTH A AND B MODE. A & B MODE DEACTIVATED ON AIRCRAFT. PLACARD MUST HAVE BEEN MISSED BY CREW. SYSTEM OPERATES NORMAL PER BMM REF 22-11-1. STATUS-CLOSED.SDR DHL2001745003Control Unit · malfunctionedWITH ANTI-SKID ON, AND BRAKE PEDALS AT MECHANICAL STOPS, ANTI-SKID WOULD NOT ENGAGE OR CYCLE. R & R ANTI-SKID CONTROL BOX WITH SERVICABLE UNIT IAW MM 32-42-0. STATUS-CLOSED. P/N OFF 42-527D, S/N OFF 1802, P/N ON 42-527D, S/N ON 1647. PCT 100434, POS ONLY.SDR DHL2001745002Fire Detector · false indicationLOWER CARGO FIRE WARNING SOUNDED DURING CRUISE, DURING DESCENT, WARNING EXTINGUISHED, THEN CAME ON AGAIN DOWNWIND THEN OFF AGAIN ON LANDING. CORRECTIVE ACTION: TESTED LOWER FIRE WARNING ON GRND IAW 727MM 26-16-00. OPS TEST CHECKS SERVICEABLE, NO DEFECTS NSDR DHL2001745001Windshield · crackedL-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERVICABLE PRESSURIZED A/C ON GROUND. NO LEAKS NOTED. STATUS CLOSED.SDR DHL2001747525Seat Track · corrodedD-CHECK, SEAT TRACK SECTION STA 850.95-760.95 RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION ON SEAT TRACK SURFACE FROM STA 850.95-760.95 RBL 45.5 IAW B727 SRM 51-10-1 PG 12-13.SDR DHL2001747533Angle · corrodedD-CHECK, ANGLE CORRODED AFT OF STA 1166 BY LAV SERVICE DOOR AFT PIT. REMOVED AFT LAV SERVICE DOOR AND PAN IAW SRM 51-30-2, REMOVED CORROSION PER SRM 51-10-6 ON L-ANGLE AND WEB.SDR DHL2001747529Frame · crackedD-CHECK, BODY FRAME STA 930 STRINGER 14 UPPER FRAME LOWER SECTION CRACKED JUST BELOW RIVET. VERIFIED CRACK 0.75 INCH IN LENGTH. RUNNING INBD FROM EDGE OF FRAME. ALSO FOUND CRACK APPROX 1.5 INCH ABOVE AND OUTBD OF ORIGINAL CRACK RUNNING INBD AND OUTBD OF FASSDR DHL2001747528Seat Track · corrodedD-CHECK, SEAT TRACK SECTION STA 851.95 TO 870 RBL 45.5 HAS CORROSION ON INBOARD SECTION OF FLANGE AROUND FASTENER HEADS.SDR DHL2001747537Floor Support · corrodedD-CHECK, CORROSION UNDER NUT PLATES ON 4 FLOOR SUPPORTS FS 950A. REMOVED CORROSION FROM 4 AREAS ON FLOOR SUPPORTS IAW 727 SRM 51-10-6 PG 6, 4 (RBL 5, RBL 10, LBL 5, LBL 10). RBL 5, RBL 10, AND LBL 5.SDR GAIA01106OPLight · looseFLT 2031 - RNO-IND - DURING CRUISE, THE EMERGENCY EXIT LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULITIES. FOUND THE EMERGENCY EXIT LIGHT TO BE LOOSE IN ITS FIXTURE. RESECURED AS REQUIRED. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS SDR DHL2001747535Keelbeam · gougedD-CHECK, KEEL BEAM LOWER CHORD INSIDE RT MLG W/W, GOUGED AND CHAFED BY MLG DOOR HINGE AT AFT HINGE AND FWD HINGE.SDR DHL2001747526Seat Track · corrodedD-CHECK, SEAT TRACK SECTION STA 950A-870 RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION AT SEAT TRACK RBL 45.5 STA 870-950A.SDR DHL2001747524Seat Track · corrodedD-CHECK, SEAT TRACK STA 720D-700 RBL 45.5 HAS CORROSION.SDR DHL2001747538Support · corrodedD-CHECK, RT WING L/E LOWER INBOARD FAIRING SUPPORT HAS LIGHT CORROSION IN END OF SUPPORT. REMOVED PART IAW SRM 51-30-2.SDR DHL2001747530Angle · corrodedD-CHECK, C1 DOOR LOWER EDGE RIBS CORRODED AND DENTED. CORROSION PROGRESSES BENEATH LEVELING COMPOUND. REMOVED LEVELING COMPOUND AND 4 LOWER DOOR ANGLES IAW 727 SRM 51-30-2. ANGLE LOWER BEAM CORRODED.SDR DHL2001747531Skin · corrodedD-CHECK, FWD PIT CORROSION ON FUSELAGE SKIN S26L FS 720-FS 720A (BELOW TRANSITION PANEL). REMOVED CORROSION PER 51-10-6. MARKED AREA AND CUT OUT DAMAGED PORTION OF UPPER AND LOWER SKIN PER 727 SRM 53-30-3 FIG 5.SDR GAIA01073BOPLine · rupturedFLT 1805 - FWA-LAX - AT FL310, HYDRAULIC SYSTEM ''A'' PRESSURE AND QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN DEN. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC LINE IN RIGHT SIDE OF AFT AIRSTAIR. REMOVED AND REPLACED THE HYDRAULIC LINE PER BSDR DHL2001747534Stiffener · corrodedD-CHECK, RT WING FWD SPAR STIFFENER HAS LIGHT CORROSION UNDERNEATH PRIMER, JUST OUTBOARD OF NR 5 FLAP ACTUATOR.SDR DHL2001747532Stiffener · corrodedC-CHECK, RT WING FWD UPPER AND LOWER SPAR STIFFENERS, RT & LT OF NR 5 L/E FLAP ACTUATOR HAVE MED CORROSION.SDR DHL2001747527Seat Track · corrodedD-CHECK, SEAT TRACK SECTION STA 990-950A RBL 45.5 HAS SURFACE CORROSION. REMOVED CORROSION ON SEAT TRACK RBL 45.5 STA 950A-990.SDR GAIA01045BOPShutoff Valve · shortedFLT 2724 - ROC-BOS - NR 2 ENGINE FAILED ON CLIMB-OUT. ATTEMPTED RESTART FAILED. DID HAVE OIL PRESSURE AND ROTATION. AIRCAFT MADE AN UNEVENTFUL RETURN TO ROC. FOUND NR 2 FUEL SHUTOFF VALVE WIRES SHORTED IN AIRCONDITIONING BAY, CAUSING NR 2 FUEL SHUTOFF VALVESDR 20010320SG001Indicator · malfunctionedABORTED TAKEOFF DUE TO A LOW EPR INDICATION AT REDUCED POWER ON ENGINE NR 2. INSPECTED AND CREW RAN ENGINE UP TO MAX POWER. NR 2 ENGINE OPS PROPERLY ON GROUND ENGINE RUN AND ALL ENGINE INDICATIONS READ NORMAL AS PER TRIM CHART 71-00-87. AIRCRAFT RETURNED TOSDR GAIA01042Light · inoperativeFLT 739 - OSC - AFTER COMPLETION OF C-CHECK MAINTENANCE, EMERGENCY EXIT LIGHTS UNABLE TO SWITCH OFF. RE-SEATED COCKPIT ENTRY ''EMERGENCY EXIT'' LIGHT. OPS CHECK GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M)SDR GAIA01036Door Frame · crackedTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. THRESHOLD FRAME BOTTOM FLANGE AT THE C-1 DOOR, BS 593, RBL 20, FORWARD PIT. FABRICATED REPAIR DOUBLER AND REPAIRED THRESHOLD. INSTALLED REPAIR IAW B727 SRM 53-10-1, SRM 51SDR GAIA01035Floorbeam · crackedTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER SURFACE OF UPPER CHORD AT BS 420, RBL 45 IS CORRODED. REPAIRED FLOORBEAM AT BS 420 RBL 45 IAW B727 SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR ANGLES IAW B7SDR GAIA01034Keelbeam · crackedTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. KEELBEAM LOWER CHORD AT BS 873, CRACKED THROUGH FASTENER. REMOVED FASTENERS AND DAMAGE, FABRICATED REPAIR DOUBLER IAW B727 SRM B727 51-30-2, 51-10-2, MM 51-20-151 AND SB 72SDR GAIA01033Shear Tie · corrodedTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. CORROSION FOUND ON BELLY FRAME TO SKIN ATTACH ANGLE AT BS 600, LBL 3 TO RBL 3. REMOVED DAMAGES SECTION IAW B727 SRM 53-10-4. FABRICATED SHEAR TIE ANGLE IAW B727 SRM 53-10-SDR GAIA01032Floorbeam · misdrilledTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE FACILITY. FLOORBEAM UPPER CAP AT BS 360, RBL 63 HAS DOUBLER DRILLED HOLES. REMOVED DAMAGES SECTION OF FLOORBEAM. FABRICATED REPAIR ANGLE IAW B727 SRM 53-10-8. INSTALLED REPAIR IAW SDR GAIA01031Frame · dentedTHIS ITEM WAS FOUND DURING ROUTINE MAINTENANCE AT THE TIMCO OSC MAINTENANCE ACILITY. CABIN FRAME DENTED AT BS 600, STRINGER 9R. FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-2, FIG 4. INSTALLED FRAME REPAIR DOUBLER AT BS 600 STRINGER 9R IAW B727 SRM 53-10-4.
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