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 DHL2003742518Stringer · crackedDURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 59874 CABIN STR 15L CRACKS STA 724D. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA AS REQUIRED FOR REPAIR IAW B-727 SRM 53-10-3 FIG 5. FABRICATED FUSELAGE STRINGER REPAIR 1 CHANNEL MAT USSDR DHL2003742514Frame · crackedDURING C-CHECK, RT WING L/E 130 INT FRAME IS CRACKED ON LOWER SKIN ATTACH ANGLE. STOP DRILL IAW B-727 SRM 51-10-1. REMOVED FASTENERS ON RT WING BL 92 INT FRAME VERT STIFFENER IAW B-727 SRM 51-30-2. FABRICATED DOUBLER FROM 7075 T6 .040 PO 900226 DIM 4.625 ISDR CA031030001Outflow Valve · failed(CAN) A/C EXPERIENCED LOSS OF PRESSURIZATION ON CLIMB OUT. CREW DISCOVERED RT PACK INOPERATIVE. A/C LANDED AT COMPANY MAINTENANCE FACILITY WHERE THE RT FWD PACK VALVE WAS REPLACED AND A/C RETURNED TO SERVICE.SDR GAIA03110OPAccessory Unit · looseON APPROACH TO PHX, THE RIGHT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE ON GEAR EXTENTION. THE SECONDARY MLG LIGHTS INDICATED DOWN AND LOCKED. THE CREW PERFORMED A MANUAL GEAR EXTENTION WITH NO CHANGE IN GEAR INDICATION. AN UNEVENTFUL LANDING WAS MADE. SDR DHL2003743015Battery · inoperativeEMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE ON PREFLIGHT. REMOVED AND REPLACED LIGHT BATTERIES, OPS GOOD IAW M/M 33-50-01. 37007-001 BATS.SDR DHL2003748010Roller · out of adjustFORWARD ENTRY DOOR DOES NOT SHUT VERY EASY, OUT OF ADJUSTMENT. LUBRICATED FORWARD ENTRY DOOR ROLLERS, HINGES AND LINKAGE IAW M/M 12-25-11. OPS CHECKED GOOD IAW DHL B-727 M/M 52-11-01.SDR DHL2003742014Window · failedL5 WINDOW SHATTERED DURING FLIGHT. OUTER AND INNER PANE. ABNORMAL PROCEDURE PERFORMED. RII REMOVED AND REPLACED L5 WINDOW IAW B727 M/M 56-11-41.SDR 2004F00071Skin · dentedDURING SERVICE CHECK, FOUND DENT ON LEADING EDGE OF SKIN OF LEFT WING AT STATION 180 ABOVE NR 3 KRUGER FLAP. CUT OUT DENTED SECTION OF WING, FIXED LEADING EDGE SKIN AND INNER SKIN AT STATION 180. FABRICATED A FLUSH REPAIR FILLER AND DOUBLER. FABRICATED SKINSDR DHL2003743014Battery · dischargedEMERGENCY EXIT LIGHTS FAILED TO OPERATE DURING STANDBY POWER CHECK AND DURING NORMAL OPERATIONS. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECKED GOOD IAW B727 M/M 33-50-71. P/N OFF AND ON: MISC-062.SDR GAIA03108OPBrake Assy · draggingFLT 372 - LAX-PHX-FWA, DURING TAXI TO DEPARTURE, THE FLIGHT CREW NOTICED THE NR 3 BRAKE DRAGGING. REMOVED AND REPLACED THE NR 3 BRAKE AND THE NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR RYN2004F00012Hinge · crackedAT (B) CHECK FOUND. MAIN CARGO DOOR AFT HINGE WITH 2 CRACKED LOBES ON THE AFT PART OF THE AIRFRAME HINGE. DRILLED, TREATED, PRIMED AND INSTALLED NEW HINGE SECTION ON MAIN CARGO DOOR.SDR C1HA200375001Flap · delaminatedLEFT OUTBOARD FORE FLAP DELAMINATED ON OUTBOARD END, UNDER SIDE.SDR DHL2003748501Seat Track · corrodedDURING C CHECK AT MFG, N/R 691F1-1601-005 MAIN PASSENGER CABIN SEAT TRACK L/H O/B STA. 688 STA. 738 CORROSION FOUND AT ATTACHING SCREWS, HOLES CRACKED OUT, TOOL MARKING IN CENTER OF TRACK. REMOVED FAB. AND INSTALLED NEW SEAT TRACK P/N 60-6549 7178 T 6511 P.OSDR DHL2003742013Fastener · looseNR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED (P6-3 PANEL). INSPECTED FIRE LOOP ON NR 3 ENGINE. FOUND LOOSE FASTENER AND SECURED IAW B-M/M 20-80-1. NO DEFECTS NOTED.SDR DHL2003748502Flap Track · corrodedDURING C-CHECK AT PEMCO IN DOTHAN, ALABAMA N/R 691F1-1442-005, RT WING LOWER TRAILING EDGE AT O/B FLAP TRACK FWD END-CORROSION ON SKIN I/B OF TRACK. REMOVED RT O/B FLAP O/B TRACK FAIRING, REPAIRED AREA PER EA PD 27-57-01. RE-INSTALLED O/B FLAP O/B TRACK FAIRSDR DHL2003748500Web · crackedDURING C-CHECK AT PEMCO, AFT CARGO DOOR LOWER LOBE BULKHEAD STA 1183, APPROX BL 44, UPPER FLOOR WEB CRACKED IN 2 EACH PLACES. STOPPED DRILLED CRACK IAW B-727 SRM 51-10-01. REMOVED ACCESS COVER ON TOP OF FLOOR, FOUND CORROSION UNDER COVER, MATERIAL OUT OF LIMSDR DHL2003742012Fire Detector · will not testNR 4 FIRE DETECTOR WON'T TEST. REMOVED AND REPLACED SMOKE DETECTOR IAW 26-17-0. OPS CHECKED GOOD.SDR DHL2003743013Detector · malfunctionedNR 3 DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. INSPECTED NR 3 ENGINE DETECTOR CIRCUIT GROUND - NO FAULTS FOUND AND NO LIGHTS ILLUMINATED. OPS CHECKED GOOD IAW M/M 26-11-0. TRANSFERRED NR 3 GROUND DETECTOR FAULT TO DMI NR 13SDR DHL2003743012Detector · malfunctionedNR 3 ENGINE DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. DEFERRED IAW MEL 26-9. DMI NR 13565 PLACARD INSTALLED. NR 3 ENGINE DETECTOR CIRCUIT GROUND FAULT LIGHT IS ILLUMINATED ON CIRCUIT BREAKER PANEL. DMI NR 13565 REF. ISOLSDR CA030718001Igniter · faulty(CAN) DURING START OF NR 3 ENGINE, IT WAS OBSERVED THERE WAS NO EGT. START WAS ABORTED & OBSERVED ALL PARAMETERS. MAINT INSPECTED AREA & REQUESTED ANOTHER START. NR 3 ENGINE STARTED & OBSERVED RAPID EGT RISE & ENG START ABORTED. MAINT INFORMED FLT DECK THAT SDR DHL2003743011Detector · intermittentNR 3 ENGINE DETECTOR CIRCUIT GROUND LIGHT CAME ON. INSPECTED NR 3 ENGINE DETECTOR AND FOUND NO DEFECTS IAW M/M 26-11-00.SDR DHL2003748009Power Supply · malfunctionedAPU FIRE DETECTION TEST WILL NOT TEST. "DEFERRED APU PER MEL 49-1; CAT. "C"; ASSIGNED DMI 13486; PLACARD INSTALLED. TROUBLESHOOTING SYSTEM, CHECKED TEST SWITCH FOR CONTINUITY BETWEEN PINS 2 & 3; CHECKED GOOD. VERIFIED THAT SENSOR/ RESPONDER IS HEATING UP WISDR DHL2003755010Brake · seizedDURING TAXI, BRAKES SEEMED TO LOCK AND NOT RELEASE. SUSPECT LEFT BRAKE. REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY AND MAIN WHEEL ASSEMBLY DUE TO BRAKE SEIZURE DAMAGE IAW 727 M/M 32-45-1 & 32-41-32. OPS CHECKED SERVICEABLE.SDR DHL2003742011Indicator · malfunctionedUPON GEAR EXTENSION HAD 3 GREEN, 3 RED LIGHTS, AND DOOR LIGHTS. S/O PANEL HAD MAIN GEAR GREEN, AND TAIL SKID LIGHT ON. BELOW 500 FT GPWS ANNOUNCED TOO LOW GEAR, AFTER GO AROUND CYCLED GEAR, ALL INDICATIONS NORMAL AND LANDED. UPON TAXI IN LEFT GREEN GEAR LIGSDR 2003F00473Fitting · corrodedAT CORROSION REPAIR INPUT, FOUND FRAME FITTING, ANGLE, CORRODED AT BS 740, RBL 16. REMOVED CORRODED FITTING. REPAIRED, DRILLED AND INSTALLED 740 RIGHT BULKHEAD FITTING IAW B727 DWG 65-15940 AND SRM 51-30-2. (M)SDR DHL2003742010Light · inoperativeMAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND OPS CHECKED OK IAW B727 M/M 33-50-71.SDR 2003F00542Hydraulic Line · damagedON TAKEOFF, OUT OF SDF AT GEAR ROTATION LOST SYS 'A' HYD FLUID, SHUT PUMPS OFF ACCOMPLISHED ABNORMAL CHECKLIST. REMOVED AND REPLACED HOSE ASSEMBLY NR 2 ENGINE P/N 10-60563-40, NO METAL FOUND IN CASE DRAIN FILTERS OR SUPPLY FILTERS REPLACED NR 1 AND NR 2 HYDRASDR CA030627001Control Cable · chafed(CAN) DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS OBSERVED THAT THE RT INBOARD AILERON CABLE ASSY WAS CHAFED AND WORN AT THE CABLE GUIDE. THE CABLE WAS REMOVED & NEW CABLE INSTALLED IAW MM 27-10-71. ADJUSTMENT AND FUNCTIONAL CHECK CARRIED OUT SERVICEABLE ISDR DHL2003755009Moisture Trap · contaminatedDURING T/O AND CLIMB NR 1 EPR AND FUEL FLOW CONTINUALLY FLUCTUATES .04 AND 400 LBS RESPECTIVELY. PERFORMED ABNORMAL PROCEDURES. FLUCTUATIONS STOPPED PRIOR TO PRECAUTIONARY ENGINE SHUT DOWN. FOUND MOISTURE IN THE NR 1 ENGINE FUEL CONTROL MOISTURE TRAP. DRAISDR DHL2003748006Seat · damagedF/O'S SEAT FORWARD - AFT ADJUSTMENT LEVER DOES NOT FULLY DISENGAGE LOCKING PIN WHEN ADJUSTING POSITION. LUBED AND OPERATED SEVERAL TIMES, OPS CHECKED NORMAL IAW M/M 25-10-41.SDR DHL2003742009Latch · brokenCOCKPIT DOOR WON'T OPEN. TRANSFERRED TO DMI 13250 PER MEL 52-14 CAT C PLACARD INSTALLED. REF DMI 13250 COCKPIT DOOR KNOB BROKEN OFF. REMOVED AND REPLACED COCKPIT DOOR IAW M/M 52-00. THIS CLEARS DMI 13250.SDR 2003F00383Clamp · looseON CLIMB-OUT FROM MIA, PASSING THROUGH F/ 29 LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED AOM AND ISOLATION PROCEDURES. RETURNED TO MIA FOR MAINTENANCE ACTION. T/S PER MM 26-14-0. FOUND LOOSE CLAMP IN AFT CARGO COMPARTMENT SIDEWALL FORWARD CORNER. SECUSDR DHL2003755008Switch · lack of lubeFORWARD ENTRY DOOR LIGHT NOT ILLUMINATED WITH FORWARD ENTRY DOOR OPEN. LUBED SWITCH IN DOOR JAMB. OPS GOOD IAW M/M 52-11-01.SDR DHL2003748008Angle · crackedDURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130 FOUND THE OUTBOARD NR 8 SLAT ACTUATOR MOUNT ANGLE TO BE CRACKED. REMOVED NR 8 SLAT ACTUATOR CRACKED O/B MOUNT ANGLE IAW B-727 SRM 51-30-2. FABRICATED NEW ANGLE FROSDR DHL2003748007Bracket · crackedDURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130, FOUND BOTH NR 1 SLAT ACTUATOR MOUNT ANGLES TO BE CRACKED. REMOVED NR 1 SLAT ACTUATOR ANGLES IAW B-727 51-30-2. FAB NEW ANGLES FROM 7075 T-6 .063 INCH PO 9912495 1SDR DHL2003755007Skin · damagedFUSELAGE HAS HOLE IN LEFT SIDE, FORWARD OF AFT PRESSURE BULKHEAD, BY GROUND VEHICLE. ACCOMPLISHED REPAIR ON DAMAGED SKIN AS PER B727 SRM 53-30-3. PERFORMED PRESSURE CHECK, CHECKS OK. PATCH REPAIRED NEEDS TO BE PAINTED. TRANSFERRED TO DMI 12871E OK PER GMM SDR C8GA20030012Line · crackedTHE NR 1 OIL QUANTITY DROPPED TO A .25 GALLON ON DOWNWIND FOR RUNWAY 12R INTO KMSP. INFLIGHT SHUT DOWN OF THE NR 1 ENGINE AS PRECAUTIONARY IN ACCORDANCE WITH CCIA PROCEDURES, ADVISED ATC AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND AN OIL PRESSDR DHL2003748005Gasper Fan · inoperativeNOXIOUS BURNING ODOR COMING FROM GASPER OUTLETS. DEFERRED GASPER FAN PER MEL 21-24 DMI 12684 CAT-D. CIRCUIT BREAKER PULLED AND CONNECTOR REMOVED AT GASPER FAN. REF DMI 12684 - NOXIOUS BURNING ODOR FROM GASPER OUTLETS. REMOVED AND REPLACED GASPER FAN AS PERSDR DHL2003755006Structure · crackedRT WING L/E STA 464 APPROX HAS APPROX 5 INCH CRACK ABOVE NR 5 SLAT. CLEANED AREA OF PAINT AT STA 444 AND 454. PERFORMED DYE PENETRANT OF SUSPECTED AREAS AND CONFIRMED SKIN CRACKS AT STA 444 & 454. CUT OUT AREA SIZE 3 X 4 INCH ON STA 444 LT WING L/E AND CUT SDR DHL2003743009Smoke Detector · inoperativeTHE 6R SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED STATION 6R SMOKE DETECTOR IAW M/M 26-16-01. OPS CHECKED GOOD.SDR 2003F00253Duct · leakingON TAKEOFF FROM CAE, AFTER GEAR RETRACTION NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ABNORMAL CHECKLIST PROCEDURES AND ENGINE SHUTDOWN PROCEDURES. DECLARED AN EMERGENCY WITH ATC AND AIRCRAFT CLEARED TO SAV FOR LANDING. LANDED AT SAV WITHOUT INCSDR DHL2003743008Fire Detector · chafedNR 3 DETECTOR CIRCUIT GROUND LIGHT COMES ON INTERMITTENTLY. FOUND SENSING ELEMENT TO BE RUBBING ON COWLING, ADJUSTMENT SEEMS TO HAVE CORRECTED PROBLEM, OPS CHECKED GOOD PER BMM 26-11-12.SDR DHL2003743007Connector · looseNR 3 GROUND FAULT DETECTOR LIGHT ILLUMINATED IN FLIGHT. FOUND FORWARD ELECTRICAL CONNECTOR LOOSE ON NR 3 ENGINE FIRE SENSING ELEMENT, RE-SECURED CONNECTOR. SYSTEM OPS CHECKED GOOD IAW BMM 26-11-00.SDR DHL2003742008Smoke Detector · malfunctioned"CARGO SMOKE" WARNING LIGHT ILLUMINATED DURING CLIMBOUT. COMPLETED EMERGENCY CHECKLIST AND RETURNED TO MIA. REMOVED AND REPLACED NR 2 SMOKE DETECTOR PER B727 M/M 26 PAGE 23. OPS CHECKED NORMAL. NO DEFECTS NOTED.SDR DHL2003743006Bracket · brokenAFTER PRE-DEPARTURE CHECK FOUND NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. DEFERRED PER MEL 26-9 CAT-C DMI 12419. REF DMI 12419; NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. FOUND BROKEN BRACKET ON B-FLANGE, REPLACED, RE-SECURED FIRE LSDR DHL2003742007Bulb · burned outNR 2 SMOKE DETECTOR WILL NOT TEST. RELAMPED, OPS CHECKED OK IAW M/M 26-10-0.SDR 2003F00245O-Ring · wornDURING APPROACH TO AUSTIN AT 29,000 FEET, BOTH B-HYDRAULIC LOW PRESSURE LIGHTS CAME ON. B-SYSTEM PRESSURE INDICATED ZERO AND SYSTEM QUANTITY NORMAL. EMERGENCY PROCEDURES WERE FOLLOWED. AIRCRAFT LANDED AT AUSTIN WITHOUT INCIDENT. REPLACED O-RING AND TIGHTENSDR CA030327005Indicator · malfunctioned(CAN) DURING CLIMB, FLAPS WERE SELECTED TO THE 2 DEGREE POSITION. THE INBOARD FLAPS STAYED AT 5 DEGREE. AIRCRAFT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. FLAP SYSTEM INSPECTED, LUBRICATED ANDCYCLED WITH SYSTEM OPERATING NORMALLY I.A.W. MM 27-51-0. FLAPSDR C8GA2003008REngine · leakingON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY TO APPROXIMATELY ONE GALLON. AIR TURNBACK TO BOSTON AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND SERVICE NR 3 ENGINE OILS. RAN ENGINE ON GROUND AND NO OIL LOSS OR LEAKS WERE NOTED OSDR C8GA20030008Bearing · failedFLIGHT 723 FROM BOS TO ROC. ON CLIMB OUT, NR 3 ENGINE OIL QUANTITY DECREASED STEADILY TO APPROXIMATELY ONE GALLON. AIR TURNBACK TO BOSTON AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND SERVICE NR 3 ENGINE OILS. RAN ENGINE ON GROUND AND NO OIL
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