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 DL72K991158Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 640 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONLY 2 CRACKS BETWEEN FS 580 AND 600. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP ANDSDR DL72S991185Frame · wornFOUND DURING MV2 CORROSION VISIT NR 266, T-ANGLE WORN THROUGH THREE PLACES FROM .75 TO 4.25 INCHES LONG AT FWD FLANGE OF T-ANGLE, NR 2 ENG CUTOUT 4 O'CLOCK POS TO 6 O'CLOCK POS STA 1453. NRC 267 NR 2 ENG CUTOUT FWD COWL STRIKER T-ANGLE WORN THROUGH/THIN 3 O'SDR DL72S991159Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION REVEALED 2 CRACKS BETWEEN FS 1030 AND 1050, AND 3 CRACKS BETWEEN FS 1050 AND 1070. THE SKIN LAP WAS CUT OUT BETWEEN FS 1SDR DL72S991132Actuator · failedON APP FLAP EXT 2 TO 5 AMBER L/E FLAP LIGHT REMAINED ILLUM. POSITION TEST SHOWED NO LIGHT FOR LEFT NR 4 SLAT RETRACTED. PERFORMED APP PER POM. C/W PROCS FOR LANDING. TAXIING AFTER LAND UPON FLAP RETRACTION, LOST A HYD SYS FLUID. PERFORMED PROCS AS PER POMSDR DL72S991128Control Cable · failedAFTER TAKEOFF, PILOT HEARD LOUD NOISE FROM NOSE WHEEL AREA AND NOTICED NLG LIGHT INDICATION. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. FOUND LOWER NLG DOOR CABLE WITH SEVERAL STRANDS BROKEN AND BIRD CAGED, NLG DOORS WERE NOT FULLY CLOSED. REPLACED CABLSDR DL72S991125Battery Pack · dischargedFIRST CLASS EMERGENCY LIGHTS DIM.SDR DL72S991124Web · crackedTPA LTR CHK B-2, LT VERT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0 PG 828, LT VERT TORQUE BOX WEB LWR LIGHTENING HOLE .375 INCH CRACK AT UPPER END AND A .625 INCH CRACK ON LWR END STA 1226. REPAIRED PER MM SDR DL72S991122Frame · crackedFOUND AT B-2 LETTER CHECK, LT AFT ENTRYWAY DOOR FRAME HAS .375 INCH VISIBLE CRACK. REPAIRED PER SRM 53-10-9.SDR DL72L991116Switch · out of adjustUNSAFE (AMBER LIGHT) INDICATION EXT AT FLAPS 5 POSITION. AFTER EXAMINATION IT WAS DETERMINED THAT L/E FLAP NR 1 FAILED TO EXTEND PROPERLY. AFTER TOUCHDOWN, L/E FLAPS LIGHT TURNED GREEN AND POS IND APPEARED NORMAL. ADJUSTED NR 1 L/E FLAP SWITCH PER MM, CHECKSDR DL72K991111Light · inoperativeL2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.SDR DL72L991253Wire · damagedON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION IN ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL24SDR DL72S991096Skin · crackedINTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 360 AND 380. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUSDR DL72S991095Skin · crackedINTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBSDR DL72S991083Battery · dischargedAFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP.SDR DL72L991073Return Line · crackedSYS A HYD QTY IND DROPPED TO ZERO QTY APPROX ONE HR AND 20 MINS INTO FLT. NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. CHECKLIST PROCEDURE INITIATED LANDING UNEVENTFUL. GROUND INVESTIGATION LEAKING HALF WAY POINT LEFT WING. FOUND NR 2 SPOIL-ER RETURN LINE CRSDR DL72K991059Angle · crackedFOUND ON C1 LETTER CK, LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 5 SLAT I/B STOP. REPAIRED PER MM 57-54-0.SDR DL72S991053Rib · crackedLT ELEV HINGE SUPPORT RIB CRACKED BETWEEN NR 3 AND 4 BAL BOARDS AT LOWER END. REPAIRED PER MM 55-10-31.SDR DL72S991043Throttle Rod · looseAT 10,000 FEET ON DESCENT, THE NR 3 ENGINE WENT TO 95 PERCENT N1 AND EGT TO 610 ENGINE SHUTDOWN WITH THE PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST. FOUND THROTTLE ROD OFF OF THRU SHAFT AT GEARBOX. REINSTALLED SAME ENGINE CHECKS NORMAL ON RUN UP ALL PARAMETERS SDR DL72S991039Switch · dirtyTAKEOFF WARNING HORN SOUNDED DURING POWER UP AND TAKEOFF WAS ABORTED AT 10 KTS. WARNING HORN ITEMS CYCLED AND SOUNDED AGAIN ON SECOND ATTEMPT. FOUND UPPER STAB TRIM SWITCH STICKING. CLEANED AND LUBED SWITCH. TAKEOFF WARNING TEST NORMAL.SDR DL72S991026Connector · looseAFTER TAKEOFF, NR 2 OIL TEMP GAUGE FLUCTUATED FOR 10 SEC AND THEN PEGGED OUT HIGH. RAN CHECKLIST AND SHUT DOWN ENGINE. REPLACED CANNON PLUG AT TEMP BULB.SDR DL72S991025Skin · crackedINTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS. ONE CRACK WAS NOTED BETWEEN FS 700 AND 720 AND 3 CRACKS WERE NOTED BETWEEN FS 720A AND 720B. THE CRACKS WERE ROUTED OUT OF THE SKSDR DL72S991024Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL. THE SKIN LAP WAS COMPLETELY CUTOUT AND REPAIRED WITH AN EXTESDR DL72S991175Web · crackedFOUND DURING MV2 CORROSION VISIT NRC 208, 2 CRACKS AT RT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. REPAIRED PER SRM 53-10-4 FIG 17.SDR DL72S991174Web · crackedFOUND DURING MV2 MID VISIT NRC 209, 2 CRACKS AT LT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. REPAIRED PER SRM 53-10-4 FIG 17.SDR DL72S991123Stringer · crackedFOUND DURING MV2 CORROSION VISIT NRC 210, STR 9 CRACKED AT FIN STA 157.2 INSIDE VERT STAB CRAWLWAY (3RD STR FROM BOTTOM, 3RD BAY UP FROM DOOR). REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72S991023Skin · crackedINTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL AT THE STRINGER 4L SKIN LAP SPLICE REVEALED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PSDR DL72S991008Web · crackedLEFT I/B TORQUE BOX VERT WEB CRACKED .5 INCH AT UPPER FASTENER STA 1214. REPAIRED PER MM 53-11-0 FIG 819.SDR DL72S990997Web · crackedTHE FS 1263 WEB OF THE RT LOWER VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER B727 S/B 53-0129 AND ER/A 367330-14AD.SDR DL72S990988Megaphone · inoperativeAFT CABIN MEGAPHONE INOP ON PREFLIGHT. REPLACED AFT CABIN MEGAPHONE.SDR DL72S990985Frame · crackedA .75 INCH VISIBLE CRACK AT L-2 DOOR FWD FRAME AT UPPER LOCK ROLLER. REPAIRED PER M/M 52-12-0.SDR DL72K991000Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACKS IN CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRESDR DL72K990999Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER PANEL. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WSDR DL72S990980Rib · crackedONE INCH CRACK NR 2 SLAT L/E NOSE RIB I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0 PG 805.SDR DL72L990970Start Valve · failedNR 1 START VALVE LIGHT ILLUMINATED IN FLIGHT. ENG SHUT DOWN PER PILOTS CK LIST. REPLACED START VALVE.SDR DL72S990973Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED MULTIPLE CRACKS IN MULTIPLE FRAME BAYS ALONG THE PANEL LENGTH. THE SKIN LAPS SPLICE WASSDR DL72S990972Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN ESDR DL72S990971Skin · crackedINTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 TO 480 REVEALED MULTIPLE CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. THE ENTIRE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLSDR CALA9900463Power Supply · inoperableIAH - TWO OVERWING EMERGENCY LIGHTS AND ONE EMERGENCY LIGHT AFT OF FLAPS LEFT SIDE OF FUSELAGE INOPERABLE. FOUND M654, M954, AND M955 POWER SUPPLIES BAD. REPLACED POWER SUPPLIES AND LIGHT ASSEMBLIES L878, L877, AND L822. EMERGENCY LIGHTS OPS CHECK NORMAL. SDR DL72K990966Angle · corrodedWHILE PERFORMING HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLES CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLES WITH ANGLES OF NEW MFG.SDR DL72S990933Power Supply · malfunctionedWHEN TAKEOFF POWER WAS APPLIED FUEL FLOW INDICATORS, INCREASED IN UNISION AND THEN FLUCTUATED IN UNISION BETWEEN BETWEEN 1000-5000 PPH. WITH T/O EPR ESTABLISHED ALL 3 FUEL FLOW GAUGES INDICATED 1000 PPH STEADY. ALL OTHER ENGINE INDICATIONS NORMAL. TAKEOFF ASDR DL72S990927Bracket · crackedNR 8 SLAT ACTUATOR I/B ATTACH BRACKET IS CRACKED. REPAIRED PER M/M 57-20-21 PG 812.SDR DL72S990926Controller · failedNOTIFIED OF SMELL IN THE CABIN, PERFORMED EMERGENCY DESCENT. AFTER LANDING, FOUND L-1 AC CONTROL CIRCUIT BREAKER POPPED IN WINDOW HEAT SECTION. ALSO, FOUND WINDOW HEAT NR 1L CIRCUIT BREAKER POPPED ON LOWER P-6 PANEL. AIRCRAFT DIVERTED TO YKM. MAINTENANCE FSDR DL72L990921Skin · crackedFUSELAGE SKIN FS 481-681, STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 52 CRACKS ALONG THSDR DL72L990917Skin · crackedFUSELAGE SKIN FS 360-481 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED 6 CRACKS IN THREE CONSECUTIVE FRAME BAYS. THE SKIN LSDR DL72L990916Skin · crackedFUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN TSDR DL72L990915Skin · crackedFUSELAGE SKIN FS 680-740 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THESDR DL72S990912Web · crackedFOUND ON C2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED .375 INCH AT STA 1289. REPAIRED PER MM 53-11-0.SDR DL72S990911Frame · crackedFOUND AT C-2 LETTER CK, LEFT AFT ENTRY WAY DOOR FRAME HAS .375 IN VISIBLE CRACK AT UPPER CUTOUT. REPAIRED PER SRM 53-10-9.SDR DL72S990904Spar Web · crackedWING CENTER SECTION, REAR SPAR WEB, RBL 13. CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK AT RBL 13, JUST BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE SPAR WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PERSDR DL72S990903Skin · crackedFUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN TWO ADJ
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