Boeing 727-247
Service difficulty reports · 2,669
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 = '727247' 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 = '727247' 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 DL72W991936Insulation · splitON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEWTYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-026SDR DL72W991802Cadc · failedAFTER T/O CAPTAINS MACH INDICATOR DISPLAYED AN OFF FLAG. ALSO, CAPTAINS ALTIMETER HAD A STANDBY FLAG ALSO NEITHER TRANSPONDER DISPLAYED MODE C TO ATL. REPLACED NR 1 CADC CHECKED NORMAL.SDR DL72W991810Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183, RBL 26.83, VERTICAL BEAM, CRACK REPAIR. THE RBL 26.83 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK. THE BEAM WAS REPAIRED PER BOEING S/B 727-53-0182, REV 1 AND DOCUMENTED PER ER/A 367994-14AD.SDR 99FDEA00301Actuator · failed99-186 - 'A' SYSTEM HYDRAULIC QUANTITY FELL TO ZERO. PRESSURE OK AT 3000 PSI. COMPLIED WITH LOSS OF 'A' SYSTEM RED TABLS. REMOVED AND REPLACED TWO WING PANELS AT LT NR 4 SLAT ACTUATOR. REMOVED AND REPLACED NR 4 LEADING EDGE SLAT ACTUATOR PER BOEING MM 27-8SDR 99FDEA00299Switch · inop99-184 - 1ST ATTEMPT TO LWR MLG RECEIVED LEFT AND NOSE UNSAFE IND, 2ND ATTEMPT ALL 3 MLG IND DOWN AND LOCKED. REMOVED AND REPLACED NOSE GEAR, LMG DOWN LOCK SENSOR,32-61-91, POSITION SWITCH PER MM 32-61-71.SDR DL72W991680Bracket · crackedFOUND ON F-1 LETTER CK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED OUTBOARD END. REPAIRED PER MM 57-20-0.SDR DL72E991664Valve · leakingON SHORT FINAL LOST ALL A HYD QTY AND PRESSURE. REPLACED FLOW REGULATOR VALVE, NR 1 AND 2 CASE DRAIN FILTERS SERVICED A HYD AND RAN ENGS. ALL INDICATIONS AND OPERATION CHECKS OK LEAK CHECKS OK.SDR DL72W991609Bulb · failedEMERGENCY LIGHT INOP LOCATED ON EXTERIOR OW BETWEEN RT EMERGENCY ESCAPE HATCHES. RELAMPED SAME, CHECKS GOOD.SDR DL72W991679Insulation · splitON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-24-026-SDR DL72W991678Insulation · splitON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-2SDR 99FDEA00263Bulb · failed99-159 - WHEN LAND GEAR 1ST LOWER NO DOWN IND ON LEFT MAIN. REMOVED AND REPLACED BULB. CK PROXIMITY SENSORS PER MM 32-61, OPS CK NORMAL.SDR DL72E991562Skin · crackedFUSELAGE SKIN, FS 481-681, STRG 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 28 CRACKS ALONGSDR DL72E991543Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 440 & 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND AN EXTSDR DL72W991507Fire Loop · failedNR 1 ENG B-FIRE LOOP ON MCO. A-LOOP FAULT LIGHT ILLUM, WOULD NOT TEST. CREW SHUT DOWN ENGINE IN FLT AND BLEW THE FIRE BOTTLE PER THE POM. REPLACED LOWER LOOP.SDR DL72W991502Battery · dischargedEMERGENCY LIGHT FIRST CLASS OVERHEAD INOP. REPLACED BATTERY, OPS NORMAL.SDR DL72W991494Ballast · failedAT DEPARTURE TIME, BURNING SMELL IN CABIN AND RT AFT CEILING LIGHT CIRCUIT BREAKER POPPED. FOUND CEILING BALLAST BAD AT SEAT 17. REPLACED SAME. .SDR UPS99230017Seat Track · crackedINSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 25, WL 206. REMOVED DAMAGED SECTION INSTALLED NEW SECTION, FABRICATED SPLICES AND REPAIR EXTRUSIONS, WORK DONE IAW SRM 51-30-2, 53-10-5 AND 51-20-4.SDR UPS99230016Seat Track · crackedINSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 45, WL 206. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION, FABRICATED AND INSTALLED FABRICATED ANGLES AND STRAPS WORK DONE IAW SRM'S 53-10-5 51-30-2 AND 51-20-4.SDR DL72W991479Fire Loop · malfunctionedWHEN TESTING SYS, NR 1 DETECTOR SYS A NR 1 FIRE HANDLE LIGHT COMES ON AND STAYS ON AFTER TEST IS COMPLETE. IN FLIGHT SHUTDOWN FOR FIRE WARNING EARLY TODAY. B SYSTEM ALREADY ON MCO. REPLACED LWR A-B FIRE LOOP, DET UNIT AND CONTROL PANEL.SDR DL72W991471Connector · dirtyINTERMITTENT FLASHING LIGHT SYS A FOR NR 1 ENG FIRE DETAT CRUISE, SMOOTH AIR. RAN PROCEDURE AND SHUT DOWN NR 1 ENG. REPLACED BLOWN FIRE EXT BOTTLE. FOUND OIL SOAKED CONNECTORS ON LOWER LOOP AND PYLON LOOP. CLEANED CONNECTORS, FIRE TEST NOW OPS NORMAL. INSSDR UPS99230019Angle · corrodedINSPECTION TYPE:C CORROSION (C53-111-03.00-01) ON L ANGLE AT BS 304, WL 150, RBL 20 (BELOW DOG HOUSE FLOOR). REMOVED, FABRICATED AND INSTALLED NEW ANGLE, WORK DONE IAW SRM 53-10-2, 51-30-2 AND SRM 51-40-2.SDR UPS99230018Angle · crackedINSPECTION TYPE:C JACK STAND COMPARTMENT SURROUNDING STRUCTURE IS CRACKED AND DENTED LBL 11 TO LBL 17. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE. WORK DONE IAW SRM'S 51-30-2, 53-10-1, 51-30-5 AND 51-10-2.SDR UPS99229981Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON LOWER CHORD OF BS 1130 FLOORBEAM AT NUT CLIP HOLES BL 0-RBL 50, WL 201. REPAIRED FLOORBEAM PER ER NR 99-5650.SDR DL72W991428Stiffener · crackedTPA LTR CHK B-1, O/B SPAR STIFFENER CRACKED AT NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 .SDR DL72W991427Frame · crackedFOUND AT B-1 LTR CK, AFT CABIN ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.SDR 99FDEA00226Clamp · failedENGINE 1 STRUT OVERHEAT LIGHT ILLUM. FOLLOW RED TAB PROCEDURE. REMOVED AND REPLACED FWD (UPSTREAM) CLAMP ON ENGINE BLD AIR SHUTOFF VALVE PER MM 36-10-001-4, MM 20-80-001-2, FIG 209.SDR UPS99229874Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 630 TO BS 638 RBL 45. REPLACED PER SRM 51-10-1.SDR UPS99229873Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 705 TO BS 708 RBL 95 WL 208. REPLACED TRACK PER SRM 51-10-1.SDR 99FDEA00225Valve · inoperativeNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENG WAS PROVIDING BLD FOR LEFT DUCT PRESSURE WHICH WAS 20 PSI HIGHER THAN RIGHT DUCT. REMOVED AND REPLACED NR 1 ENGINE HIGH PRESSURE MODULATING AND SHUTOFF VALVE PER MM 36-12-42 PG 401 AND 402. LEAK AND OPESDR UPS99229876Shear Tie · corrodedINSPECTION TYPE:SI, SHEAR TIE CORRODED BS 720 FRAME BETWEEN 25 AND 26 RT. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2 PG 2.SDR DL72E991379Bracket · crackedFOUND ON A1 LETTER CK, NR 8 SLAT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21.SDR UPS99229875Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 690 LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5 PG 4.SDR DL72E991366Line · leakingON TAKEOFF IMMEDIATELY AFTER SELECTING FLAPS TO 2 DEGREES FROM 5 DEGREES, EXPERIENCED A SYSTEM HYDRAULIC LOSS QTY AND PRESSURE DECREASED RAPIDLY TO 0. SYSTEM B NORMAL THROUGHOUT. MAINTENANCE FOUND ACTUATOR LINE IN NLG WHEELWELL LEAKING. REPLACED LINE, SERVISDR UPS99229845Stringer · corrodedINSPECTION TYPE:SI, CORROSIN AND TOOLING DAMAGE ON STRINGER 7 LT BS 720B AND 1270+18. REMOVED CORROSION DAMAGE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED STRINGER REPAIR PER SRM 53-10-3.SDR UPS99229842Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 5 FLAP TRACK AT SPOILER BEAM PAD FWD ATTACH LUG AND INSIDE L/G BEAM ATTACH HOLES. REMOVED NR 5 FLAP TRACK PER MM 27-51-31. REMOVED ATTACH HARDWARE ON NR 5 FLAP TRACK PER SRM 51-30-2. RECEIVED REPLACEMENSDR UPS99229841Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 1 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED NR 1 FLAP TRACK, ROUTED TO CSD, RECEIVED NEW FLAP TRACK AND INSTALLED IAW 27-51-31.SDR UPS99229844Seat Track · corrodedINSPECTION TYPE:SI, SEAT TRACK CORRODED AND DAMAGED TSS 1029 TO BS 1031 RBL 24 WL 208. AFTER REMOVAL OF CORROSION, FOUND THE SEAT TRACK TO GO BEYOND ALLOWABLE LIMITS PER SRM 53-10-1. FABRICATED NEW SEAT TRACK, ALODINED, PRIMED AND PAINTED AND INSTALLED SEAT SDR UPS99229843Frame · dentedINSPECTION TYPE:SI, DENTED I/B FLANGE ON FRAME AT BS 680, LBL 34, STR 24 IN FWD CARGO BAY. THE DENT ON FRAME OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS, ALODINED AND PRIMED THE REPAIR PARTS. INSTALLED REPAIR PARTS, ALL WSDR DL72W991309Web · crackedLT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A CRACK BETWEEN BS 294 AND 286 AT APPROX WL 170. REPAIRED PER ERA 367566-14.SDR 99FDEA00211Floorbeam · corrodedCORROSION (C53-111-01,3) ON FLOORBEAM LOWER CHORD AT BS 1070, WL 200, LBL 40 TO RBL 48. *S/D* REMOVED AND REPLACED FLOORBEAM PER FEDEX EA 7-5310-45262A.SDR DL72W991296Angle · crackedNR 13 SPOILER ACTUATOR SUPPORT FITTING O/B ATTACH ANGLE CRACKED. REPLACED ANGLE PER M/M 57-42-0 PG 802.SDR DL72W991295Skin · crackedFOUND ON F1 LETTER CK, .375 INCH CRACK ON LT ELEVATOR LOWER SKIN. REPAIRED PER SRM 55-20-3.SDR DL72W991293Frame · crackedFOUND AT F-1 LETTER CHECK, AFT ENTRY DOOR CUTOUT RT FRAME HAS .5 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.SDR UPS99229781Track · corrodedINSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED AND REPLACED NR 7 FLAP TRACK.SDR UPS99229778Keel Beam · corrodedINSPECTION TYPE:SI, CORROSION ON KEEL BEAM AT BS 760, RBL 7, LBL 7 WL 148. REPLACED PER SRM 51-10-1.SDR UPS99229776Shear Tie · corrodedINSPECTION TYPE:SI, CORROSION ON SHEAR TIE BS 1130 RBL 5 WL 148. REPLACED PER SRM 51-10-2, SRM 51-10-1.SDR DL72E991283Rib · crackedA-1 LTR CHK, NR 5 SLAT ACT NOSE RIB CRACKED O/B SIDE AT FWD RADIUS.SDR 99FDEA00206Frame · dentedTHREE DENTS ON TOP FLANGE OF FRAME AT BS 660 BETWEEN STRS 23 AND 26R. *S/D* REMOVED DAMAGE FROM INNER FLANGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-45287 AND SRM 51-40-2.SDR DL72E991292Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT AND AN EXTERNALSDR UPS99229784Skin · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-02.00-02) EMINATING FROM UNDER 3 RIVNUTS ON INNER SKIN OF AFT CARGO DOOR 11 FROM BOTTOM OF DOOR AFT OF FWD FRAME 10, 18 AND 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS ON INNER SKIN OF AFT CARGO DOOR AT 35 FROM FWD F
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