Boeing 727-231
Service difficulty reports · 840
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 = '727231' 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 = '727231' 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 TWAA9814302Gasket · leakingNR 1 STRUT OVERHEAT ILLUMINATED IN FLIGHT. EXTINGUISHED WHEN NR 1 BLEED SELECTED CLOSED. FLIGHT RETURNED TO STL. REPLACED 2 EA 13TH STAGE WING ANTI-ICE VALVE GASKETS. CHECK-C 8-23-98 MCI.SDR TWAA9814505Seat Track · corrodedDURING CHECK-C, FOUND CORROSION ON NR 1 CHAIR TRACK, LBL 46 IN AT STA 1100. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK AND FASTENERS PER SRM 53-10-5.SDR TWAA9814504Skin · corrodedDURING CHECK-C MAINT, FOUND FUSELAGE ON RT SIDE PELLOWING, PULLED, AND POPPED RIVET HEADS AT STA 660, S28R AND 28L. CORROSION REMOVED, INSTALLED DOUBLER OVER AREA OF SKIN THAT WAS BEYOND LIMITS OF CORROSION REMOVAL. ALSO, INCORPORATED EXISTING REPAIR PER SRMSDR TWAA9813202Power Supply · inoperativeEMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER WAS POPPING. REPLACED BATTERY POWER SUPPLY. CHECK-C 9-5-97.SDR TWAA9813201Circuit Breaker · trippedTHE EMERGENCY LIGHTS BATTERY CHARGER POPPED CIRCUIT BREAKER. CHECKED BATTERY CHARGER AND WIRING, NO PROBLEM FOUND. REPLACED 115V C/B. CHECK-C 9-5-97 MCI.SDR 98ZZZM617Battery Pack · dischargedON 'A' SERVICE, FOUND RIGHT OVEWING EMERENCY LIGHT INOPERATIVE. TROUBLESHOT SYTEM. FOUND RIGHT OVERWING BATTERY PACK LOW CHARGE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-1. (M)SDR TWAA9814506Intercostal · corrodedDURING CHECK-C, MAINT FOUND CORROSION ON VERTICAL INTERCOSTAL AT FS 700, STR 28L, BOTTOM MOUNTING FLANGE, BELOW FWD CARGO COMPT FLOOR LEVEL. CORRODED PARTS REMOVED AND REPLACED WITH NEW PARTS MADE OF 7075T6. TREATED, PAINTED, SEALED AND INSTALLED WITH RIVETSSDR TWAA9814502Panel · crackedDURING CHECK-C MAINT, FOUND RT WING UPPER WING PANEL CRACKED AT OTBD END OF OTBD SPOILER. INSTALLED FIBERGLAS REPAIR PER SRM 57-20-4 AND 51-40-6.SDR 98ZZZM585Fire Loop · malfunctionedPASSING THROUGH FL190 ON TAKEOFF WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. IN MIA REMOVED AND REPLACED LEFT AND RIGHT WHEEL WELL FIRE WARNING SENSOR LOOPSSDR 98ZZZM586Fire Loop · malfunctionedPASSING THROUGH FL190 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. ON ARRIVAL PERFORMED VISUAL INSPECTION OF DETECTOR LOOPS, SENSORS, WHEEL WELL AND LANDING SDR TWAA9814501Skin · missingRT WING INBD MID FLAP HAD PIECE OF SKIN MISSING, 4 IN BY 16 IN, TOP OTBD EDGE. REPAIRED RT MID FLAP PER BOEING 727 SRM 51-40-6. CHECK-C 2-13-98 MCI.SDR TWAA9812001Rt Unit · failedSMOKE REPORTED TO BE COMING FROM BEHIND THE FIRST OFFICERS INSTRUMENT PANEL. FLIGHT DIVERTED TO ABQ. FOUND WEATHER RADAR CIRCUIT BREAKER POPPED. REPLACED WEATHER RADAR NR 1 RECEIVER/TRANSMITTER. CHECKED ELECTRICAL WIRE BUNDLES IN ELECTRONIC COMPT, CHECKED SDR TWAA9812212Skin · wornDURING CHECK C, FOUND RT WING RT O/B FOREFLAP WITH ROUND DEPRESSION WORN IN I/B LEADING EDGE. INSTALLED 2024-T42 DOUBLER PER SRM 57-50-4, PG 2B.SDR TWAA9812211Skin · corrodedDURING CHECK-C, FOUND 14 IN BY 2 IN BY .375 IN HOLE IN LT WING L/E ABOVE LANDING LIGHT. ACCOMP FLUSH REPAIR PER SRM 57-30-4, PAGES 2B, 3, AND 4, FIG 2.SDR TWAA9812209Rib · crackedDURING CHECK-C, FOUND CRACK 17 IN LONG AT BOTTOM OF RT WING RIB WEB ANGLE, 27 IN O/B OF WING BODY FAIRING, FWD. REMOVED AND REPLACED WEB ANGLE AT O/B END OF WING BODY FAIRING, PER SRM 51-10-1, AND 51-40-3.SDR TWAA9812210Stringer · corrodedDURING CHECK-C, FOUND FS 720, S28L WITH CORROSION. HEAVY CORROSION ON STRINGER, LIGHT SKIN CORROSION. REMOVED SKIN CORROSION PER SRM 51-10-6, AND FABRICATED NEW STRINGER AND INSTALLED PER SRM 51-10-1.SDR TWAA9811701Lights · inoperativeDURING OVERNIGHT MAINTENANCE, FOUND THE AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED THE LIGHT ASSEMBLY. CHECK-C 10-31-97. (M)SDR 98ZZZX2876Light · inoperativeLOG PAGE: 24839: ON PRE-FLIGHT TRANSIT, FOUND ESCAPE PATH LIGHTING R2 DOOR NOT LIGHTING. TROUBLESHOT SYSTEM. REPAIRED WIRING. OPS CHECKED OK IAW 33-50-01. (X)SDR TWAA9812208Stringer · corrodedDURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5.SDR 98ZZZX2877Control Unit · malfunctionedLOG PAGE: 24836 - DURING CRUISE, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED AOM PROCEDURES AND INDICATION DID NOT RETURN. THE NGU TROUBLESHOT SYSTEM, INSPECTED LOOPS, WIRING, GROMMETS, AND FASTENERS IN L/R WHEELS. NO DEFECTS NOTED. REMOVED WSDR TWAA9811101Cover · crackedIN THE AFT CABIN, A FOUR-INCH SECTION OF TH EGRESS LIGHT COVER WAS FOUND BROKEN AND A PIECE MISSING. REPLACED SECTION OF COVER. CHECK-C 5-25-98 JFK.SDR EISA98178Generator · malfunctionedDURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMINATED. COULD NOT BRISDR 98ZZZX2879Voltage Reg · malfunctionedDURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMINATED. COULD NOT BRISDR 98ZZZX2878Generator · malfunctionedDURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMINATED. COULD NOT BRISDR TWAA9810902Light · inoperativeSTL - DURING MAINTENANCE FOUND EGRESS FLOOR LIGHTS INOPERATIVE AT OVERWING EXIT. RECONNECTED FLOOR LAMP AT OVERWING EXIT. CHECK-C 10-20-97 JFK. (X)SDR TWAA9810901Lamp · failedSTL - DURING MAINTENANCE, FOUND FWD GALLEY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LIGHT. CHECK-C 10-20-97 JFK. (X)SDR TWAA9810502Light · looseJFK - FLT 361 - EGRESS FLOOR STRIP LIGHTING COMING LOOSE AT ROW 15 LEFT SIDE. FLOOR STRIP WAS SECURED. (M)SDR EISA98168Switch · inoperativeNR 3 OIL FILTER BYPASS LIGHT CAME ON WHEN TAKEOFF POWER WAS SET. EXTINGUISHED AFTER CLEARING RUNWAY. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 3 ENGINE OIL FILTER BYPAS SWITH IAW MM CHAPTER 79. OPS CHECK GOOD. (M)SDR TWAA9810303Power Supply · inoperativeSTL - FLT 611 - EGRESS LIGHTING AFT OF ROW 22 CAME ON IN-FLIGHT. REPLACED EGRESS POWER SUPPLY ABOVE SEAT 24. CHECK-C 10-21-97 MCI. (X)SDR EISA98140Structure · corrodedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD NR 269, INSPECTION OF PLENUM CHAMBERS. OBSERVED CORROSION AT STR S4C AND LBL 29.9 AND LBL 31.8 AND STR S3C RBL 16.5 AND STR S4C AT RBL 32.0. BOEING REPAIR NR EOIR980527 AND EOIR980529. (X)SDR EISA98129Fitting · mismanufacturedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD 045R, FOUND RIGHT HAND 740 FITTING CRACKED. DURING REPLACEMENT OF 740 FITTING, FOUND THAT REPLACEMENT FITTING WAS DIFFERENT. THE EDGE DISTANCE WAS TOO CLOSE. BOEING ENGINEERING SUPPLIED DRAWING AND INFORMATSDR TWAA9809804Skin · crackedMCI - DURING CHECK-C, MAINTENANCE FOUND RT WING LE WITH CRACKS IN SKIN AND RIVETS CRACKED AND LOOSE, 19 INCHES OTBD OF NR 5 LE SLAT OTBD 'UP' STOP. REMOVED CRACKED SKIN AND REPAIRED PER SRM 57-30-4, PAGES 10 AND 11. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: SDR TWAA9809802Door Stop · crackedJFK - EDDY CURRENT FOUND LT NR 1 CABIN DOOR TOP AFT DOOR STOP CRACKED. REMOVED AND REPLACED STOP FITTING PER 727 SRM 51-10-1. CHECK-C 5-10-98 JFK. TOTAL TIME: 70,079 HOURS. TOTAL CYCLES: 46,814. (X)SDR TWAA9809801Skin · crackedMCI - DURING CHECK-C MAINTENANCE FOUND ON RT WING LE A CRACK IN THE SKIN AT RIVETS, AND THE RIVETS WERE CRACKED AND LOOSE, 11 IN OTBD OF NR 5 LE SLAT OTBD UP-STOP. REMOVED CRACKED SKIN AND REPAIRED PER SRM 57-30-4, PAGES 10 AND 11. TOTAL TIME: 47,795 HOURS.SDR TWAA9809201Wire · looseDSM - FLT 290 - DURING GROUND CHECK OF EGRESS LIGHTS FOUND ONE ESCAPE PATH LIGHT STRIP INOP IN MID CABIN. PLACARDED LIGHT PER MEL. ON LAYOVER PLUGGED IN THE LIGHT STRIP IN WORKED NORMAL. CHECK-C 8-30-97 MCI. (M)SDR TWAA9809806Skin · corrodedMCI - DURING CHECK-C, MAINTENANCE FOUND COROSION ON RT SIDE OF FUSELAGE SKIN AT STA 870, STR 10R. REMOVED CORROSION PER SRM 51-10-6. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-3, PAGE 14D. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,SDR TWAA9809805Floorbeam · corrodedMCI - DURING CHECK-C, MAINTENANCE FOUND CORROSION ON RT FLOOR SUPPORT ANGLE FROM STA 370 TO STA 418, AT RT SERVICE DOOR THRESHOLD. REPLACED ANGLE PER SRM 51-10-1, AND TWA STD PRACTICES. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. (X)SDR TWAA9809008Battery · dischargedSTL - FLT 8601 - DURING PRE-FLIGHT INSPECTION, FOUND AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES MFG PN 30-0544-1. CC-01 10-31-97 JFK. (X)SDR TWAA9809007Power Supply · failedSTL - FLT 8601 - DURING PRE-FLIGHT INSPECTION, FOUND L1 AND R1 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY MFG PN 61-0478-1. CC-01 10-31-97 JFK. (X)SDR TWAA9809803Floorbeam · corrodedMCI - DURING CHECK-C, MAINTENANCE FOUND CABIN FLOOR SUPPORT AT STA 418 WITH CORROSION FROM RBL 44 INTO OTBD END OF SUPPORT. NEW SUPPORT INSTALLED PER SRM 51-10-1, PAGES 4 AND 4A. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. (X)SDR TWAA9809001Cover · looseJFK - FLT 904 - REPORT TO MAINTENANCE THAT THE EGRESS LIGHTS AT ROW 13 WERE BUCKLED UP. COVER WAS RESECURED. CC-04 4-3-98 JFK. (X)SDR TWAA9808401Pump · failedSTL - FLT 484 - DURING CRUISE, LOST 'B' HYDRAULIC SYSTEM PRESSURE. REPLACED 'B' SYSTEM HYDRAULIC PUMPS NR 1 AND NR 2 MFG P/N A00336-2. (M)SDR EISA98133Frame · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD SEQ 237, RIGHT SIDE STA 760.95 FOUND FRAME CRACKED. INSTALLED BOEING REPAIR KIT PER SB 53-0197. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)SDR EISA98132Fitting · crackedDURNG ACCOMPLISHMENT OF ROUTINE WORK CARD 045 OR SB 53-62 R6, INSPECTION OF 740 FITTINGS FOUND RIGHT HAND 740 FITTING CRACKED. REPLACED RIGHT-HAND 740 FITTING PER SB 53-0062. USED BOEING KIT 65C13724-96. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)SDR EISA98131Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE WORK CARD FOR C-CHECK SEQ 237, FOUND UPPER RIB CHORD CRACKED AT BBL 70.5 STA 760.95 ON LEFT HAND SIDE OF AIRCRAFT. INSTALLED REPAIR KIT PER SB 57-112 R5. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)SDR EISA98130Fitting · crackedDURING ACCOMPLISHMENT OF C-CHECK, CPCP CARD NR C53-100-01, BS 1170 LEFT HAND SIDE AT AFT LAV DOOR AREA STR 20 FOUND BULGE, OPENED SKIN FOUND CRACK AND CORROSION ON FITTING. REMOVED CORROSION AND REPLACED STRINGER PER MM 53-10-3. ACFT TT: 65,287:32 HOURS. ASDR 98ZZZM489Pump · failedSTL - FLT 484 - DURING CRUISE, LOST 'B' HYDRAULIC SYSTEM PRESSURE. REPLACED 'B' SYSTEM HYDRAULIC PUMPS NR 1 AND NR 2 MFG P/N A00336-2. (M)SDR EISA98119Battery Charger · failedON POST-FLIGHT INSPECTION, FOUND THE BATTERY VOLTAGE TO BE ZERO. AFTER CONSULTING WITH MAINTENANCE (BRUSSELS), FOUND A 50-AMP CIRCUIT BREAKER IN LOWER 48 LABELED BATTERY CHARGER. WHEN CIRCUIT BREAKER WAS RESET, BATTERY POWER RESTORED, HOWEVER, AFTER 2 MINUTESDR TWAA9807603Tire · failedSLC - FLT 342 - DURING TAKEOFF FROM SLT, THE LEFT INBOARD TIRE CAME APART AND WAS DIGESTED INTO THE NR 1 ENGINE. SHUT DOWN NR 1 ENGINE. FLT PROCEEDED TO HOLDING AREA TO DUMP FUEL, THEN RETURNED TO SLC. REPLACED WHEEL, REPAIRED DAMAGE TO TE FLAP, AND REPLACESDR TWAA9806204Stringer · corrodedJFK - DURING C-CHECK, FOUND FUSELAGE STRINGER 27L WITH CORROSION BETWEEN STATION 700 AND STATION 720. REMOVED SECTION OF STRINGER AND INSTALLED SPLICE SECTION PER SRM 53-10-3. (M)
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