Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 02FDEA00500Clamp · brokenLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CRUISE AT FL 310, 20 MINUTES AFTER TAKEOFF. ACCOMPLISHED CHECK LIST PROCEDURES AND LIGHT EXTINGUISHED IAW CHECK LIST LEAK WAS BETWEEN BLEED VALVE AND PACK VALVE. REPLACED BROKEN SUPPORT CLAMP SET BLEED DUCT ONSDR 02FDEA00496Sleeve · deterioratedLOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. COMPLIED WITH QRH & SECURED RIGHT PACK NR 3 ENG BLEED. LIGHT STAYED ON IAW QRH, MOVED NR 3 THROTTLE TO IDLE, AND OVERHEAT LIGHT IMMEDIATELY WENT OUT. QRH INDICATES LEAK IS BETWEEN NR 3 BLEED VALVE ANSDR 02FDEA00497Oxygen Bottle · faultyTHIRTY MINUTES INTO FLIGHT AT FL 350 OXYGEN QTY INDICATES ZERO. ALL OXYGEN REGULATORS WERE IN EMERGENCY-OFF POSITION. PERFORMED LEAK CHECK OF OXYGEN LINES IN E&E BAY, NO LEAKS. CHECKED ALL MASKS AT REGULATORS IN COCKPIT, CHECK OK. REPLACED BOTH OXYGEN BOTTSDR 02FDEA00490Wire · chafedREPEAT WRITE UP. NR 3 GENERATOR BREAKER TRIPPED, ACCOMPLISHED CHECKLIST PROCEDURES. RESET GENERATOR AND IT RE-TRIPPED AFTER 1 MINUTE. REMOVED AND REPLACED NR 3 ENG DRIVEN GENERATOR IAW 727 MM 24-20-001-4. FOUND FIELD EXCITATION WIRE (F) CHAFED THROUGH WISDR 02FDEA00487Gcu · malfunctionedNR 3 GENERATOR BREAKER TRIPPED. RESET IAW CHECK LIST. RETRIPPED AFTER APPROXIMATELY 1 MINUTE. NR 2 FIELD AND NR 2 GENERATOR TRIPPED. ACCOMPLISHED CHECK LIST PROCEDURES. UNDER VOLTAGE INDICATED ON NR 2. REMOVED AND REPLACED NR 3 GENERATOR CONTROL UNIT ISDR 02FDEA00486Switch · faultyHYD A-SYSTEM OVERHEAT LIGHT ILLUMINATED ON TAXI OUT. RAN THE CHECKLIST AND LIGHT EXTINGUISHED. TALKED WITH MX T/O. DURING CLIMBOUT HYD A-SYSTEM OVERHEAT LIGHT RE-ILLUMINATED. RAN THE CHECKLIST AND RETURNED TO MEM. REMOVED AND REPLACED NR 1 & NR 2 ENG HYD SDR 02FDEA00475Hydraulic Line · looseRIGHT GEAR FAILED TO RETRACT AFTER T/O. GEAR DOOR INTRANSIT LIGHT FLICKERED GREEN, RIGHT GEAR LIGHT REMAINED ILLUM'D WITH THE GEAR HANDLE IN THE OFF POSITION. SECURED LOOSE HYDRAULIC LINE ON SEQ VALVE AND RECENTERED RIGHT GEAR UPLOCK MECH MG, OPS CHECK OK PESDR 02FDEA00480Stringer · crackedCRACKED STRINGER AT VERTICAL FIN STA 20, STR LT RIB NR 2. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1. REPAIRED STR 4 LT AT VERTICAL FIN STA 20, RIB NR 2 IAW SRM 55-30-4 FIG 1.SDR 02FDEA00481Stringer · crackedCRACKED STRINGER AT VERT FIN STRINGER 8 AT RIB NR 2 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1.SDR 02FDEA00474Relief Valve · out of adjustNR 2 OIL PRESSURE READ 60 PSI DURING INITIAL CLIMBOUT. AFTER REACHING 5K NR 2 THROTTLE PULLED TO IDLE IAW RED TAB PROCEDURE. OIL PRESSURE DROPPED TO 58 PSI INITIALLY THEN SLOWLY DROPPED INTO GREEN BAND APPROX 52 PSI AT IDLE AND REMAINED THERE DURING APPROACHSDR 02FDEA00472Frame · corrodedCORROSION ON FRAME WEB BS 990, STR 24 RT. REPAIRED FRAME BS 990 STR 22-29 RT PER SRM 51-40-2.SDR 02FDEA00431Skin · corrodedFOUND CORROSION ON SKIN UNDER WEB/INTERCOSTAL AT BS 950F - 970, LBL 14, WL 148. REPAIRED SKIN BS 950F - 970, LBL 14, WL 148 IAW SRM 53-30-3 FIG 3.SDR 02FDEA00433Skin · corrodedFOUND CORROSION AT STR 28L, BS 950F+8, WL 148. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 3.SDR 02FDEA00434Frame · corrodedFOUND FRAME CORRODED AT BS 720C, RBL 25, WL 148 C53-111-01. REMOVED AND REPLACED FRAME PER SRM 51-40-3 FIG 1.SDR 02FDEA00432Frame · corrodedCORROSION ON FRAME AND SHEAR TIE BS 990 BETWEEN STR 28-29 LT. REPAIRED SHEAR TIE & FRAME IAW FEDEX EA 7-5310-64980 & SRM 53-10-4 FIG 15.SDR 02FDEA00435Angle · crackedAFT AIRSTAIR RT LWR TORQUE BOX INTERNAL BS 1263 BULKHEAD UPPER FWD SIDE L-ANGLE IS CRACKED, JUST BELOW AIR STAIR ACTUATOR. REMOVED AND REPLACED AFT AIRSTAIR PER SRM 51-30-2 & 51-10-2.SDR 02FDEA00424Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON FOLLOWED RED TAB PROCEDURES. LIGHT EXTINGUISHED 1 MINUTE AFTER NR 3 BLEED AND RIGHT PACK VALVES WERE CLOSED. RAN NR 3 ENG PER JRH CHAPTER 5A, COULD NOT DUPLICATE. FAULT ON LEAK CHECK FOUND CLAMP LOOSE DOWN STREAM OF NR SDR 02FDEA00429Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 890, LBL 50-52, WL 201 AFT SIDE OF LWR FLANGE UPPER SIDE.SDR 02FDEA00423Warning System · malfunctionedFUEL HEAT ICING LIGHT ILLUMINATED ON ENG NR 3 APPROX 10-11000 MSL FOR ABOUT 1-2 MIN, THEN WENT OUT AND STAYED OUT. FUEL TEMP WAS +35DC. SUMPED ALL TANKS AND FOUND NO CONTAMINATION. FOUND FUEL FILTER PRESSURE SWITCH BACKSHELL EXTREMELY LOOSE AND WILL NEED TISDR 02FDEA00421Skin · corrodedCORROSION AT INNER SKIN SURFACE AT BS 470, WL 138, BL 0, COMMON TO ANTENNA MOUNT AREA.SDR 02FDEA00414Spar · chafedVERT FIN MID SPAR IS CHAFED AT STA 228, LEFT HAND SIDE. REMOVED AND REPLACED VERT FIN PER EA 7-5510-64976.SDR 02FDEA00415Spar · chafedVERT FIN MID SPAR IS CHAFED AT STA 228 RIGHT HAND SIDE. REMOVED AND REPLACED VERT FIN MID SPAR PER EA 7-5510-64975.SDR 02FDEA00413Frame · chafedCHAFING ON FRAME FROM HYDRAULIC LINE AT BS 560, STR 4R.SDR 02FDEA00418Skin · corrodedCORROSION STR 19L TO 23L, BS 350-360 SKIN BULGING AROUND FASTENERS. REMOVED AND REPLACED SKIN PER EA 7-5330-64974 & SRM 53-30-3.SDR 02FDEA00407Oil Cooler · faultyDURING CLIMBOUT NR 1 CSD AND NR 3 CSD OVERHEATED (NR 1 REPEAT), NR 1 WAS 130C & NR 3 125C WITH NR 2 105C (IN LIMITS). IAW QRH NR 1 GEN BREAKER WAS TRIPPED AND WAS STILL OVER 120C AFTER 3 MIN. DISCONNECTED NR 1 CSD. NR 3 GEN WAS TRIPPED AND WAS OVER 120C AFTSDR 02FDEA00396Overheat Loop · out of positionDURING CR FLT AT FL350 BOTH PACKS ON GOT A LWR AFT BODY OVERHEAT WARNING LIGHT. COMPL WITH RED TABS. WHEN R/PACK & ENG NR 3 BLEED AIR VLVS CLOSED, LIGHT WENT OUT WITH THROTTLE NR 3 REDUCTION. SYSTEM CK GOOD. LEFT RT PACK AND NR 3 BLEED SWITCHES CLOSED. RESDR 02FDEA00400Frame · dentedFRAME DENTED BS 500, STR 24 - 25L.SDR 02FDEA00399Floorbeam · corrodedCORROSION ON UPPER FLANGE OF FLOORBEAM BS 1050, LBL 19, WL 208.SDR 02FDEA00401Frame · dentedFRAME DENTED BS 680, STR 24R.SDR 02FDEA00447Fitting · corrodedLEFT WING O/B AILERON FITTING CORRODED ON TOPSIDE OF FITTING. REMOVED AND REPLACED FITTING PER MM 27-10-131-4.SDR 02FDEA00428Keelbeam · crackedRIGHT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS. R & R KEELBEAM PER SRM 51-30-2.SDR 02FDEA00410Keelbeam · crackedRT WHEEL WELL KEELBEAM FWD VERTICAL CHORD IS CRACKED BETWEEN TWO FASTENERS.SDR 02FDEA00398Floorbeam · corrodedCORROSION ON FLOORBEAM LWR FLANGE BS 900, LBL 54-68, WL 208 (C53-224-01, 2).SDR 02FDEA00385Overheat Loop · faultyDURING CRUISE FLT AT FL330 WHEN POWER WAS REDUCED TO DESCEND, LOWER AFT BODY OVERHEAT LIGHT FLICKERED THEN CAME ON STEADY. COMPLIED WITH RED TAB PROCEDURES, LIGHT WENT OUT. SYSTEM TEST SATISFACTORY. MONITORED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED FSDR 02FDEA00393Strap · crackedLAST HOLE IN REINFORCEMENT STRAP CRACKED. REMOVED AND REPLACED STRAP PER SRM 51-30- 5, 51-10-2.SDR 02FDEA00386Stringer · crackedCRACKED STR WITH 4 OPEN HOLES BS 640, STR 27 LT. REMOVED AND REPLACED STRINGER PER SRM 53-10-3 FIG 1.SDR 02FDEA00394Angle · crackedHOLE IN L-ANGLE CRACKED AT BS 783.SDR 02FDEA00392Skin · chafedSKIN CHAFED AT BS 1352 AT NR 2 ENG RT RAIN GUTTER 15 INCHES BELOW NR 3 PYLON T/E AND RAIN GUTTER. REMOVED AND REPLACED PER EA 7-5410-64955 & SRM 54-30-3.SDR 02FDEA00391Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM BS 360, RBL 6. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.SDR 02FDEA00387Structure · damagedAFT LWR CARGO DOOR HAS DAMAGE AT FWD UPPER CORNER. REMOVED AND REPLACED DOOR PER SRM 52-00-3 FIG 4, 52-00-2.SDR 02FDEA00381Floorbeam · corrodedCORROSION ON FLOORBEAM BS 900, LBL 43. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-64924.SDR 02FDEA00371Overheat Loop · faultyLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT DOWN TO LEAK BETWEEN NR 3 BLEED & RT PACK VALVE. OPENED KEEL BEAM ACCESS IN RT W/W AND LEAK CHECKED WITH NR 3 ENGINE RUNNING NO LEAKS FOUND IN KEEL BEAM AREA, CARGO COMPARTMENT, OR AFT STAIRS ASDR 02FDEA00379Frame · damagedMECHANICAL DAMAGE TO FRAME AT BS 720, STR 4L AND CEILING SUPPORT. REMOVED AND REPLACED FRAME PER SRM 53-10-4.SDR 02FDEA00370Duct · leakingLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER 1+10 FLIGHT TIME. DID RED TAB PROCEDURE. ISOLATED LEAK ON NR 3 ENG BETWEEN BLEED VALVE AND RIGHT PACK VALVE. FOUND STARTER DUCT LEAKING ON NR 3 ENG BLEED MANIFOLD. STARTER DUCT WAS MISALIGNED, REALIGNED STARSDR 02FDEA00367Web · corrodedSHEAR WEB BULGING AROUND FASTENERS BS 1147, LBL 53-61, WL 208. REMOVED AND REPLACED WEB & FLOORBEAM PER SRM 51-40-2 FIG 1 & 53-10-8 FIG 3.SDR 02FDEA00368Floorbeam · crackedCORROSION BS 870, WL 208, LBL 65 TO RBL 65. REMOVED AND REPLACED FLOORBEAM PER EA 7- 5310-54227.SDR 02FDEA00369Floorbeam · corrodedCORROSION ON TOP OF FRETTED FLOORBEAM BS 740, WL 208, LBL 60 - RBL 65. REMOVED AND REPLACED FLOORBEAM PER SRM 51-20-4, 51-30-2.SDR 02FDEA00364Engine · failedAFTER 30 MINUTES IN FLIGHT OIL TEMP CLIMBED TO YELLOW BAND DURING RED TAB PROCEDURES WITH ENGINE AT IDLE TEMP CLIMBED ABOVE RED BAND. SHUT DOWN NR 3 ENGINE IN ACCORDANCE WITH RED TABS. REMOVED AND REPLACED OIL TEMP BULB PER M/M 727-200 79-34-021-4, LEAK AND SDR 02FDEA00362Frame · crackedWHILE WORKING FOUND FRAME CRACKED AT BS 720, LBL 2, WL 154. REMOVED AND REPLACED FRAME PER SRM 51-40-3 & EA 7-5310-64910.SDR 02FDEA00363Screen · dirtyON CLIMBOUT APPROX 1500 AGL AFTER SETTING QUIET EPR AND RETRACTING FLAPS TO 5 DEGREES, EXPERIENCED SEVERE COMPRESSOR STALL WITH AUTOPACK TRIP, ENGINE PARAMETERS REMAINED WITHIN LIMITS RETURNED TO GTF. PERFORMED TROUBLESHOOTING PER PWA JT8D M/M 72-00-00 STEPS
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