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 02FDEA00649Overheat Loop · out of positionFL 280 LOWER AFT BODY OVERHEAT LIGHT CAME ON. BLEED 3 OPEN, RIGHT PACK OPEN. CARGO HEAT OUTFLOW NORMAL. FOLLOWED QRH PROCEDURE. DESCENDED TO FL 250, RIGHT NR 2 BLEED OPEN, RIGHT PACK ON. CARGO HEAT OUTFLOW NORMAL. INCREASED THRUST ON NR 3 ENGINE TO 85.5 SDR 02FDEA00650Switch · faultyDURING GEAR RETRACTION DURING TAKEOFF A RED DOOR WARNING LIGHT ON THE GEAR WARNING PANEL AND ASSOCIATED RIGHT GEAR DOOR LIGHT ON SECOND OFFICERS PANEL ILLUMINATED AFTER PLACING THE GEAR HANDLE TO THE OFF POSITION. QRH WAS REFERENCED. LIGHT WENT OUT AFTER PLASDR 02FDEA00646Computer · faultyON CLIMB OUT EXCESSIVE PITCH FORCE NEEDED TO ROTATE. ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED WITH ASSOCIATED SLOW A SYSTEM LEAK. PERFORMED HYD SYS LEAK OR LOSS CHECKLIST AND ISOLATED LEAK TO ELEVATOR SYSTEM A. DUMPED FUEL AND RETURNED FOR LANDSDR 02FDEA00643Control Unit · malfunctionedLOWER AFT BODY OVERHEAT LIGHT STARTED TO FLICKER ON PASSING THROUGH 27K FT. ON CLIMBOUT LIGHT WENT OUT AFTER TURNED OFF RT PACK AND CLOSED BLEED NR 3 COMPLETED QRH PROCEDURES CONTINUED AT FL280. COMPLIED WITH ADJUST AND TEST AND TROUBLE SHOOTING CHART UNABLESDR 02FDEA00653Skin · dentedDENT ON FUSELAGE EXTERIOR SKIN AT BS 194 BELOW STR 20L. R&R SKIN PER SRM 53-30-3 FIG 24.SDR 02FDEA00633Sensor · failedDURING TAKEOFF ROLL THE RIGHT GEAR RED LIGHT CAME ON AFTER GEAR RETRACTION THE RED GEAR LIGHT REMAINED ON WITH ALL OTHER GEAR LIGHTS EXTINGUISHED (GEAR WAS RE-CYCLED). REPLACED RT MAIN GEAR UPLOCK SENSOR PER M/M 32-61-081-4. ALSO REPLACED THE LANDING GEAR ACSDR 02FDEA00624Warning Light · illuminatedLOUD BOOM & AIRFRAME SHUDDER EXPERIENCED ON CLIMBOUT, AUTOPACK TRIP ACTIVATED. ENGINE FAIL LIGHT BLINKED MOMENTARILY, BUT STAYED OUT. SUSPECT COMPRESSOR STALL BUT UNABLE TO IDENTIFY ENG. ALL ENG INSTRUMENTS NORM. BORESCOPED ENGINES 1, 2, 3 PER MM 72-00-00-SDR 02FDEA00627Stringer · crackedSTR 15L IS CRACKED AT BS 720B+16. R&R STRINGER PER SRM 53-10-3.SDR 02FDEA00626Skin · chafedCHAFING ON SKIN LAP BS 720D PLUS 10 STR 19L. R&R SKIN PER SRM 53-30-3 FIG 14 & DWG SR 27-57-056.SDR 02FDEA00625Skin · chafedSKIN CHAFED AT BS 720D+10, STR 19R.SDR 02FDEA00632Frame · gougedGOUGE IN FRAME BS 348, LBL 44, WL 281.SDR 02FDEA00630Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 660, STR 6L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00629Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 660, STR 9L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00628Stringer Clip · crackedSTR CLIP CRACKED AT BS 660, STR 7L. R&R STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00621Switch · faultyDURING FLAP RETRACTION FROM 15 TO 5 L/E FLAP INDICATOR WENT FROM GREEN TO AMBER. S/O LED POSITION INDICATORS SHOWED NR 6 LED RETRACTED. CYCLING FLAPS CHANGED NOTHING. LANDED WITH FLAPS 30 WITH A L/E FLAP AMBER WITH NR 6 INDICATING RETRACTED. REPLACED NR 6 SDR 02FDEA00622Module · faultyLEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON TAKEOFF AFTER GEAR RETRACTION. CYCLED GEAR PER QRH. ALL GEAR EXTENDED NORMALLY, BUT LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER RETRACTION. FLIGHT CONTINUED PER QRH WITH GEAR HANDLE IN THE UP POSITION. PSDR 02FDEA00685Stringer Clip · damagedSTR 7R CLIP AT BS 720F HAS ELONGATED HOLE IN CLIP AND FRAME. R&R STRINGER CLIP PER SRM 51-30-2.SDR 02FDEA00603Controller · faultyLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT AT FL250. ENG A/ICE HAD BEEN ON FOR SEVERAL MINUTES PRIOR AND TURNED OFF PRIOR TO GOING TO QRH. LIGHT EXTINGUISHED PER QRH PROCEDURE, REPEAT WRITE-UP. REMOVED AND REPLACED FIRE DETECTION CONTROLLER PER MM SDR 02FDEA00606Flap · failedOUTBOARD FLAPS DID NOT EXTEND PAST 23 ALTERNATE FLAP MOTOR USED TO EXTEND FLAPS.SDR 02FDEA00599Warning System · false activationAT FL 280 DURING CLIMB THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. PROCEDURE WAS ACCOMPLISHED. WHEN ENG NR 3 BLEED VALVE AND THE RIGHT PACK WERE CLOSED AND TURNED OFF, THE LIGHT WENT OUT IN 2 MINUTES. SYSTSDR 02FDEA00594Beam · damagedTWO HOLES WITH PILOT HOLES ADJACENT TO THEM AND 1 ELONGATED HOLE IN STUB BEAM WEB AT BS 783, WL 204-207, LBL 65. REMOVED AND REPLACED STUB BEAM PER EA 7-5310-65851.SDR 02FDEA00595Skin · damagedCOMPLY WITH EA 7-5330-65843 FUSELAGE SKIN REPAIR BS 304 & STR 22R/23R. COMPLIED WITH EA 7-5330-65843.SDR 02FDEA00593Cooler · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. NO PACK TAKEOFF, ALL BLEED AIR SWITCHES CLOSED, 0 PSI MANIFOLD PRESSURE PRIOR TO TAKEOFF. LIGHT WENT OUT AS THRUST LEVERS RETARDED AND NR 1 BLEED AIR VALVE WAS OPENED. OVERHEAT SYSTEM TESTESDR 02FDEA00591Skin · gougedSKIN GOUGED AT BS 720D+13, STR 10L.SDR 02FDEA00584Module · defectiveNOSE GEAR LIGHT (GREEN) DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. PUSHED PRESS TO TEST GREEN LIGHT ILLUMINATED. MANUALLY EXTENDED THE GEAR. CHECKED ALIGNMENT STRIPE ON NOSE, INDICATED DOWN AND LOCKED BUT STILL NO GREEN LIGHT. REPUSHED PRESS TO TEST AND GRESDR 02FDEA00586Skin · chafedEXTERNAL SKIN CHAFED AT STR 19 LT, BS 720D+13.SDR 02FDEA00582Switch · faultyDURING INITIAL TAKEOFF, AS FLAPS WERE BROUGHT FROM 5' TO 2' THE L/E FLAP INDICATOR REMAINED AMBER (DID NOT SHOW GREEN). L/E FLAPS POSITION TEST ON S/O PANEL INDICATED 2, 3, 5, 6 & 7 STILL EXTENDED (IN GREEN). QRH (RED TABS) PROCEDURE ACCOMPLISHED. UNEVENTFUSDR 02FDEA00580Skin · dentedDENT IN SKIN AT BS 1072, RBL 60, WL 200. REMOVED AND REPLACED SKIN PER SRM 53-30-1.SDR 02FDEA00585Keelbeam · corrodedCORROSION (C53-113-01) ON KEELBEAM FLANGE AT BS 950B - 950B+11, LBL 7, WL 149. REMOVED AND REPLACED KEELBEAM FLANGE PER DWG 27-53-023.SDR 02FDEA00590Skin · damagedBULGE IN SKIN AT STR 28L, BS 1030. REMOVED AND REPLACED SKIN PER SRM 53-10-3 & 53-30-3, 53-30-1 FIG 2.SDR 02FDEA00587Brake Assy · fireFIRE IN RIGHT MAIN LANDING GEAR BRAKE AFTER SHUTDOWN CLEARED TO LAND ON 19R AT ICT. WINDS 020/8. TOOK LONGER THEN NORMAL TO SLOW DOWN TO TAXI SPEED. EVERYTHING ELSE WAS OTHERWISE NORMAL. FIRE STARTED AFTER BLOCK IN. FIRE WAS AT NR 3 BRAKE ASSEMBLY. INSPESDR 02FDEA00601Floorbeam · corrodedCORROSION ON BS 344 FLOORBEAM TOP CHORD AT NUT PLATE LOCATIONS UPPER AND LWR FLANGES LBL 57 TO RBL 12, WL 208. R&R UPPER CHORD ON FLOORBEAM PER SRM 53-10-8.SDR 02FDEA00581Loop · out of positionLOWER AFT BODY HEAT WARNING LIGHT CAME ON IN CLIMB. RAN LOWER AFT HEAT CHECKLIST. AFTER TURNING OFF NR 3 BLEED, LOWER AFT BODY HEAT LIGHT WENT OUT. TESTED SYSTEM, TEST OK. RETURNED TO MEM. FOUND ONE LOOP TOUCHING STRUCTURE. REPOSITIONED LOOP. RAN ENGINESDR 02FDEA00556Warning System · false activationON T/O ROLL, FIRE BELL SOUNDED WITH NO OTHER FIRE INDICATIONS. BELL WOULD NOT SILENCE WITH APU BELL CUTOUT BUTTON, BELL SILENCED WITH GLARESHIELD BELL SHUTOFF BUTTON, ABORTED AT 110 KTS. PERFORMED FIRE TEST ON BOTH LOOPS & APU ALL NORMAL NO ABNORMAL ENGINE ISDR 02FDEA00548Warning System · malfunctionedLEFT GEAR DOOR LIGHT REMAINED ILLUMINATED ON TAKEOFF. LIGHT STAYED ON AFTER CYCLING GEAR IAW RED TABS. OPERATED LEFT LANDING GEAR DOOR SEVERAL TIMES. DOOR INDICATION OPS GOOD AT THIS TIME.SDR 02FDEA00549Switch · lack of lubeLEFT MAIN GEAR DOOR INDICATED UNSAFE WHEN GEAR WAS LOWERED. CYCLED GEAR AND DOOR LIGHT WENT OUT PER NORMAL OPS. CLEANED AND LUBED LEFT MAIN LANDING GEAR DOOR SWITCH CHECKED ADJUSTMENT AND TEST PER MM. OPERATED DOORS SEVERAL TIMES AND OPS CHECKED GOOD.SDR 02FDEA00566Skin · chafedSKIN IS CHAFED AT BS 475, 2 INCHES ABOVE STR 21R. REMOVED AND REPLACED SKIN PER SRM 53-30-3.SDR 02FDEA00546Proximity Switch · malfunctionedON TAKEOFF RED LEFT GEAR LIGHT ON FWD INSTRUMENT PANEL REMAINS ILLUMINATED WITH GEAR HANDLE UP. CYCLED GEAR AS PER QRH AND REMAINED ILLUMINATED WITH GEAR HANDLE UP. REMOVED AND REPLACED LT MAIN GEAR UPLOCK PROX SWITCH PER 727 M/M 32-61-081-4. OPS CHECKED SESDR 02FDEA00547Csd · overheatedNR 3 CSD OVERHEATED DURING CLIMBOUT, 121C WITH NR 1 CSD AT 115C AND NR 2 CSD DISCONNECTED. ELECTED TO RTB AND NOT REDUCE TO ONE GEN OPERATIONS.SDR 02FDEA00545Csd · failedREPEAT WRITE-UP, DURING CLIMBOUT NR 2 CSD OVERHEATED TO 125C WITH NR 1 & 3 CSD'S IN LIMITS AT 110C & 118C IAW QRH. DISCONNECTED NR 2 GEN FOR 3 MIN COOLING. AFTER 2 MIN NR 3 CSD OVERHEATED TO 121C WITH NR 1 CSD 115C IAW QRH. DISCONNECTED NR 3 GEN AND RETURNSDR 02FDEA00568Stringer Clip · crackedCRACK STRINGER CLIP AT BS 700, STR 2 L. *S/D* REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 02FDEA00638Spar · crackedRIGHT REAR SPAR CHORD CRACKED APPROX BS 200.SDR 02FDEA00543Solenoid · faultyAFTER LIFTOFF LANDING GEAR HANDLE WOULD NOT RAISE ABOVE THE OFF POSITION. CREW WENT THROUGH APPROPRIATE RED TABS. COULD NOT FIX PROBLEM. RETURNED TO DEPARTURE AIRPORT. REPLACED L/G CONTL LEVER LOCK SOLENOID PER 727 MM 32-31-016-4. CYCLED GEAR SEVERAL TIMESDR 02FDEA00532Panel · missingON POST FLIGHT INSPECTION FOUND SLIDE PANEL ON RIGHT SIDE OF VERTICAL STAB MISSING. FOUND HINGE ASSY TORN & BROKEN. REMOVED REMAINDER OF HINGE ASSY. ALSO NOTED FORWARD SLIDER TRACK HAS SECTION TORN OUT AND AFT TRACK WAS BENT. NOTED AFT HONEY COMB PANEL A DSDR 02FDEA00514Engine · malfunctionedNR 2 ENGINE LOST OIL QUANTITY AND PRESSURE SHORTLY AFTER TAKEOFF, WITH CORRESPONDING LOW OIL PRESSURE/FILTER BYPASS LIGHT ON IN FRONT PANEL. SHUTDOWN ENGINE IAW CHECKLIST AND RETURNED FOR UNEVENTFUL LANDING. REPLACED NR 2 ENGINE. OPS AND LEAK CHECK OK.SDR 02FDEA00515Adc · failedCAPTAINS AIRSPEED AND ALTIMETER AND VERTICAL SPEED INDICATOR FAILED ON ROTATION WITH WINDSHEAR WARNINGS. REPLACED CADC IAW MM. OPS CHECK GOOD. CAT STATUS DOWNGRADED TO CHK II, CHK II. OVERALL CAT STATUS IS NOT II.SDR 02FDEA00507Stringer · corrodedCORROSION SKIN BULGE AT BS 1075, STRINGER R28. REMOVED AND REPLACED STRINGER PER SRM 53-10-1, 53-10-3.SDR 02FDEA00504Overheat Loop · out of positionON 2ND FLIGHT APPROACHING DESCENT INTO KMEM, LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED QRH AND ISOLATED RIGHT PACK AND RIGHT BLEED (NR 3) ALONE W/ THE CARGO HEAT OUTFLOW. FINDING SAME AS REPEAT WRITE-UP. SYSTEM TEST GOOD, ALL C/BS CHECK GOOD. BEGAN TSDR 02FDEA00505Warning Horn · activatedON INITIAL CLIMBOUT FROM COS THE ALTITUDE WARNING HORN CAME ON PASSING APPROX 12,500 FT MSL. A CHECK OF THE CABIN PRESSURE GAUGE SHOWED CABIN ALTITUDE IN EXCESS OF 10,000 FT MSL WITH THE CABIN STILL CLIMBING. DESCENDED BACK TO 10,000 FT MSL AND RAN THE PROCSDR 02FDEA00501Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON 30 MIN INTO FLIGHT. WHILE RUNNING THE QRH AND WITH BOTH PACKS NR 1 AND NR 3 BLEEDS ON, THROTTLE WAS MOVED TO IDLE. OVERHEAT LIGHT THEN EXTINGUISHED. REPEAT WRITEUP. RETURNED TO NORMAL CONFIGURATION WITH NO REPEAT OCCUR
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