Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 00FDEA00425Rib · crackedDURING ROUTINE INSPECTION, NR 6 LEADING EDGE SLAT WAS FOUND CRACKED AT INBD ACTUATOR ATTACH RIB. R&R PER IAW SRM 57-50-3.SDR 00FDEA00424Rib · crackedDURING ROUTINE INSPECTION, NR 4 LEADING EDGE SLAT WAS FOUND CRACKED AT OTBD ACTUATOR ATTACH RIB. R&R IAW SRM 57-50-3.SDR 00FDEA00423Rib · crackedDURING ROUTINE INSPECTION, NR 6 LEADING EDGE SLAT WAS FOUND CRACKED AT THE OTBD ACTUATOR ATTACH RIB. R&R PER IAW SRM 57-50-3.SDR 00FDEA00422Seat Track · corrodedDURING ROUTINE INSPECTION, MAIN CABIN SEAT TRACK AT LBL 48 WAS FOUND CORRODED OUT OF LIMITS FROM BS 760-848. R&R PER IAW SRM 53-10-5, 51-30-2.SDR 00FDEA00421Case · crackedDURING ROUTINE INSPECTION, THE NR 3 ENGINE INLET GUIDE VANE CASE WAS FOUND CRACKED. R&R NR 3 ENGINE IAW FEDEX WORK CARD 70T0001-03.SDR 00FDEA00420Drain Line · crackedDURING ROUTINE INSPECTION, NR 3 ENGINE PS 4 DRAIN BOSS FOUND CRACKED. R&R NR 3 ENGINE PER IAW FEDEX WORK CARD 70T0001-03SDR 00FDEA00410Bracket · crackedNOSE LANDING GEAR DOWNLOCK ACTUATOR SUPPORT BRACKET FITTING CRACKED. INSPECTION NOTE: MEASURED CRACK TO BE APPROX 1 IN. FROM RT UPPER MOUNT HOLE PROGRESSING THRU HOLE DOWNWARD. INSTALLED NEW BRACKET ASSY.SDR 00FDEA00409Floorbeam · corrodedCORROSION BS 480 FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES AT RBL 11 & LBL 28, LOWER SURFACE OF CHORD, WL 208. R&R PER FEDEX SRM 51-10-6, 53-10-1.SDR 00FDEA00408Seat Track · corrodedNR 446 CORROSION ON LONGITUDINAL BEAM AND SEAT TRACK AT BS 846 TO BS 760, WL 208, RBL 45. ** S/D ** R&R CORROSION PER FEDEX SRM 51-30-2.SDR 00FDEA00407Skin · gougedGOUGE IN EXTERIOR FUSELAGE SKIN BS 691 JUST BELOW STR 25 RT. R&R PER FEDEX SRM 53-30-3 FIG 1.SDR 00FDEA00404Engine · failedNR 1 ENG - FLAMES AND METAL PARTS REPORTED BY ACFT BEHIND, ON T/O AND TOWER. NR 1 ENG TEMP 610 ON T/O ROLL. ALL OTHER IND NORMAL. *S/D* REMOVED AND REPLACED NR 1 ENGINE PER WORK CARDS 70T0001-01, AND 70T0301-01.SDR 00FDEA00395Switch · malfunctionedUPON DESCENT LANDING GEAR LOWERED BELOW 250 KNOTS. WHEN GEAR HANDLE RAISED, NOSE GEAR CAME UP BUT MAIN GEAR WOULD NOT COME UP AND LOCK. RED MAIN GEAR DOOR LIGHTS REMAINED ON AND DOOR LIGHTS ON S/O PANEL REMAINED ON. CYCLED GEAR 1 TIME BUT DID NOT FIX IT. LSDR 00FDEA00390Detector · chafedON CLIMB, LWR AFT BODY OVERHEAT LIGHT FLASH INTERMITTENT. FOUND AFT BODY DETECTOR LOOP IN AFT AIRSTAIRS CHAFED THROUGH. *S/D* REMOVED AND REPLACED ELEMENT PER B727 MM 26-14-1.SDR 00FDEA00385Skin · gougedGOUGE IN FUSELAGE EXTERIOR SKIN BS 480, BETWEEN STR 2 AND 23 RT. R&R PER FEDEX SRM 53-30-3.SDR 00FDEA00389Skin · corrodedCORROSION BS 720E, PRESSURE NUT PLATE IS CORRODED. STR 19 RT EXTERNAL SKIN. R&R PER FEDEX SRM 53-30-3 FIG 5.SDR 00FDEA00384Floorbeam · corrodedNR 456 CORROSION ON FLOORBEAM BS 680, WL 208, BL0 - LBL 25. ** S/D ** R&R UPPER FLANGE PER FEDEX SRM 53-10-8 FIG 3.SDR 00FDEA00388Floorbeam · corrodedNR 402 CORROSION AROUND NUT CLIP HOLES LOWER CHORD BS 1130 FLOORBEAM LBL 1 - LBL 38, WL 200. ** S/D ** R&R CORROSION PER IAW FEDEX EA 7-5310-52109 & FEDEX MM 51-20-151.SDR 00FDEA00355Warning Light · illuminatedLOWER AFT BODY HEAT LIGHT ILLUM IN FLT. UTILIZED RED TAB PROC. LIGHT REMAINED ILLUM. *S/D* REPLACED CONNECTOR PER 727-200 MM 20-62-14. REMOVED AND REPLACED PANELING PER 727-200 MM 26-14-1. NO FURTHER DEFECTS NOTED. OK FOR SERVICE.SDR 00FDEA00350Switch · inoperativeNR 2 ENG LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUM. REMOVED AND REPLACED MAIN OIL STRAINER PER MM 72-61-0. REMOVED AND REPLACED NR 2 ENGINE LOW PRESSURE SWITCH PER 79-33-001. REMOVED AND REPLACED OIL FILTER BYPASS SWITCH PER 79-34-002-2. OPS CK NORMAL.SDR 00FDEA00329Clamp · looseDURING CLIMB AT 1400 FT, ENG 1 STRUT OVERHEAT LIGHT ILLUM. ACCOMPLISH ON RED TAB PROC. SECURED LOOSE CLAMP AT FWD DUCT OF NR 1 ENG PLYON PRECOOLER. RAN ENG, OP CK OK PER MM 26-14-001-2.SDR 00FDEA00304Access Door · missingHYDRAULIC ACCESS DOOR MISSING. *S/D* INSTALLED HYD DOOR PER STANDARD MAINTENANCE PRACTICES.SDR AALA20000711Skin · corrodedTUL - FOUR EACH FASTENER HEADS DISHED ON FUSELAGE BETWEEN STA 1150 AND 1166. STR 25L TO STR 27L. REMOVED CORRODED SHEAR TIES AND REPLACED WITH NEW. CUT OUT CORRODED SKIN AND REMOVED CORROSION ON STR 27L. INSTALLED STR 27 STRAP REPAIR PER ESO 11097 DATED 4-1SDR 00FDEA00299Warning Light · illuminatedHDG COMPARATOR LIGHT REPEATEDLY ILLUM. *S/D* REPLACED SPLICES AS PER MM 20-30-12, REPAIRED WIRES AS PER SMP & REPLACED NR 1 & 2 COMPASS RACKS & DIRECTIAL GYROS AS PER MM 34-21-071-4.SDR 00FDEA00298Amplifier · inoperativeDURING CLIMBOUT INOP HEADING FLAGS WERE OBSERVED ON CAPT RMI & FOS HSI. HDG INSTRUMENT COMPARATOR LIGHT ALSO ILLUM. REMOVED AND REPLACED NR 1 COMPASS AMP RACK AS PER SMP AND NR 1 DG AS PER MM 34-21-071-4. PERFORMED OPER TEST OK.SDR 00FDEA00291Angle · corrodedFWD BAG BIN CENTER FLOOR PANEL RT SUPPORT CORRODED BS 643. R&R FAB IAW SRM 51-40-4.SDR 00FDEA00290Panel · corrodedTRANSITION PANEL CORRODED ABOVE STR 26 RT AT BS 1030. REMOVED DAMAGE. FAB REPAIR IAW SRM 51-40-2. INSTALL IAW SRM 5 1-30-2.SDR 00FDEA00289Floor Support · corrodedHEAVY CORROSION ON FLOOR SUPPORT IN FWD BAG BIN BS 643, LBL 10 & LBL 14. CUT OUT DAMAGED AREA. FAB & INSTALL REPAI R ANGLES IAW SRM 51-40-4.SDR 00FDEA00287Fitting · crackedLT MLG DOOR RIB FITTING CRACKED ABOVE THE ACTUATOR POINT. R&R LT MAIN LG DOOR IAW MM 32-12-1.SDR 00FDEA00286Keelbeam · corrodedMODERATE TO HEAVY CORROSION INSIDE OF DELTA KEEL BEAM ON ATTACH FITTINGS, LT & RT CHORDS, AND LOWER WEB. REMOVED FAB & INSTALL NEW ATTACH ANGLEA AT STA 750-840 IAW SRM 51-10-1 & SRM 51-30-2.SDR 00FDEA00285Skin · crackedFUSELAGE SKIN CRACKED AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT.SDR 00FDEA00284Cap · crackedNR 5 LEADING EDGE SLAT I/B END CRACKED. REMOVED AND REPLACED I/B END CAP ON NR 5 SLAT IAW SRM 51-30-2.SDR 00FDEA00283Web · crackedAIRSTAIR AREA, RT SIDE WEB CRACKED AT LIGHTENING HOLE AT BS 1240. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-2 & SRM 51-30-2.SDR 00FDEA00282Web · crackedAIRSTAIR AREA, LT SIDE WEB CRACKED AT LIGHTENING HOLE AT BS 1260. STOP DRILLED CRACK, FABRICATED AND INSTALL REPAIR IAW SRM 51-40-2 & 51-30-2.SDR AALA20000710Stringer · corrodedTUL - CORROSION ON STRINGER 30 STA 1070 - STA 1090. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG1. (X)SDR 00FDEA00254Warning Light · activatedENG 3 STRUT OVERHEAT LIGHT CAME ON. REMOVED ACCESS PNLS 5501 & 5502 INSP NR 3 PYLON OH DETECTOR ELEMENT LOOP AND ASSOCIATED DUCTING. NO DISCREPANCIES NOTED OR EVIDENCE OF AIR LEAKS. SYS CK NORM IAW MM 26-14-000-5. REINSTALLED ACCESS PNL. AC OK TO CONTINUESDR AALA20000050Line · leakingPLS - FLT 625 - DURING DESCENT INTO PLS, SYSTEM 'B' HYDRAULIC FAILURE. CREW DECLARED EMERGENCY AND LANDED PLS WITHOUT INCIDENT. REPLACED PRESSURE LINE ON NR 2 PUMP. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED WITH TEMPORARY HOSE. (M)SDR 00FDEA00139Door · crackedA/C FAIL TO PRESSURIZE, AFT GEAR RETRACTION EQUIP ACCESS DOOR LIGHT CAME ON. AVIONIC ACCESS DOOR CRACKED. CLOSED AND OPS CK PER MM 52-40-011-4, CK NORMAL.SDR 00FDEA00094Warning Light · illuminatedNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. POWER REDUCED PER RED TABS AND LIGHT EXTINGUISHED. REPLACED ALL THE CLAMPS AND RETORQUED SWIVEL GLAND, RAN APU AND ENGINE. LEAK CHECK OK PER BAC MM 36-00-001. OK TO CONTINUE.SDR 00FDEA00047Connector · contaminatedON GEAR RETRACT, LV LATCH FAIL TO RELEASE. COMPLETED THE RED TABS STEP. PRECAUTIONARY CLEAN CONNECTOR AT LG ASSY UNIT, LG SYS TEST OK.SDR 99FDEA00507Controller · malfunctionedCLIMB THRU FLT LEVEL 180 CABIN PRESS START TO DECREASE AT 1200 RPM (4.8 PSID & DECREASING). PERFORMED CABIN PRES CKLIST, NO HELP. *S/D* ACCOMPLISH EXCESS CABIN PRESS LEAKAGE CONDITION, REF B727 MM 05-51-101-2, TEST OK. NO DEFECTS NOTED AT THIS TIME, A/C OKSDR 99FDEA00501Window · cracked99-284 - R2 WINDOW STARTED ARCING. SHUT R2 OFF COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 2 SLIDING WINDOW. ADJUSTED PER MM 56-12-011-5.SDR 99FDEA00499Switch · failedRT MAIN DOOR LIGHT STAY ON WITH GEAR HANDLE IN OFF POS. REMOVED AND REPLACED RT MAIN GEAR DOOR LOCK SWITCH PLUG (D752) PER STAND MAINT PRACT AND REF WIRING DIAGRAM MANUAL 32-62-01. OPER CK WARN SWITCH REF MM 32-62-011-5. OPER CK NORM. OK FOR SERVICE.SDR AALA991837Relay · failedTPA - FLT 811 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SWITCH IN ARM POSITION EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT RELAY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR 99FDEA00492Accessory Unit · malfunctionedWHEN LANDING GEAR EXTENDED, BOTH GROUND AND RED IND LIGHTS WERE PRESENT ON FRONT IND. REMOVED AND REPLACED LANDING GEAR ASSY UNIT AND CLEANED ELECTRICAL CONNECTORS ON THE RACK WITH CONTACT CLEANER MM 32-01-122, TEST OK ON GROUND.SDR 99FDEA00490Accessory Unit · inopDURING GEAR EXT, 3 GRN LIGHT+3 RED GEAR LIGHT+TAILSKID LIGHT WERE ILLUMINATED. REMOVED AND REPLACED L/G ACCESSORY UNIT PER MM 32-09-122 & TEST OK.SDR 99FDEA00487Unknown · odorDURING T/O A BURNING RUBBER ODOR AND SMOKY HAZE BEGAN TO FILL THE COCKPIT AND CARGO AREA. RED TABS FOLLOWED AND A/C INITIATED RETURN TO BASE. INSP'D FOLLOWING AREAS FOR PROBLEMS, BOTH E & E BAYS, A/C PACK BAYS, AFT AIRSTAIRS, GEARWELLS, SNAKE PIT IN FWD BELLSDR 99FDEA00486Door · malfunctionedRED DOOR LIGHTS AND S/O AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUM'D AFTER GEAR RETRACTION W/HANDLE UP. CREW FELT/HEARD NOSE GEAR DOOR NOT FULLY CLOSED. ACCOMPLISHED RED TABS. AFTER GEAR WAS RECYCLED CREW FELT/HEARD SUBSTANTIALLY LESS NOISE AIRSPEED LIMITED SDR 99FDEA00485Valve · failedDURING GEAR RETRACT RED DOORS LIGHT AND AMBER GEAR DOOR LIGHT (2ND OFF PNL) REMAIN ILLUM. RECYCLED GEAR. *S/D* REMOVED AND REPLACED NOSE SCHRADER VALVE AND RESERVICE PER MM 12-15-025-2. CHECKED 6 HRS LATER, NO LEAKS AND PRESSURE THE SAME.SDR 99FDEA00479Window · crackedNR 42 F/O'S R1 WINDOW CRACKED IN FLIGHT. *S/D* REMOVED AND REPLACED NR 1 F/O'S WINDOW IAW FEDEX MM 56-11-011-4. WINDOW HEAT CKS GOOD IAW FEDEX MM 30-41-002-5 STEP 3.SDR 99FDEA00451Controller · inopAUTO PRESSURIZATION FAILURE IN FLT. COULD NOT CONTROL CABIN ALT IN ANY PRESSURIZATION MODE. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM 21-31-010-4. OPER CHECK NORM.
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