Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72L972153Angle · crackedFROM MV1C1, .25 INCH VISIBLE CRACK KEEL BEAM VERTICAL ANGLE INBD OF APU LOAD CONTROL VALVE. REPAIRED PER SRM 53-10-9.SDR DL72L972151Support · crackedFROM MV1C, NR 7 SLAT ACTUATOR O/B SUPPORT STRUCTURE CRACKED. REPAIR PER M/M 57-42-0.SDR DL72S972347Skin · looseRIGHT O/B AILERON LOOSE C-MAX RIVETS ON OUTER SKIN SEVERAL PLACES, MARKED W/ RED CRAYON AND NUMBERS. FABRICATED DOUBLER PER SRM 57-50-5 FIG 3, INSTALLED SKIN SPLICE PER SRM 57-50-5 FIG 3. OK TO INSTALL SKIN SPLICE. REMOVED AND INSTALLED ON RC 654.SDR DL72S972148Light · inoperativeEMERGENCY LIGHT ABOVE L2 DOOR INOP. REPLACED LIGHT ASSY.SDR DL72L972189Frame · corrodedFUSELAGE C3 DOOR SURROUND FS 1142.7 FRAME STRG 28R. REPAIR FOR CORRODED SKIN ATTACH FLANGE. C3 AFT DOOR JAMB FRAME (FS 1142.7) WAS FOUND CORRODED AT STRG 28R. THE LOWER FLANGE OF THE FRAME SKIN ATTACH ANGLE WAS TRIMMED OFF. ANGLE REPAIR INSTALLED PER ER/A SDR DL72L972152Skin · crackedFROM MV1C1, .5 INCH CRACK IN VERTICAL SKIN AT UPPER RIVET ROW OF LT TORQUE BOX AT STA 1223. REPAIR PER M/M 53-11-0.SDR DL72K972146Skin · crackedFOUND ON B2 LETTER CK, .75 INCH CRACK AT NR 2 ENGINE INLET, OUTER SKIN 2ND RIB FROM L/E 2 O'CLOCK POS. REPAIRED PER MM 54-30-1.SDR DL72K972145Rib · crackedFOUND ON B2 LETTER CK, NR 5 SLAT INBD AND O/B ACT ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-54-0.SDR CALA9701502Power Supply · inoperativeINSPECTION FOUND LEFT OVERWING EXIT AFT LIGHT INOPERATIVE. THE LEFT OVERWING EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLACED. OPERATION OF THE LIGHT CHECKED GOOD.SDR DL72L972180Skin · corrodedFUSELAGE SKIN FS 480-500, STRG 28L, SKIN CUT OUT DUE TO CORROSION. REPAIRED PER ER/A 362981-14.SDR DL72L972166Charger · inoperativeEMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER.SDR DL72K972143Hyd Line · leakingAFTER TAKEOFF 'B' SYSTEM HYDRAULIC PRESSURE AND QTY WENT TO ZERO. HYDRAULIC SYSTEM LEAK OR LOSS AND B SYSTEM LEAK OR LOSS FOLLOW UP PROCEDURES ACCOMPLISHED. MAINTENANCE FOUND OUTBOARD B SYSTEM PUMP CASE DRAIN AND PRESSURE LINES CHAFFED AND LEAKING. REPLACEDSDR DL72K972138Battery Pack · dischargedON LAYOVER, FOUND RT OVERWING FWD EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CKS GOOD.SDR DL72S972133Skin · holeHOLE IN LT L/E SKIN, 34 INCH FROM BOTTOM. INSTALLED REPAIR DOUBLER PER SRM 55-40-3 FIG. 1.SDR DL72S972132Skin · holeHOLE IN LEFT L/E SKIN ON LOWER RUDDER. REPAIRED PER SRM 55-40-3.SDR DL72S972131Skin · gougedSKIN GOUGED AT LOWER END OF LOWER RUDDER. INSTALLED DOUBLER PER SRM 55-40-3, FIG 1.SDR DL72S972130Exhaust Pipe · crackedWHILE PERFORMING A POST-REMOVAL INSPECTION OF A GTCP85-98CK APU EXHAUST PIPE (3850089-1), A 10 INCH CIRCUMFERENTIAL CRACK WAS NOTED ON THE PLENUM MOUNTING FLANGE. CAUSE FOR CRACK IS UNKNOWN. EXHAUST PIPE WAS MODIFIED BY ALLIED SIGNALTO SATISFY REQUIREMENTS OSDR DL72S972245Angle · crackedTHE LOWER AFT CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION AT HMV VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY STOP DRILLING CRACK AND INSTALLING A DOUBLER.SDR DL72S972126Bulb · failed1R DOOR EXT EMER LIGHT AND C2 AFT LIGHT INOP. REPLACED BULBS.SDR DL72S972172Rib · crackedDURING SHOP VISIT, THE IB AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED PER 727 MM 57-52-0 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.SDR DL72S972124Hinge · crackedFOUND ON D2 LETTER CHECK, .5 INCH CRACK AT NR 3 L/E FLAP OUTBD HINGE. REPAIRED PER ERA 363018-14 CODE 4-57-54.SDR DL72S972120Bulb · failedAFT MOST RED BULB INOP ON FLOOR PROX LIGHT STRIP. REPLACED BULB SOCKET.SDR DL72S972099Fitting · wornRT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807, IPC REF 65-26763-10 ITEM 350.SDR DL72S972098Fitting · wornLT MLG DOOR FWD ATTACH FITTING WORN. REPAIRED PER SRM 57-43-0 PG 806 AND 807 IPC LOC 32-10-00-10 ITEM 345.SDR CALA9701556Skin · puncturedINSPECTION FOUND A HOLE IN LT SIDE OF LOWER RUDDER TRAILING EDGE. THE AREA WAS ROUTED OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR DL72S972091Battery Pack · dischargedON S/C, FOUND LT AND RT FWD DOOR EXTEROIR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS NORMAL.SDR DL72L972100Light · inoperativeOVERHEAD EMERGENCY LIGHT ABOVE AISLE AT SEAT ROW 15 INOP. REPLACED LIGHT ASSY.SDR CALA9701555Intercostal · crackedINSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL BEAM AT STA 760, BL 0. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9701554Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BEAM AT STA 848, BL 0, AT BOTH LT AND RT SIDES. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9701553Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BEAM AT STA 720F AND 740 AREA, BL 0. THE TOP CAP WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR DL72S972081Fuel Control · failedAPPROX 40 MINS INTO FLIGHT AT FL330 THE NR 1 ENG INVOLUNTARILY WENT TO FULL POWER. THE THROTTLE DID NOT MOVE. PHYSICAL MOVEMENT OF THE THROTTLE PRODUCED NO ENGINE RESPONSE. PARAMETERS AT SHUTDOWN AS FOLLOWS OIL PRESSURE POSITIVE 45 EPR 2.4 N1-102 EGT-600C SDR DL72S972080Oven · failedFWD GALLEY OVEN FIRE IN FLT AFTER DEPARTURE. PERFORMED SMOKE/ID, RMVAL AND CLEAN UP CHECKLIST. RETURNED TO LAND AT PHX. REMOVED OVEN, INSPECTED WIRING AND COMPARTMENT, ALL CKD OK. REPLACED OVEN AS PRECAUTIONARY.SDR DL72K972083Skin · crackedFOUND DURING B-2 LETTER CHECK, 1 INCH CRACK S-DUCT HOUSING 10 FT AFT NR 2 ENG INLET BELOW ACCESS PANEL. REPAIRED PER M/M 54-30-0.SDR DL72K972082Skin · crackedFOUND DURING B-2 LETTER CHECK, 3 EA .75 INCH CRACKS IN OUTER SKIN OF NR 2 ENG INLET AT 3 O'CLOCK POSITION. REPAIRED PER M/M 54-30-0.SDR CALA9701558Rib · crackedINSPECTION FOUND CRACKS BETWEEN FASTENERS IN THREE LOCATIONS OF LT INBOARD MIDFLAP CAST RIBS. THE CRACKS WERE 1 TO 2 INCHES LONG. THE CRACKS WERE LOCATED AT 4TH RIB FROM INBOARD END, 5TH RIB FROM INBOARD END, AND AT INBOARD SIDE OF CENTER IDLER TRACK. THE MSDR CALA9701557Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT WING OUTBOARD MIDFLAP INBOARD MOST RIB AT AFT END IN LOWER RADIUS. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9701552Skin · crackedINSPECTION FOUND L-2 DOOR UPPER FORWARD CORNER OF EXTERIOR SKIN JUST BELOW GATE BENT WITH A 1.25 CRACKED. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 52-00-3.SDR DL72S972079Actuator · failedSYS-A HYDRAULIC QTY DECREASED TO ZERO IN FLT. FOUND NR 3L SLAT ACTUATOR FAILED IN RETRACT POSITION. SEALS BLOWN AT ACTUATOR ROD.SDR DL72S972077Strap · crackedTHE REINFORCEMENT STRAP OF THE FS 761 LT FRAME HAD PILOT HOLES DOUBLE DRILLED WITH EXISTING FASTENER HOLES AT THE 3RD AND 4TH FASTENER LOCATION BELOW THE FLOOR LINE. ADDITIONALLY, THE FRAME ITSELF HAS A CRACK MEASURING APPROX 2.5 LONG. AREA WAS REPAIRED PER SDR DL72S972073Chord · crackedFOUND ON F-2 LETTER CK, LT ATTACH CHORD CRACKED .75 INCH AT VERTICAL STAB S-7L. REPAIRED PER MM 55-30-0.SDR DL72S972072Web · crackedFOUND ON F2 LETTER CK, .75 INCH CRACK LOWER RT CORNER OF WEB STA 1303 ABOVE NR 2 ENGINE S-DUCT. REPAIRED PER SRM 53-10-4.SDR DL72L972075Chord · corrodedCORROSION FOUND ON O/B FLANGE OF NOSE WHEEL WELL SIDE PANEL T-CHORD RT WALKWAY BEAM AFT OF STA 312 AND 344. CLEANED CORROSION WITHIN LIMITS PER SRM 53-10-4 FIG 7. TREATED AND PAINTED REWORKED AREAS.SDR DL72L972058Fitting · crackedNR 7 SLAT ACT OUTBD SUPPORT FITTING CRACKED. REPAIRED PER M/M 57-42-0 PG 812.SDR CALA9701559Wire · brokenTHE AFT GALLEY AREA CEILING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND WIRES TO EXIT LIGHT BROKEN. THE WIRES WERE REPAIRED AND OPERATION OF THE EXIT LIGHT CHECKED GOOD.SDR DL72S972186Stringer · crackedSTRINGER TO RIB CRACK LEFT WING STA 686.5 AT STR 12. REPAIRED PER M/M57-13-0 FIG 804.SDR DL72L972076Rib · crackedA .25 INCH CRACK IN NR 4 SLAT I/B ACTUATOR ATTACH NOSE RIB. REPAIRED PER MM 57-40-0.SDR CALA9701436Light · inoperativeAFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOP. REPLACED LIGHT ASSEMBLY.SDR DL72S972056Stringer · crackedHFEC INSPECTION PER OPN NO 8602 AS SHOWS CRACK ON STRINGER TO RIB AT STA 686.5 5-10. PERFORMED DYE CHECK TO IDENTIFY CRACK. NO STOP DRILL HOLE REQUIRED. DISCONNECTED FUEL DUMP LINE AT STA 686.5 - 700 FOR ACCESS TO REPAIR. DRILLED UP REPAIR DOUBLERS PER MM SDR DL72L972116Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER I/B SIDE OF THE SECOND FROM THE I/B HINGE FITTING. THE CRACK IS APPROXIMATELY .25 LONG. THIS CRACK LENGTH IS WITHIN THE .250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED UNSDR DL72S972114Strap · double drillTHE REINFORCEMENT STRAP OF THE FS 761 LT FRAME HAD PILOT HOLES DOUBLE DRILLED WITH EXISTING FASTENER HOLES AT THE THIRD AND FOURTH FASTENER LOCATION BELOW THE FLOOR LINE. ADDITIONALLY, THE FRAME ITSELF HAD A CRACK MEASURING APPROXIMATELY 2.5 LONG AT THE FLOOR
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