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 DL72K960334Blkhd Stiffener · crackedFOUND ON MV1 1183 BULKHEAD VERTICAL STIFFENER CRACKED 1 INCH AT LOWER END, BL 8L WL 185. REPAIR: REPAIRED PER M/M 55-11-0, PAR 9.SDR DL72S960326Retract Mech · out of rigAFTER TAKEOFF WITH GEAR HANDLE IN OFF POS, FELT AND HEARD LOUD THUMP 4 OR 5 TIMES AT APPROX 2 MIN INTERVALS. PROBLEM WENT AWAY WITH HANDLE IN UP POSITION. RIGGED AND ADJUSTED NOSE GEAR DOORS PER MM, OPERATION NORMAL.SDR DL72S960312Retract Mech · lack of lubeRT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF. INSPECTED, LUBRICATED RT MAIN GEAR. JACKED A/C CYCLED GEAR SEVERAL TIMES, OPERATION NORMAL.SDR DL72L960313Light · inoperativeOVERHEAD EMERGENCY LIGHT AT BOTTOM OF AIRSTAIRS IS INOP. REPLACED LIGHT ASSEMBLY.SDR DL72S960311Identifier · inoperativeDURING LAYOVER CHECK, AFT CABIN DOOR EMERGENCY EXIT IDENTIFIER INOP ON TEST. REPLACED AFT CABIN DOOR IDENTIFIER AND REPAIRED BROKEN WIRE AT D9069P.SDR DL72S960310Battery Pack · inoperativeDURING LAYOVER CHECK, FOUND FWD AND AFT BULLNOSE EMERGENCY LIGHTS WOULD NOT TEST. REPLACED BATTERY PACK AT FWD 1088 AND REPLACED BATTERY PACK AT AFT 1089, NOW CHECKS OK.SDR DL72S960298Web · crackFOUND DURING E-1 LETTER CHECK, .25 INCH CRACK LWR TORQUE BOX VERTICAL WEB LIGHTENING HOLE FWD OF BS 1243 LEFT SIDE. REPAIRED PER M/M 53-11-0 PAR 15.SDR DL72S960297Skin · tornFOUND DURING E-1 LETTER CHECK, .75 INCH TEAR RIGHT ELEVATOR LWR SKIN 15 INCHES AFT OF HINGE CENTERLINE AND 6 FEET O/B OF I/B END. REPAIRED PER SRM 55-20-3 FIG 4.SDR DL72S960290Skin · crackedA .375 INCH CRACK AT F/O EYEBROW WINDOW LOWER FWD CORNER CUTOUT. FOUND DURING F-2 LTR CHECK TPAMM. REPAIRED PER SRM 53-30-3.SDR DL72S960291Sensor · dirtyON GEAR RETRACTION, RED RT GEAR AND GREEN RT GEAR LIGHTS REMAINED ON. COMPLETED LDG GEAR RETRACTION MALFUNCTION CHECK LIST, BOTH LIGHTS REMAINED ON. ABOUT 40 SECONDS LATER, BOTH LIGHTS OUT. CHECKED AND CLEANED RIGHT MAIN LANDING GEAR DOWNLOCK, SENSOR OPERATSDR DL72S960283Angle · crackedFOUND ON B1 LETTER CHECK, NR 7 SPOILER ATTACH CASTING CRACKED AT LOWER WING ATTACH. REPAIRED PER MM 57-20-22.SDR DL72S960282Angle · crackedFOUND ON B-1 LETTER CHECK, TWO L/E SPAR STIFFENERS CRACKED .50 INCH, ONE AT NR 3 SLAT INBD TRACK, THE OTHER AT NR 2 SLAT OUTBD TRACK. REPLACED ANGLES PER MM 57-20-21.SDR DL72S960281Stiffener · crackedFOUND ON B1 LETTER CHECK, 2 INCH CRACK IN WING L/E SPAR STIFFENER AT NR 6 SLAT INBD TRACK. REPLACED STIFFENER PER MM 57-20-21.SDR DL72S960274Door Actuator · iced upON DEPARTURE, RT MAIN GEAR WOULD NOT RETRACT, TRANSIT LIGHT ON AND SECOND OFFICER'S PANEL NEVER ILLUMINATED. REMOVED ICE BUILD-UP ON RT GEAR DOOR ACTUATOR, LUBED GEAR AND DOORS, PERFORMED GEAR SWING AND OPS NORMAL.SDR DL72S960300Blkhd Channel · wornAT MID VISIT 2, FOUND VERT SUPPORT CHANNEL WORN AT TOP STA 720D ABOVE STR 26 LT. REMOVED DAMAGED SECTION PER SRM 53-10-9 FIG 9. DRILLED NEW DOUBLER AND INSTALLED PER SRM 53-10-9 FIG 9.SDR DL72S960289Skin · gougedDURING INSPECTION OF C-3 CARGO DOOR, A SMALL GOUGE WAS FOUND IN THE EXTERIOR SKIN. THE DAMAGE WAS REPAIRED PER SRM 52-00-3.SDR DL72S960273Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 700 TO 720F FROM STR 26R TO 27R. THE SKIN PANEL WILL BE REPLACED IN ACCORDANCE WITH B727 SRM 51-10-1.SDR DL72S960266Slat · damagedON CREW WALK-AROUND, NR 2 LEADING EDGE SLAT DAMAGE. ANTI-ICE TELESCOPING DUCT DAMAGED SLAT AND WING. REPLACED SLAT, FERRIED TO ATL FOR FURTHER MAINTENANCE.SDR DL72S960264Panel · wornHMV, LEADING EDGE O/B END WORN, NR 4 TRAILING EDGE FLAP. REPLACED WORN SEAL ON TRAILING EDGE PANEL, CUT OUT DAMAGE AND REPAIRED PER M/M 57-52-0 FIG 803.SDR DL72S961589Transverse Beam · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACSDR DL72S960255Wire · brokenON CLIMBOUT, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON, WING ANTI-ICE NOT ON, BUT DUCT TEMP SHOWED 200 DEGREES. FOUND STRUT WING ANTI-ICE VALVE STUCK OPEN. REMOVED AND REPLACED RELAY R32 AND FOUND BROKEN WIRES IN CANNON PLUG ON STRUT VALVE. REMOVED AND REPLASDR DL72L960257Stringer · crackedSTRINGERS CRACKED 3RD BAY UP IN VERT STAB ON LT AND RT SIDE UPPER END AND 3RD BAY UP RT LOWER. FOUND DURING A-2 LTR CK TPAMM AND REPAIRED PER SRM 55-30-0.SDR DL72S960249Angle · crackedFOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 7 L/E SLAT LWR COVE SKIN ATTACH ANGLE BELOW I/B TRACK. REPAIRED PER M/M 57-54-0.SDR DL72S960248Bracket · crackedFOUND DURING C-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET AT I/B LWR END. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72S960247Bracket · crackedFOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BRACKET I/B LWR SIDE. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72S960243Light · inoperativeEMERGENCY EXIT LIGHT AT R1 AND R2 DOOR INOP. REPLACED EMERGENCY LIGHTS OVER R1 AND R2 DOORS AND OPERATION NORMAL.SDR DL72K960245Rib · crackedUPON INSPECTION FOR NR 1 LEADING EDGE SLAT, RIB NR 15 WAS FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S960265Floorbeam · corrodedFOUND ON MV-1 CHECK, CORROSION ON FLOORBEAM STA 344 RBL 45. REPAIRED PER SRM 53-10-8 FIG 10.SDR DL72S960242Battery · dischargedFWD OVERHEAD EMERGENCY LIGHT INOP IN COACH CABIN. REPLACED BATTERIES, CKS GOOD.SDR DL72S960236Fuel Pump · failedON TAKEOFF ROLL CVG AT 78 KTS, NR 2 ENGINE APPEARED TO FLAME, ALL ENGINE INST ROLLED BACK. REJECTED TAKEOFF AND RETURNED TO GATE. INSPECTED INTAKE AND EXHAUST, PULLED OIL FILTER, ALL CHECKS OK. FOUND NO FUEL FLOW TO ENGINE. REPLACED FUEL CONTROL AND FUEL PSDR DL72L960246Comb Chamber · failedON TAKEOFF, THE NR 1 ENGINE SHUTDOWN WITH FIRE WARNING IND FOLLOWING. AFTER A/C RETURNED, MAINTENANCE FOUND THE NR 1 ENGINE HAD A UNCONTAINED FAILURE. ALSO, AFTER FURTHER INSPECTION A/C SUBSTAINED MORE DAMAGE TO THE TAIL, FUSELAGE AND S-DUCT DUE TO PARTS COMSDR DL72L960238Prbc · failedON TAKEOFF, GOT COMPRESSOR STALL NR 2 ENGINE. INSPECTED INLET AND EXHAUST, ALL OK. RAN ENGINE TO TAKEOFF POWER, ALL CKS NORMAL, BUT ON DECEL GOT COMPRESSOR STALL AT 80 TO 85 N2. REPLACED PRBC, RAN ENGINE PER PFHB TEST-E AND ALL CKS GOOD.SDR DL72S960463Rib · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S960221Light · inoperativeEMERGENCY LIGHTS OVER DOOR INOP AT R1 AND R2. REPLACED LIGHT ASSYS.SDR DL72L960229Bracket · crackedNR 1 SLAT ACTUATOR I/B BRACKET BROKEN OUT AROUND FWD ATTACH BOLT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER M/M 57-20-21.SDR DL72S960219Skin · crackedNR 4 KRUEGER FLAP HAS TWO 1 INCH CRACKS AT O/B CUTOUT FOR LWR LIP ATTACH FITTING. REPAIRED PER SRM 57-50-3.SDR DL72S960218Skin · crackedLOWER L/E SKIN CRACKED AND WORN AT FENCE ATTACH HOLE. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 LE SLAT.SDR DL72S960217Skin · crackedOUTER SKIN CRACKED AT FENCE ATTACH HOLE AND GROOVED AT REMAINING ATTACH HOLES. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.SDR DL72S960216Rib · crackedRIB WAS FOUND TO BE CRACKED ON INSPECTION. RIB WAS REPAIRED PER M/M 57-54-00. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.SDR DL72S960233Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BELLY SKIN ABOVE THE RAM AIR INLET. THE DAMAGE CUTOUT MEASURES 12 INCHES FWD AND AFT BY 10 INCHES INBD AND OUTBD AT FS 720C. IN ACCORDANCE WITH 8110-3 DATED 1/26/96, AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLEDSDR DL72S960206Skin · crackedFOUND DURING A-2 LETTER CHECK, .75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LWR HINGE CUTOUT. REPAIRED PER ERA 303079-14 AND M/M 53-30-0.SDR DL72S960204Web · crackedFOUND ON A-2 LETTER CHECK, .375 INCH CRACK IN TORQUE BOX LIGHTENING HOLE AT STA 1303 RIGHT SIDE 48 SECTION. REPAIRED PER MM 53-11-0.SDR DL72S960202Deck · crackedDURING MIDVISIT, TWO 1 INCH CRACKS WERE FOUND IN THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK BETWEEN STATIONS 940 AND 950, BETWEEN LBL 50 AND 60. MODIFICATION INSTALLED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 727-53-0149, REVISION 4.SDR DL72S960198Angle · crackedFOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE, ADJACENT TO O/B TRACK. REPAIRED PER M/M 57-54-0.SDR DL72S960268Skin · dentedDURING INSPECTION, C-3 CARGO DOOR OUTER SKIN WAS FOUND WITH THREE DENTS BEYOND ALLOWBLE LIMITS. REPAIRED SKIN PER SRM 52-30-1 FIG 9.SDR DL72S960180odorON TAKEOFF, COCKPIT AND CABIN FILLED WITH SMOKE, DID NOT SMELL LIKE ELECTRICAL. FLIGHT RETURNED TO SEA. MAINT INSPECTED ENGINES INLETS AND EXHAUST APU AREA AND RAM AIR DOORS, NO DISCREPANCY FOUND. RAN APU WITH A/C PACKS AND ENGS WITH PACKS. SUSPECT ANTI-ICSDR DL72S960174Spar · crackedDURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A.SDR DL72S960178Cable · brokenLEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. REPLACED DOOR SLIDE PER M/M 25-60-15.SDR DL72S960177Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S960176Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.
Back to Boeing 727-232