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 CALA9901584Wire · chafedINSPECTION FOUND THE LT OVERWING EMERGENCY LIGHTS IN MID AND AFT POSITIONS INOPERATIVE. MAINTENANCE FOUND A CHAFED WIRE BEHIND WHEEL WELL FAIRING PANEL AREA. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.SDR CALA9901583Battery Pack · dischargedINSPECTION FOUND THE L-1 AND L-2 DOOR EXIT SIGNS INOPERATIVE. THE BATTERY PACK FOR EACH SIGN WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01.SDR DL72S992700Shear Clip · crackedTHE SHEAR CLIP FOR THE FS 1263 FRAME BETWEEN STRINGERS 13L AND 14L WAS FOUND WITH A 1 INCH CRACK IN THE SKIN FLANGE RADIUS. THE SKIN FLANGE WAS TRIMMED OFF TO REMOVE THE CRACK. THE SHEAR CLIP WAS RESTORED BY INSTALLING AN ALUMINUM REPAIR ANGLE PER ER/A 3689SDR DL72S992692Line · leakingDURING CLIMBOUT OF STL, A SYS QTY DROPPED TO 1.2 GAL AFTER GEAR RETRACTION. ONCE AT CRUISE ATL, A SYS QTY SLOWLY DROPPED TO .2 GAL. A SYS LOSS PROCEDURES WERE FOLLOWED. LANDING GEAR WAS LOWERED NORMALLY AND FLAPS WERE LOWERED BY ALT METHOD. LOW PRESS LIGHSDR DL72S992688Light · inoperativeFLIGHT DECK EMERGENCY PORTABLE EXIT IDENTIFIER LIGHT WOULD NOT TEST. REPLACED BATTERY PACK, OP CKS GOOD.SDR CALA9901581Light · inoperativeINSPECTION FOUND THE EMERGENCY EXIT LIGHT AT AFT ENTRY INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECKED IAW MM 33-50-01.SDR DL72S992808Bracket · crackedC2 DOOR (S/N 634) HAD 2 BRACKETS BROKEN, ROD BENT, WEB DAMAGED AT LIGHTNING HOLE. REPAIRED PER SRM 52-30-20, OPS CHECK GOOD.SDR DL72S992683Bracket · crackedNR 1 LEADING EDGE SLAT I/B AND O/B ACTUATOR MOUNT BRACKETS CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S992682Skin · crackedA .5 INCH CRACK AT FWD LWR SIDE OF NR 2 MIDFLAP AT I/B AFT FLAP ACTUATING ROD CUTOUT. REPAIRED PER MM 57-52-0 AND ERA 368899-14.SDR DL72S992680Beam · crackedC-2 DOOR HORIZONTAL BEAM WEB DAMAGED AT LIGHTNING HOLE AT DOOR HANDLE SNUBBER SRM 52-30-2D FIG 802D.SDR DL72S992679Stiffener · crackedVERTICAL SPAR STIFFENER CRACKED NR 7 SLAT O/B SIDE OF I/B TRACK. REPLACED SPAR STIFFENER PER MM 57-20-21.SDR DL72S992678Angle · crackedCOVE SKIN ANGLE CRACKED 15 INCHES O/B OF NR 7 SLAT ACTUATOR ROD. REPAIRED PER MM 57-54-0.SDR DL72L992813Track · corrodedDURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, (P/N 65-19269-18), CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND WEAR AT THE FWD ATTACH LUG. PART WAS REPAIRED PER ER/A 372298-14AD REVISION B.SDR DL72L992812Track · corrodedDURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY (P/N 65-19270-12) CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND WEAR WAS FOUND AT THE FWD ATTACH LUGS AND THE MLG DOOR HINGE FITTING ATTACH HOLES AND THE TOGGLE DETENT HOLE. SUBJECT PART WASDR DL72S992660Bulb · failedON SVC CHECK, FOUND RT R1 EMERGENCY LIGHT INOP. REPLACED BULB, OPS CK GOOD.SDR DL72K992664Skin · dentedTHE FUSELAGE SKIN WAS BADLY DAMAGED BY CONTACT WITH GROUND EQUIPMENT. THE SECTION OF SKIN BETWEEN FS 416 & FS 484 AND BELOW STRINGER 22R WAS CUTOUT. NEW SECTIONS OF SKIN WERE INSTALLED WITH AN EXTERNAL ALUMINUM SPLICE STRAP PER ER/A 368846-14AD, REV A.SDR DL72K992663Frame · crackedTHE FUSELAGE WAS BADLY DAMAGED BY GROUND EQUIPMENT RESULTING IN DENTING AND CRACKING OF THE FS 440 & FS 460 FRAMES BETWEEN STRINGERS 22R & 26R. THE DAMAGED SECTIONS OF FRAMES WERE CUT OUT AND NEW SECTIONS INSTALLED WITH NEW FORMED SHEET ALUMINUM SPLICES SDR DL72K992653Motor · failedAFTER T/O, O/B FLAPS FROZE AT 15 FOR A FEW SECONDS THEN WENT TO 5. O/B FLAPS DID NOT EXTEND FOR LANDING. PER PILOT REPORT AN EMERGENCY WAS DECLARED. FOUND O/B FLAP HYD DRIVE MOTOR AT FAULT. MOTOR AND CASE DRAIN CHECK VALVE WERE REPLACED PER M/M.SDR DL72S992665Frame · crackTHE WEB OF THE FS 560 C1 DOOR JAMB FRAME WAS FOUND WITH 2 SMALL CRACKS AT EXISTING FASTENER HOLES BELOW THE UPPER SILL. THE CRACKS WERE ROUTED OUT OF THE WEB AND A TITANIUM DOUBLER INSTALLED TO REPAIR THE DAMAGE AND ENABLE INSTALLATION UNDER THE EXISTING UPSDR DL72L992758Skin · gougedGOUGE FOUND IN THE SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. THE DAMAGE AREA IS LOCATED JUST BELOW STR 24R. DAMAGE IN SKIN, DOUBLER AND TRIPLER BUT NOT THE INTERNAL BEAR STRAP ER/A 333860-14 REV A.SDR GAIA99227Bulkhead · crackedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. TAIL SKID CAVITY BULKHEAD WEB AT STATION 1183 HAS CRACK ON LEFT SIDE 5 INCHES BELOW FLOOR. REMOVED EXISTING REPAIR AND INSPECTESDR GAIA99226Floorbeam · crackedFOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEABY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, BS 1183 BULKHEAD LEFT VERTICAL BEAM HAS CRACK AT LOWER END, LBL 8. PERFORMED NDT INSPECTION TO DETERMINE END OF CRACK, PER B727SDR GAIA99225Frame · corrodedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. NOSE SECTION INTERNAL CIRCUMFERENTIAL FRAME HAS CORROSION ON LEFT SIDE OF DOG HOUSE BELOW HORIZONTAL WALKWAY BEAM BS 303 AND STRSDR GAIA99224Vent Lines · chafedFOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FUEL VENT TUBING WAS FOUND TO BE CHAFING AT THE FOLLOWING WING STATIONS, LWS 656.5, LWS 546.5, LWS 519.0, RWS 601.5 AND RWS 546SDR GAIA99223Angle · crackedFOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. MAIN CABIN STRINGER 17L BODY STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME. ACCOMPLISHED REPAIR ON MAIN CABIN STRINGER SDR GAIA99222Stringer · corrodedFOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY (MIAMI) PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. CORROSION AT STRINGER 7R UPPER FLANGE, JUST FORWARD OF BS 1148. REMOVED CORRODED AREA AT STRINGER 7R UPPER FLANGE FORWASDR GAIA99221Seat Track · mismanufacturedFOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. SEAT TRACK AT LBL 24.75 TOO SHORT AT SPLICES FOR CARGO MOD BODY STATION 1050 TO 1070. REMOVED AND REPLACED SEAT TRACK AT LBL 2SDR GAIA99220Bear Strap · crackedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER BEAR STRAP HAS CRACK. STOP DRILLED CRACK AT GALLEY DOOR CUTOUT BEAR STRAP IAW B7SDR GAIA99219Floorbeam · corrodedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FORWARD GALLEY FLOORBEAM AT BODY STATION 380, RBL 14 TO RBL 64 IS CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMSDR GAIA99218Seat Track · mismanufacturedFOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 45.5 IS TOO SHORT FOR CARGO MOD AT SPLICE, BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 45.SDR GAIA99217Seat Track · mismanufacturedFOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT LBL 45.5 TOO SHORT FOR CARGO MOD BODY STATION 1110 TO 1130. REMOVED AND REPLACED SEAT TRACK AT LBL 45.5 FROM BS 1030SDR GAIA99216Floorbeam · corrodedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FLOORBEAM AT BODY STATION 400, RBL 12 CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMOVED DAMAGED AREAS PER SRM 5SDR GAIA99215Seat Track · mismanufacturedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KGA CERTIFICATE, SEAT TRACK AT RBL 45.5, BS 680 TO BS 720A HAS WRONG SPLICE FOR 9G BULKHEAD. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FROM STASDR GAIA99214Seat Track · mismanufacturedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 24.75 TOO SHORT FOR CARGO MOD BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 24.75 FROM BS SDR DL72S992634Power Supply · failedRT FWD EMERG EXIT HATCH EMERGENCY LT INOP. FOUND FUSE BROKEN OFF IN SOCKET OF PWR SUPPLY. REPLACED SAME.SDR DL72S992632Angle · crackedFOUND ON D1 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72L992782Rib · crackedAT HMV2 FOUND NR 3 SLAT RIBS CRACKED. REPAIR AT RIB MARKED NR 3, RIB MKD NR 10, RIB MKD NR 17. CORROSION - DYE CKD AS PER PS 900-6-3 AND NO CRACKS. FABRICATED DOUBLER PER MM 57-54-0 PG 807. INSTALLED DOUBLER PER SAME, DYE CHECKED RIB NR 17 PER PS 900-6-3 SDR DL72L992727Rib · crackAT HMV2, FOUND NR 4 SLAT RIB (MARKED) CRACKED. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. DYE CHECKED END OF CRACK PER FIG 504. CHEM TESTED PER PS 900-2-4-1 NR 2. REPAIRED RIB PER MM 57-54-0.SDR DL72L992671Rib · crackedAT HMV2, FOUND NR 8 SLAT RIB'S CRACKED, NR 4, 14 (MARKED). REMOVED I/B SLTRK AND STOP DRILLED CRACK PER MM 57-40-0 FIG 809, FABRICATED REPAIR PARTS PER MM 57-54-00 FIG 809.SDR DL72K992633Light · inoperativeAFT CARGO DOOR EMERG LIGHT INOP. REPLACED BATTERY AT RACK M957, CHECKS GOOD.SDR DL72L992783Skin · tornAT HMV2 ELEVATOR T/E CHIPPED/TORN LT ELEVATOR EXTREME O/B END. BUSHED AREA AND FOUND TO BE WITHIN LIMITS PER SRM 55-20-1 FIG 161, INSTALLED FASTENERS.SDR DL72L992670Skin · disbondedAT HMV2, FOUND RT ELEV T/E DISBONDED BETWEEN UPPER AND LWR SKIN SEVERAL AREA'S FROM I/B TO O/B AREA. REPAIRED PER MM 55-20-0 PG 801 NR 2.SDR DL72L992669Skin · delaminatedAT HMV2, FOUND LT ELEVATOR T/E DELAMINATED I/B AND O/B OF TAB. REPAIRED PER MM 55-20-0 PG 801 NR 2.SDR DL72L992668Skin · disbondedAT HMV2, FOUND RT ELEVATOR I/B TRAILING EDGE DISBONDED. REPAIRED PER MM 55-20-0 PG 801 NR 2.SDR DL72L992667Stringer · crackedAT HMV2, FOUND STRINGER 5R CRACKED AT RIB NR 9 VERT STAB INTERIOR. DYE CHECKED AND FOUND CRACK EXTENDS TO EDGE OF MATERIAL. CHEM TREATED PER PS 900-2-4-1 NR 2, FABRICATED REPAIR PER MM 55-30-0 PG 803, AND INSTALLED PER SAME.SDR DL72K992629Battery · dischargedEMERGENCY LIGHT AT COCKPIT DOOR INOP. REPLACED BATTERY, CKS OK.SDR DL72S992609Power Pack · leakingSYS A QTY RAPIDLY DECREASED ON GEAR RETRACTION. FOUND RT ELEV POWER PACK LEAKING. REPLACED RT ELEV POWER PACK.SDR DL72S992601Oven · contaminatedFORWARD GALLEY WORK LIGHT C/B POPPED. F/A REPORTED LIGHT PLASTIC SMELL. NO SMOKE NOTED. BREAKER WAS NOT RESET. ON CHECK, FOUND GALLEY WORK LIGHT C/B POPPED AND COLLARED BY PREVIOUS ENG ORDER. CHKD OPS OF OVENS, COFFEEMAKER. ALL ELEC OPERATIONS NORMAL. FOSDR DL72S992591Battery Pack · dischargedDURING L/O CHECK, FOUND SVL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTS AND PACKS, ALL CHECK OK.SDR DL72L992584Skin · corrodedCORROSION WAS FOUND IN THE STR 26R LAP JOINT BETWEEN FS 500 AND 520. THE DAMAGE WAS REPAIRED PER ERA 333773-14AD AT HMV.
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