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 CALA9701589Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER CHORD AT STA 344 FROM LBL 0 TO LBL 20. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701588Support · corrodedINSPECTION FOUND CABIN FLOORBEAM SUPPORT UPPER CHORD CORRODED AT STA 328, LBL 45.5 TO BL 0. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-2. A T-CAP AND SPACERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-1.SDR CALA9701587Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED IN AFT BAGGAGE COMPARTMENT AT STA 1180, STRINGER 23L. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW SRM 51-10-1.SDR CALA9701586Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WINGTIP RIB AT WS 795. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9701585Skin · dentedINSPECTION FOUND RT WING LEADING EDGE DENTED ABOVE NR 4 LEADING EDGE FLAP ACTUATOR. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, AND 51-40-1.SDR CALA9701584Battery Pack · dischargedINSPECTION FOUND THE RT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR DL72S980579Spar · crackedCRACKED IN AFT SPAR RAIL 56 FROM I/B END NR 2 MIDFLAP. REPAIRED PER BOEING M/M 57-52-0 PAGE 807.SDR DL72S972250Light · inoperativeDURING SVC CHK AD9 FOUND L1 AND L2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSYS. OPS NML.SDR DL72S972249Rib · crackedFOUND DURING D-2 LETTER CHECK - VERTICAL FIN RIB CRACKED AT RIB TO STRINGER ATTACH BOLT FIN STA 133.8 R/H SIDE 5TH \ATRINGER UP FROM BOTTOM REPAIRED PER M/M 55-30-0SDR DL72S972241Multiplier · inoperativeFL_330 LOSS PRESSURE,DESCEND TO 10,000 _REPLACED FLOW MULTIPLIERSDR DL72S972599Rib · crackedRW INTERNAL HYDRO-PRESSED RIB TO STRINGER STA 686.50 STRINGER 2ND FRAME AFT IS CRACKED. STOPED DRILLED PER MM 57-13-00 FIG 801. REMOVED FUEL PROBE DRILLED NEW REPAIR DOUBLER PER MM 53-13 AND INSTALLED.SDR DL72S972598Stringer · crackedFOUND AT HMV REF OPN 8602 HFEC INSP OUTER WING UPPER STRINGER TO PILE CRACK IND W5 546 RT WING 2ND STRINGER AFT OF AFT VENT BOX. STOP DRILLED PER MM 57-13-0 DRILLED NEW REPAIR MM 57-1 3-0 FIG 802, INSTALL PER MM 57-13-0 FIG 802.SDR DL72S972388Skin · wornTHE NR 5 L/E SLAT EXTERNAL SKIN WORN AND CRACKED WHERE FENCE ATTACHES. BEGAN FABRICATED DOUBLER PER MM 57-54-0 FIG 8B, DRILLED DOUBLER PER MM 57-54-0 FIG 813, ROUTED OUT CRACKED AREA PER MM 57-54-0 FIG 813. DYE CHECK PER PS 900-6-3, SHOWS NO FURTHER DAMAGE. SDR DL72S972387Skin · wornTHE NR 4 L/E SLAT EXTERNAL SKIN AND ATTACHMENT HOLES WORN WHERE FENCE FAIRING ATTACHES. BEGAN REPAIR PER MM 57-40-0 PG 817, FABRICATED REPAIR PER MM 57-40-0 PG 817. COMPLETED INSTALL OF DOUBLER PER 57-54-0 PG 817.SDR DL72S972321Floorbeam · corrodedSTA 344 FLOORBEAM CORRODED LEFT TO RIGHT SIDES. REPAIRED PER SRM 51-10-8 FIG 11.SDR DL72S972272Floorbeam · corrodedCABIN FLOOR BEAM CORRODED STA. 380 LBL14 TO RBL60. REPAIRED PER SRM 53-10-1 FIG. 4.SDR DL72S972251Stringer · crackedHFEC INSP OUTER WING UPPER STRINGER TO RIB CRACK INCL W 5.629.0 LT SIDE 2ND STRINGER AFT OF AFT VENT BOX. STOP DRILLED CRACK AND BEGAN TO DRILL UP ALL ANGLES PER M/M 57-13-0 FIG 802. COMPLETED DRILLING UP REPAIR ANGLES PER M/M 57-13-0 FIG 802. TRIMMED, TREASDR DL72S972242Web · crackedA 1.5 INCH CRACK UPPER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER LT CUTOUT 1303 WEB. A 1 INCH CRACK UPPER LT CUTOUT 1303 WEB. INSTALLED PERM REPAIRS PER SRM 53-10-4 FIG 17 FOR ALL 4 CRACKSDR DL72S972240Rib · crackedNR 2 SLAT RIB OUTBD OF ANTI-ICE DUCT CRACKED. REPAIR PER M/M 57-54-00.SDR DL72S972239Skin · crackedA .75 INCH CRACK IN OUTER SKIN OF DOGHOUSE FAIRING LT SIDE BELOW PANEL 9523. REPAIRED PER M/M 54-30-0.SDR DL72L972235Power Supply · inoperativeEMERGENCY FLOOR ESCAPE PATH LIGHT FROM SEAT 27 AFT INOP. - REPLACED BATTERY PACK POWER SUPPLY M9027-OPSSDR DL72S972229Line · failedHYD LINE TO NR 5 SPOILER CRACKED. CRACK IS OUTBD OF T-FITTING AND BENDS. LOST B-SYSTEM HYD FLUID. EMERGENCY EQUIPMENT CALLED OUT.SDR DL72L972224Hose · rupturedA-SYS HYD LOST QTY AND PRESS AFTER GEAR AND FLAP EXTENSION B-SYS OK. FOUND PRESS HOSE AT LT GEAR DOOR ACT LEAKING. REPLACED HOSE, REPLACED ENG 1 AND 2 CASE DRAIN FILTERS. RAN ENGINES, PUMPS CK NORMAL.SDR DL72S972297Stringer · crackedSTRINGER 11 AT WS 601.5 CRACKED (MARKED). CUT OUT ACCESS FOR REPAIR PER MM 57-13-0 FIG 803 STARTED REPAIR PER MM 57-13-0 FIG 804. OK TO INSTALL REPAIR. BEGAN INSTALLING REPAIR ANGLES. COMPLETED INSTALLATION OF REPAIR ANGLES PER M/M 57-13-0, FIG 804. INSTASDR DL72S972282Stringer · crackedSTRINGER NR 10 CRACKED AT WS 656.5. REPAIRED PER M/M 57-13-0 FIG 802.SDR 97ZZZX4772Bearing · failedFAN BALL BEARING STARTING TO COME APART. PARTIAL FAILURE OF BEARING. 712.42 HOURS SINCE NEW PART INSTALLED.SDR DL72S972210Casting · crackedNR 13 SPOILER ACT I/B AND O/B ATTACH CASTINGS ARE BROKEN. REPLACED PER M/M 57-42-0.SDR DL72S972209Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK POWER SUPPLY WILL NOT CHARGE. REPLACED BATTERY PACK.SDR DL72S972531Doudler · crackedREPAIR DOUBLER CRACKED ON LOWER AFT CHORD ANGLE 37 FROM I/B END OF FLAP. DAMAGE REPAIRED PER M/M 57-52-0 PAGE 807, ON SHOP ORDER 331063.SDR DL72S972516Flap · damagedAFT LWR CHORD IS CRACKED AT I/B AFT FLAP TRACK CUT OUT, TWO PLACES. ALSO, AFT LOWER CHORD ANGLE IS CRACKED 57 FROM I/B END. BOTH REPAIRS PER M/M 57-52-0 FIG 807.SDR DL72S972343Stringer · damagedTRANS FROM SMS PERMANENT REPAIR STR 18A DAMAGE IN NORMAL FLANGE PER SRM 53-12-0. CORRECTION CONTINUED ON NR 1160 CORRECTION. REMOVED TIME LIMITED REPAIR. FABRICATED REPAIR DOUBLER AND STARTED PER MM 53-12-0. OK TO TREAT AND PAINT. RSDR DL72S972270Frame · crackedFRAME AT STA 910/913 CRACKED IN RT WHEEL WELL. REPAIRED PER MM53-11-0 PG 814.SDR DL72S972204Battery Pack · dischargedMSU - CK OP OF ALL EMER LIGHTS. FOUND LT OVERWING EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS NML.SDR DL72S972349Floorbeam · wornCABIN FLOORBEAM UPPER CAP IS WORN THIN AT FLOOR PNL SCREW HOLE FS 344 RBL 12 TO LBL 45. BLENDED AREAS FOR FURTHER EVALUATION. FOUND BEAM OUT OF LIMITS PER 53-10-1 FIG 4. REMOVED T-CAP FROM RBL 60 TO LBL 60. STARTED DRILLING NEW T-CAP PER SRM 53-10-8. INSSDR DL72S972348Frame · crackedFRAME CRACKED NR 2 INLET S-DUCT HOUSING FRAME CRACKED ON LT SIDE FS 1233 AT INTERSECTION WITH HORSE COLLAR. REMOVED DAMAGE AND FABRICATED DOUBLERS PER SRM 51-400-3, INSTALLED DOUBLERS PER SRM 51-40-3.SDR DL72S972483Skin · crackedVERTICAL STAB SKIN CRACKED. DRILLED REPAIR DOUBLER PER SRM 55-30-3, CUTOUT DAMAGE PER SRM 55-30-3. VERIFIED CRACK REMOVAL AND INSTALLED REPAIR DOUBLER PER SRM 55-30-3.SDR DL72S972482Skin · crackedVERTICAL STAB SKIN CRACKED. CUT OUT CRACK PER SRM 55-30-3 AND VERIFIED CRACK REMOVAL. FABRICATED REPAIR AND INSTALLED DOUBLER/REPAIR.SDR DL72S972262Web · crackedWEB - CRACKED VETICAL STAB INTERIOR FS 1303 WEB CRACKED AT STRINGER CUTOUT, RH SIDE FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17BEGAN INSTALLING DOUBLER PER SRM 53-10-4 FIG 17.STOP DRILLEDCRACK AND DYE CHECKED PER SRM 53-10-4. COMPLETED INSTASDR DL72S972261Web · crackedWEB - CRACKED VERT STAB INTERIOR FS1303 WEB CRACKED A T LOWER LH CORNER FABRICATED REPAIR DOUBLER AND DRILLED PE R SRM 53-10-4 FIG 17DYE CHECKED AND STOP DRILLED CRACK PER SRM 53-10-4. OK TO INSTALL REPAIR. INSTALLED REPAIR PER SRM 53-10-4 FIG 17SDR DL72S972206Bulkhead Beam · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX 1 LONG AND IS LOCATED AT APPROX WL237 IN THE INBD RADIUS OF THE AFT CHORD. REPAIRED PER ERA 330932-14.SDR DL72S972175Plate · wornLEFT FWD SVC DOOR GUST LOCK BROKEN. REPLACED UPPER DOOR ARM GUIDE PLATE. DOOR AND GUST LOCK OPERATION NOW NORMAL.SDR DL72L972164Megaphone · inopON PREDEPARTURE CK, FOUND F/C MEGAPHONE INOP. REPLACED F/C MEGAPHONE.SDR DL72S972346Skin · crackedSKIN IS CRACKED AT RIVET ON THE LT SIDE OF S1 STA 1090. INSP OF SKIN 2 EA CRACKS LT AND RT FIRST FAST, EACH SIDE OF S1 STA 1090. FABRICATED REPAIR DOUBLER AS PER SRM 53-30-3 PAGE 15B. OK TO INSTALL. INSTALLED DOUBLER PER SRM 53-30-3, TREAT PAINT PER SRM 5SDR DL72S972345Rib · crackedNR 6 SLAT HAS A CRACKED RIB ON INSIDE RADIUS, MARKED. DYE PENETRANT INSPECTED CRACK PER PS 900-6-3 NR 1, STOP DRILLED CRACK AND FABRICATED DOUBLER PER MM 57-40-0 FIG 814. OK TO INSTALL DOUBLER. INSTALLED DOUBLER ON NR 6 SLAT JUST O/B OF ANTI-ICE DUCT.SDR DL72S972344Frame · crackedNR 2 SLAT RACK FRAME CRACKED SECOND FROM RT END. REMOVED DAMAGE, FABRICATED DOUBLER PER MM 57-54-0 PG 818. INSTALLED DOUBLER PER MM 57-54-0 PG 818.SDR DL72S972160Skin · cracked.5 INCH CRACK IN LOWER SKIN OF LT ELEVATOR 5 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3.SDR DL72S972157Stringer · crackedVERT FIN STR 9L IS CRACKED AT FIN STA 133.800. REPAIR PER MM 55-30-0.SDR DL72S972156Stringer · crackedVERT FIN STR 9L CRACKED AT FIN STA 157.200. REPAIR PER MM 55-30-0.SDR DL72S972155Web · cracked.0625 INCH CRACK AT RT VERT TORQUE BOX WEB LWR LIGHTING HOLE AT STA 1223 RT. REPAIR PER MM 53-11-0.SDR DL72S972154Skin · cracked.5 INCH CRACK IN LOWER SKIN OF LEFT ELEVATOR 5 IN FROM I/B EDGE. REPAIR PER SRM 55-20-3.
Back to Boeing 727-232