Boeing 727-232

Service difficulty reports · 6,539

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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.

SDR DL72S990716Frame · crackedFOUND ON C1 LETTER CK, AFT RT ENTRY DOOR FRAME CRACKED. REPAIRED PER SRM 53-10-9.Mar 31, 1999 · N403DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9900347Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN FUSELAGE SKIN JUST UNDER FORWARD END OF NR 3 ENGINE PYLON. REPAIRED IAW SRM 53-30-3, FIGURE 3 SHEET 1.Mar 31, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990714Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN THREE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH ANDMar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990713Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 43 TOTAL CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANELMar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990712Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 71 TOTAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WIMar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990711Skin · crackedLFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN NEAR FS 486. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED A SINGLE CRACK AT FS 486. THE CRACK WAS ROUTED OUT AND REPAIRED PER B7Mar 30, 1999 · N528DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990688Angle · corrodedFOUND ON D2 LETTER CK, CORROSION ON ATTACH ANGLE FOR A/C DOOR 3448R. REPAIRED PER MM 53-30-1.Mar 29, 1999 · N538DA · Boeing 727232 · Air Conditioning DoorsSDR DL72S990675Battery Pack · dischargedFWD AISLE EMERGENCY LIGHT STAYED ON. REPLACED EMERGENCY LIGHT RACK AND BATTERY, OPS CK OK.Mar 28, 1999 · N409DA · Boeing 727232 · Emergency LightingSDR DL72S990671Wire · failedLT GENERATOR ON LANDING, LOUD SOUND OF GENERATOR FAILING. ELECTRICAL SMELL IN COCKPIT. DIFF FAULT LIGHT ON ANN PANEL. MTC FOUND BURNT WIRES GOING TO DISTRIBUTION 1 SECT X C/B C829. REPAIRED WIRING PER M/M.Mar 27, 1999 · N533DA · Boeing 727232 · Electrical Power System WiringSDR DL72L990701Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT FOR THE ENTIRE PANEL ANMar 27, 1999 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990672Line · looseNR 1 GEN ON MCO. ON T/O FROM FLL LOST NR 2 GEN, WAS ABLE TO GET NR 2 GEN BACK ON LINE BUT LOW PRESS LIGHT WAS FLICKERING AND OIL TEMP WAS HIGH. FOUND OIL LEAK AT COOLER, TIGHTENED LINE.Mar 26, 1999 · N540DA · Boeing 727232 · Engine Oil Storage (Airframe Furnished)SDR DL72S990667Clamp · brokenAFTER PUSHBACK, HEARD LOUD BANG AND EXPERIENCED SMOKE IN CABIN. FOUND CLAMP OFF DUCT IN AREA OF FLOW MULT REF IPC 21-10-0-4 ONLY AFFECTS AIR FROM APU. PUT APU AIR TO MCO AND PLACARD.Mar 26, 1999 · N531DA · Boeing 727232 · Pneumatic Distribution SystemSDR DL72K990668Skin · wornNR 3 MIDFLAP/UPPER SKIN WBL 70 TO 106, WEAR DAMAGE FOUND TO NR 3 MIDFLAP UPPER SKIN DUE TO INTERFERENCE WITH FOREFLAP. WEAR AREA IS APPROX 37.5 SPAN-WISE X 7.5 CHORD-WISE. INSTALLED INTERNAL TITANIUM DOUBLER FOR FLUSH REPAIR.Mar 26, 1999 · N491DA · Boeing 727232 · Trailing Edge FlapsSDR DL72K990666Skin · crackedINSPECTIONS PER SI 4-74176-12AD, RESULTED IN FINDING 15 CRACK INDICATIONS IN THE S4R LAP JOINT BETWEEN BS 681 AND BS 740. THE 15 CRACK INDICATIONS WERE LOCATED IN THREE DIFFERENT FRAME BAYS. REPAIRED PER ERA 332942-14AD.Mar 26, 1999 · N480DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990664Skin · crackedINSPECTION PER SI 4-74176-12AD, RESULTED IN 24 CRACK INDICATIONS FOUND IN THE S4R LAP JOINT BETWEEN BS 481 AND BS 681. THE 24 CRACK INDICATIONS WERE LOCATED IN SEVEN DIFFERENT FRAME BAYS. REPAIRED PER ERA 332941-14AD.Mar 26, 1999 · N480DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990663Skin · crackedDURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-74176-12AD SIX CRACK INDICATIONS WERE NOTED AT THE S4R LAP JOINT FROM BS 360 TO 480. THE SIX CRACKS WERE LOCATED IN THREE DIFFERENT FRAME BAYS. REPAIRED PER ERA 332940-14AD.Mar 26, 1999 · N480DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990662Skin · crackedDURING ACCOMPLISHMENT OF SI 4-74176-12AD, SEVERAL CRACK INDICATIONS WERE NOTED IN THE S4L LAP JOINT BETWEEN BS 360 AND 480. FOUR CRACKS WERE CONFIRMED, IN THREE DIFFERENT STRINGER BAYS. REPAIRED PER ERA 332943-14AD, REV A.Mar 26, 1999 · N480DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990703Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN TWO SEPARATE FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUT OUT AND REPAIREDMar 25, 1999 · N492DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990661Battery Pack · dischargedL2 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS GOOD.Mar 25, 1999 · N417DA · Boeing 727232 · Emergency LightingSDR CALA9900322Skin · crackedAN INSPECTION OF THE LOWER SKIN OUTER SURFACE ALONG THE LOWEST ROW AT STRINGER 4R LAP SPLICE FROM BS 681 TO BS 740 FOUND CRACKS IN THE ENTIRE LENGTH OF THE PANEL. THE CRACKS MEASURED FROM .0625 INCH TO .25 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5330-02785Mar 25, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990705Frame · crackedFOUND DURING MV2 CORROSION VISIT NRC 134, .375 INCH VISIBLE CRACK LT CUTOUT FRAME, AFT ENTRY DOORWAY AT SECOND FROM UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990631Web · crackedFOUND ON MV2 CK, .5 INCH CRACK IN STA 1303 WEB LT LOWER CORNER. REPAIRED PER SRM 53-10-4.Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990630Web · crackFOUND ON MV2 CK, .5 INCH CRACK STA 1303 WEB RT AT LOWER RT CORNER. REF NR 143. FOUND ON MV2 CK, .5 INCH CRACK STA 1303 WEB RT AT THE CUTOUT FOR THE STRINGER. REF NR 142. BOTH CRACKS REPAIRED WITH THE SAME DOUBLER PER SRM 53-10-4.Mar 23, 1999 · N532DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990628Rib · crackedFOUND ON E1 LETTER CK, NR 5 SLAT ACT I/B ATTACH RIB CRACKED. REPAIRED PER MM 57-54-0.Mar 23, 1999 · N533DA · Boeing 727232 · Leading Edge DevicesSDR DL72K990633Light · failedCOCKPIT OVER DOOR EMERGENCY LIGHT FAILED TO TEST. REPLACED, OPS NORMAL.Mar 23, 1999 · N415DA · Boeing 727232 · Emergency LightingSDR DL72S990722Stringer · crackedREPAIRED CRACK AT UPPER STRINGER TO RIB FASTENER HOLE AT RT WING STA 656.50 STR 14 PER M/M 57-13-0.Mar 22, 1999 · N532DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L990611Indicator · failedOUTBOARD T/E FLAPS DID NOT EXTEND WHEN FLAP LEVER MOVED FROM UP TO 2 DEG. RETURNED LEVER TO UP, RAN THE POM CK LIST. TRAILING EDGE FLAP ABNORMAL ALTERNATE/FLAP EXTENSION ON I/B FLAPS WORKED FINE. CHECKED CABLES AND PULLEYS, ALL CKS OK. REPLACED O/B FLAP POSMar 22, 1999 · N506DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72L990605Battery Pack · dischargedFWD AND REAR OVER AISLE EMERG EXIT LIGHTS FLICKER WHEN STANDBY PWR SELECTED. REPLACED 2 BATTERY PACKS, OPS NORMAL.Mar 22, 1999 · N513DA · Boeing 727232 · Emergency LightingSDR CALA9900305Skin · dentedINSPECTION FOUND RT WING NR 9 SPOILER DENTED ON LOWER END. THE NR 9 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.Mar 22, 1999 · N77780 · Boeing 727232 · SpoilersSDR CALA9900304Light · inoperativeINSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.Mar 22, 1999 · N77780 · Boeing 727232 · Emergency LightingSDR CALA9900303Panel · bentINSPECTION FOUND RT WING NR 8 SPOILER OUTBOARD AREA BENT UP. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-62-1.Mar 22, 1999 · N77780 · Boeing 727232 · SpoilersSDR DL72S990626Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTMar 20, 1999 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990624Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED Mar 20, 1999 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990623Skin · crackedCRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL Mar 20, 1999 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990621Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTMar 20, 1999 · N477DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990620Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUTOUT Mar 20, 1999 · N477DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990618Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED SEVERAL CRACKS IN SEPARATE FRAME BAYS ALONG THE PANEL LENGTH THE SKIN LAP SPLICE WMar 20, 1999 · N477DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990606Skin · corrodedTHE LOWER FUSELAGE SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND CORRODED BETWEEN FS 720 +17 AND FS 740 NEAR AN A/C DUCT CUTOUT. THE DAMAGED SECTION OF SKIN WAS CUT AWAY AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ERMar 19, 1999 · N484DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990595Power Supply · inoperativeON S/C FOUND E PATH LIGHTING AT SECTION 20 TO 26 INOP. FOUND BAD FUSE ON AFT PWR SUPPLY. REPLACED AFT PWR SUPPLY, OPS NORMAL NOW.Mar 19, 1999 · N519DA · Boeing 727232 · Emergency LightingSDR DL72S990594Fan · failedON TOP OF DESCENT, CREW AND PASSENGERS COMPLAINED OF AN ELECTRICAL SMELL IN CABIN WITH NO SIGN OF SMOKE. AFTER A SAFE LANDING AND NORMAL DEPLANING, CONTRACT MAINTENANCE FOUND GASPER FAN CAUSING SMELL. REPLACED FAN.Mar 19, 1999 · N545DA · Boeing 727232 · Air Distribution FanSDR DL72K990614Spar · misdrilledDURING SHOP VISIT AND ACCOMPLISHMENT OF EO 4-58705-3AD, MTC UNABLE TO INSTALL REQUIRED COLLAR FOR ONE OF THE UPPER SPAR-TO-UPPER SKIN ATTACH FASTENERS DUE TO PROXIMITY TO SPAR RADIUS. AUTHORIZED USE OF RADIUS BLOCK AND MINI NUT.Mar 19, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S990589Stringer · crackedVERT FIN STR 10L CRACKED AT STA 180.600. INSTALLED DOUBLER PER M/M 55-30-0.Mar 18, 1999 · N523DA · Boeing 727232 · Vertical StabilizerSDR DL72S990587Frame · crackedFOUND AT B-2 LETTER CK, .5 INCH CRACK AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER STOP CASTING. REPAIR PER SRM 53-10-9.Mar 18, 1999 · N523DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9900296Stiffener · corrodedINSPECTION FOUND STIFFENER CORRODED AT RT WING FRONT SPAR FS 249. THE CORRODED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-02, PAGE 4.Mar 18, 1999 · N77780 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9900295Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT BS 1164. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.Mar 18, 1999 · N77780 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9900294Bolts · corrodedINSPECTION FOUND VERTICAL STABILIZER TENSION TIE BOLTS (8) PITTED AND CORRODED. THE TENSION TIE BOLTS WERE REMOVED AND REPLACED IAW MM 55-30-51, PAGE 406-408.Mar 18, 1999 · N77780 · Boeing 727232 · Vertical StabilizerSDR CALA9900293Intercostal · corrodedINSPECTION FOUND LOWER FLANGE OF INTERCOSTAL CORRODED IN AFT CARGO AREA AT STA 1128-1148 OUTBOARD OF STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.Mar 18, 1999 · N77780 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9900292Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD SUPPORT BRACKET AT TOP AND BOTTOM OF NR 6 LEADING EDGE FLAP ACTUATOR. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.Mar 18, 1999 · N77780 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9900291Cowl · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 3 ENGINE NOSE COWL ACOUSTIC LINING WITH LINING ERODED IN SEVERAL AREAS. THE NR 3 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 54-00.Mar 18, 1999 · N77780 · Boeing 727232 · Engine Cowling SystemSDR CALA9900290Housing · corrodedINSPECTION FOUND HORIZONTAL STABILER LEFT AND RIGHT HINGE BUSHING HOUSINGS CORRODED. THE BUSHINGS AND BEARINGS WERE REMOVED AND REPLACED IAW ECRA 555C028 AND ECRA 5550-01033.Mar 18, 1999 · N77780 · Boeing 727232 · Horizontal Stabilizer Structure
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