Boeing 727-232

Service difficulty reports · 6,539

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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 DL72K000926Splice · corrodedAT HMV2, FOUND SPLICE STRAP CORRODED FS 970 - 990 STR 29R. REMOVED CORR PER SRM 51-10-6 & COMMON FASTENERS THRU SKIN FOR FURTHER EVAL, REMOVED RT SIDE OF REPAIR ANGLE, CLEANED/REMOVED ALL CORROSION PER SRM 51-10-6, WITHIN LIMITS PER 53-10-110, ROTO PEENED AREApr 17, 2000 · N529DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00257Channel · corrodedNR 829 CORROSION (C53-111-01-1) BETWEEN STRAP & FLOOR STRUCTURE AT BS 302, LBL 46, WL 207 AT MISSING NUT PLATE. ** S/D ** R&R PER FEDEX SRM 51-30-2.Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00262Stringer · corrodedNR 1071, CORROSION ON STRINGER 28 RT AT BS 524 - 528. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3.Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Longeron/StringerSDR 00FDEA00261Stringer · crackedVERTICAL STABILIZER STR 9 RT IS CRACKED WHERE IT ATTACHES TO RIB NR 7. *S/D* REMOVED AND REPLACED NEW STRINGER PER FEDEX SRM 55-30-04 PG 5.Apr 17, 2000 · N497FE · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR 00FDEA00260Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 328, LBL 2 - 20, WL 208. *S/D* REMOVED AND REPLACED REPAIR PER SRM 53-10-1, 53-10-8, 51-20-1.Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00259Skin · corrodedCORROSION ON INTERIOR SKIN OF FORWARD CARGO BAY AT BS 527, RBL 7, WL 147. *S/D* REPAIRED PER SRM 53-30-3 & FEDEX EA 7-5330-50044.Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 00FDEA00258Skin · crackedNR 271 CRACKS IN EXTERNAL SKIN AT STRINGERFASTENERS, BS 524-528, RBL 6, STR 28. ** S/D ** REPAIRED PER SRM 53-30-3 & FEDEX EA 7-5330-50044.Apr 17, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000740Bulkhead · crackedTHE LT AFT ENTRY DOOR FRAME ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK AT WL 276. THE CRACK IS TYPICAL OF AD 99-18-05 AND BAC S/B 727-53-0210. THE CRACK WAS ROUTED OUT OF THE FRAME AND REPAIRED WITH THE S/B 727-530- 0210 REPAIR/MOD KIT ON AApr 17, 2000 · N491DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S000733Valve · damagedAIR TURNBACK DUE TO NR 3 ENGINE START VALVE LIGHT ILLUMINATED DURING CLIMBOUT. FOUND STARTER VALVE AT FAULT. ADDITIONAL DAMAGE TO STARTER AND STARTER ADAPTOR. REPLACED STARTER VALVE STARTER AND STARTER GEARBOX ADAPTER.Apr 16, 2000 · N515DA · Boeing 727232 · Engine Start Valves/ControlsSDR DL72S000732Flow Divider · overheatedCREW REPORTS SOMKE IN CABIN. REPLACED FLOW MULTIPIER.Apr 16, 2000 · N540DA · Boeing 727232 · Air Distribution SystemSDR DL72K000728Frame · crackedA PREVIOUS REPAIR WAS FOUND ON THE FS 910 FRAME AT STR 18A ON THE RIGHT SIDE OF THE AIRCRAFT. THE REPAIR WAS REMOVED, INSPECTED AND A NEW REPAIR INSTALLED PER ERA 334253-14. THE DAMAGE WAS FOUND AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K000727Frame · corrodedCORROSION WAS FOUND ON THE FS 1142.7 CARGO DOOR OPENING FRAME ON THE FORWARD SIDE OF THE WEB. THE CORROSION WAS BLENDED AND A DOUBLER INSTALLED PER ERA 334273-14 AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L000726Skin · crackedA CRACK WAS FOUND IN THE STR 4L LAP JOINT BETWEEN FS 420 AND FS 440. THE CRACK WAS CUT OUT AND REPAIRED PER ERA 334325-14AD AT HMV.Apr 16, 2000 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000725Frame · corrodedTHE 1166 FRAME AND BONDED DOUBLER WERE FOUND WITH CORROSION DAMAGE BETWEEN STRINGER 30 AND STRINGER 29R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 334245-14AD AT MV-2.Apr 16, 2000 · N510DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L000724Stiffener · crackedTHREE CRACKS WERE FOUND IN THE LBL 26.83 VERTICAL STIFFENER ON THE FORWARD SIDE OF THE FS 1183 BULKHEAD. THE CRACKS WERE FOUND BETWEEN WL 243 AND WL 263. EACH CRACK WAS APPROX 2 INCHES LONG. THE STIFFENER WAS REPAIRED PER ERA 334327-14AD AND S/B 727-53-0192Apr 16, 2000 · N509DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K000723Skin · gougedA GOUGE WAS FOUND IN THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-2 DOOR AT FS 990. THE DAMAGE WAS LOCATED APPROX 1 INCH ABOVE STRINGER 24R. THE SKIN, DOUBLER AND TRIPLER WERE TRIMMED, INSPECTED AND TREATED PER ERA 334268-14. THE DAMAGE WAS FOUND AT HMV.Apr 16, 2000 · N410DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000822Stringer · crackedLT WING TANK TOP SKIN STR 9 CRACKED AT RIB STA 629. REPAIRED PER 57-13-0 PAGE 801 FIG 802.Apr 13, 2000 · N509DA · Boeing 727232 · Wing, Longeron/StringerSDR 00FDEA00237Intercostal · crackedNR 1088, REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 358, LBL 67, WL 216. ** S/D ** R&R PART PER IAW FEDEX SRM 51-40-2, 51-30-2, 51-10-2 & 51-30-6.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00240Stringer Clip · crackedCRACKED STRINGER CLIP 10R, BL 700. *S/D* REMOVED AND REPLACED STR.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00239Stringer Clip · crackedBS 660, STR 7R STRINGER CLIP CRACKED. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-2.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00238Strap · crackedTIE STRAP AT BS 328, RBL 45, WL 200 IS CRACKED AT PREVIOUS REPAIR. *S/D* REPAIR STRAP PER FEDEX SRM 53-10-8 FIG 6.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00234Strap · corrodedCORROSION (C53-224-04) ON STABILIZER STRAP BS 1070, LBL 25, WL 200. *S/D* REMOVED, FAB & INSTALL PER FEDEX SRM 53-10-8.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00243Strap · crackedTIE STRAP AT BS 344, RBL 25, WL 200 IS CRACKED AT PREVIOUS REPAIR. *S/D* STOP DRILL CRACK PER FEDEX SRM 51-10-1, 53-10-8 FIG 6.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00241Seat Track · corrodedCORROSION (C53-224-04) ON SEAT TRACK FLANGE BS 1070, RBL 45, WL 208. *S/D* REMOVED AND REPLACED, ALODINED, PRIMED PER FEDEX SRM 53-10-1 FIG 3, 51-30-5 FIG 1 & 2, 51-10-2.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S000702Skin · crackedLOWER EXT SKIN CRACKED AT RIB ATTACH FASTENER HOLES 8.5 INCHES FROM I/B END. REPAIRED PER MM 57-54-0 FIG 801.Apr 12, 2000 · N546DA · Boeing 727232 · Leading Edge DevicesSDR 00FDEA00242Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE AND NUT PLATE HOLE BS 312, LBL 19, WL 208.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00233Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 620, LBL 45 TO RBL 25, WL 208.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00232Strap · crackedTIE STRAP AT BS 312, RBL 45, WL 200 IS CRACKED AT PREVIOUS REPAIR.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00231Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 700, STR 7L.Apr 12, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00222Floorbeam · corrodedCORROSION ON LWR CHORD FLOORBEAM BS 1130, RBL 16-34 AROUND FASTENER HOLES. ** S/D ** R&R CORROSION FND TO BE OUT OF LIMITS PER ER 005113.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00223Stringer Clip · corrodedNR 0847, CORROSION ON STRINGER CLIP BS 1148, STR 22L, LBL 49, WL 170. ** S/D ** R&R CORROSION FND OUT OF LIMITS IAW SRM 53-10-1. R&R STR CLIP PER IAW SRM 51-30-5, 51-30-2.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000764Harness · damagedFOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA OF NR 3 ENG. REPLACED CABLES FROM SPLICES IN RT 48 SECTION TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727Apr 11, 2000 · N535DA · Boeing 727232 · AC Generation SystemSDR DL72L000739Skin · damagedC/W SRM 53-11-0 PERMANENT REPAIR STA 910 LT SIDE. REMOVED 2 HYDRAULIC LINES FOR ACCESS. REMOVED ANGLE PER SRM 53-10-4D STEP 1. REMOVED FASTENERS, CLIP AND FILLER PER SRM 53-10-4D. BEGAN DRILLING PARTS FOR BS 910 PER SRM 53-10-4D. FINISHED DRILLING REPAIR Apr 11, 2000 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000693Rib · crackedRIB NUMBER 7 CRACKED MANUFACTURED DOUBLER. INSTALLED DOUBLER PER 57-54-0 FIG 814 MM.Apr 11, 2000 · N490DA · Boeing 727232 · Leading Edge DevicesSDR 00FDEA00230Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 680, BL 0 TO LBL 45, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8 FIG 3.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00229Skin · misdrilledSKIN REPAIR BS 1123, STRINGER 9L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Plate/SkinSDR 00FDEA00227Floorbeam · corrodedCORROSION (C53-224-04) AROUND FASTENER HOLE BS 950F, LBL 11, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8 FIG 8 & FEDEX SRM 53-10-2 FIG 7 SHEET 2, 24.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00228Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE BS 620, LBL 45 TO RBL 25, WL 208.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR 00FDEA00226Stringer Clip · crackedBS 560, STR 10R STRINGER CLIP IS CRACKED.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00225Stringer Clip · crackedBS 720B, STR 7R STRINGER CLIP CRACKED.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR 00FDEA00224Splice · corrodedCORROSION ON FRAME DOUBLER ABOVE STR 24R, BL 1070, RBL 45.Apr 11, 2000 · N497FE · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L000809Rib · crackedRIB CRACKED AT LWR RADIUS NR 5 SLAT TRACK SUPPORT BOX. REMOVED SLAT TRACK. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER PER MM 57-54-0 FIG 808. OK TO INSTALL DOUBLER AND FILLER. INSTALLED REPAIR PER MM 57-54-0 FIG 808 AND BEGAN INSTALLING SLAT TRACApr 10, 2000 · N509DA · Boeing 727232 · Leading Edge DevicesSDR DL72S000838Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 55 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPLACING A SECTION AND SPLICING PER MM 57-52-0, FIG 802.Apr 8, 2000 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000837Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 37 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPLACING A SECTION OF THE ANGLE AND SPLICING IT WITH A DOUBLER PER MM 57-52-0, FIG 802.Apr 8, 2000 · N516DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000676Pcu · malfunctionedRUDDER LOAD LIMITER FOLLOWING MEL PROCEDURES WHEN REENGAGED SYSTEM A RUDDER BEFORE FLAP EXTENSION RECEIVED UNCOMMANDED LOWER RUDDER YAW 1 INDICE RT SYS A RUDDER THEN TURNED OFF AGAIN. STBY ON AND LOWER RUDDER RETURNED TO NORMAL. CENTERED POSITION. LANDING MApr 8, 2000 · N519DA · Boeing 727232 · Rudder Control SystemSDR MZZA00007Toggle · crackedFLT 977 - AFTER TAKEOFF, INDICATION OF LEADING EDGE FLAPS AND SLATS EXTENDED INDICATED AT CONTROL PANEL AND GREEN LIGHT MAIN FLAPS OUTBOARD INDICATION STOPPED AT 4 DEGREES, INBOARD INDICATION STOPPED AT 2 DEGREES, AILERON L-1 DEGREE, RUDDER L-2.5 DEGREES TO GEApr 7, 2000 · N15790 · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72L000673Light · corrodedRIGHT FORWARD OVERWING EMERGENCY LIGHT IS INOP. T/S SYSTEM AND CLEANED CORROSION FROM LIGHT SOCKETS AND REPLACED BULBS. NOW CHECKS NORMALLY.Apr 7, 2000 · N512DA · Boeing 727232 · Emergency LightingSDR DL72S000672Acm · malfunctionedLEFT PACK ON DESCENT INCREASED TO 90 DEGREES AND SMOKE WAS EXHAUSTING BRIEFLY INTO THE CABIN WITH A SMELL. REDUCING MANUALLY TO 50 DEGREES STOPPED SMOKE. MTC ATL NOTIFIED IN FLIGHT. REMAINDER OF FLIGHT NORMAL. RAN LEFT PACK IN AUTO AND MANUAL THROUGH FULL Apr 7, 2000 · N532DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S000670Fitting · crackedLEFT I/B TENSION TIE FITTING CRACKED IN 48 SEC. REPLACED FITTING PER BAC DRAWING 65-17509 REV M. NRC 63 TPA F-2 LTR CHECK.Apr 7, 2000 · N416DA · Boeing 727232 · Empennage StructureSDR DL72K000668Door Frame · crackedTHE RT FRAME OF THE AFT ENTRY DOOR WAS FOUND CRACKED IN THE FORWARD FLANGE AT WL 276. THE BEAM WAS CUT AND A NEW SECTION SPLICED IN PER ERA 334236-14. THE DAMAGE WAS FOUND AT HMV.Apr 7, 2000 · N410DA · Boeing 727232 · Fuselage Miscellaneous Structure
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