Boeing 727-247

Service difficulty reports · 2,669

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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 = '727247'
  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 DL72W972457Baffle · crackedA .75 INCH CRACK NR 3 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACT AND .5 INCH CRACK NR 2 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACTUATOR. REPAIR PER MM 57-54-0.Nov 24, 1997 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W972384Light · inoperativeL1 EMERGENCY DOOR LIGHT INOP. REPLACED LIGHT ASSY.Nov 16, 1997 · N291WA · Boeing 727247 · Emergency LightingSDR DL72W972353Skin · corrodedTHE FUSELAGE SKIN LAP SPLICE AT STR 26L WAS FOUND WITH SEVERAL AREAS OF CORROSION AND SEVERAL EXISTING SRM REPAIRS. THE SECTION OF SKIN BETWEEN STA 480 TO 680 AND S24L TO 27L WAS REMOVED AND A NEW SECTION OF SKIN SPLICED IN PER ER/A 363125-14, REV B.Nov 12, 1997 · N2811W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W972323Pump · leakingON CLIMBOUT WITH B-SYS PUMP NR 2 B PRESSURE STARTED TO DROP TOWARD ZERO. SWAPPED B-PUMPS THEM B-SYS HYD QTY DROPPED TO ZERO. REPLACED HYD PUMP.Nov 10, 1997 · N2807W · Boeing 727247 · Hydraulic Pump (Electric/Engine), MainSDR DL72W972298Skin · crackedFOUND ON L/O CK, NUMBER 1 L/E FLAP CRACKED AT THE INBD HINGE CUTOUT. REPAIRED PER MM 57-30-0 AND ERA 363182-14.Nov 9, 1997 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W972276Stringer · crackedFOUND ON B-2 LETTER CK, CRACK AT BOLT HOLE OF VERTICAL STAB STRINGER S-9 AT STAB STA 133.80 RT SIDE. REPAIRED PER MM 55-30-0.Nov 6, 1997 · N2812W · Boeing 727247 · Vertical StabilizerSDR DL72W972221Fuel Control · failedENGINE NUMBER ONE FAILURE IMMEDIATELY AFTER T/O. FLAMEOUT/ LOSS OF THRUST REPORT FILLED OUT. REMOVED AND REPLACED NR ONE ENGINE FUEL BOOST PUMP AND FUEL CONTROL. RAN AND TRIMMED ENGINE PER PRHB.Oct 31, 1997 · N2817W · Boeing 727247 · Fuel Control/Turbine EnginesSDR DL72W972219Wire · crossedRT AFT EXTERIOR EMERGENCY LIGHT INOP. FOUND WIRES SWAPPED AT PLUG D5024. REPAIRED SAME AND REPLACED M957 FOR FUSES BLOWN, SYS CHKS GOOD.Oct 31, 1997 · N2807W · Boeing 727247 · Light System WiringSDR DL72E972331Stringer · crackedSTRINGER CRACKED VERT STAB INTERIOR STRINGER 1R AT RIB NR 4. STOP DRILLED CRACKS PER M/M 55-30-0 FIG 803. FABRICATED REP AIR PER M/M 55-30-0 PG 803 FIG 803. OK TO INSTALL. INSTALLED REPAIR PER M/M 55-30-0 PG 803 FIG 803.Oct 27, 1997 · N831WA · Boeing 727247 · Vertical StabilizerSDR DL72W972165Battery Pack · dischargedEMERGENCY EXIT LIGHT ON OVERHEAD FWD OF AFT GALLEY INOP. REPLACED BATTERY PACK.Oct 25, 1997 · N296WA · Boeing 727247 · Emergency LightingSDR DL72W972159Battery Pack · dischargedFWD AND MID OVERWING EMERG LIGHTS INOP. FOUND BATT PACK FOR FWD EMERG LIGHT INOP. REPLACED BATT PACK. OPS CK OK. FOUND PWR SUPPLY FOR MID EMERG LIGHT INOP. REPLACED PWR SUPPLY AND BATT PACK. OPS CK OK.Oct 25, 1997 · N2812W · Boeing 727247 · Emergency LightingSDR DL72W972134Bracket · cracked1.5 INCH VISIBLE CRACK IN NR 1 SLAT ACTUATOR ATTACH BRACKET I/B SIDE, FOUND AT E1 LTR CK. REPAIR PER M/M 57-20-21.Oct 22, 1997 · N2807W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W972101Fire Test Panel · malfunctionedAPU FIRE BELL CAME ON IN FLT WITH NO OTHER INDICATIONS AND WOULD NOT RESET OR CUT OUT AFTER SEVERAL ATTEMPTS. FINALLY WENT OUT AFTER MOVING BELL RESET PUSH-BUTTON SIDE TO SIDE. RESEATED CONNECTORS ON FIRE DETECT TEST PANEL.Oct 18, 1997 · N296WA · Boeing 727247 · Fire DetectionSDR DL72W972117Bulkhead Web · crackedDURING INPSECTION OF STA 1183 BULKHEAD PER SPECIAL INSPECTION 4-69150-12, A CRACK WAS DISCOVERED JUST BELOW A STIFFENER AT LBL 30, WL 188 IN THE WEB. THE CRACK MEASURED 2.5 INCHES. THE WEB MATERIAL IS .050 2024-T3 CLAD. THE -12 SPECIAL INSPECTION CALLS FOR Oct 15, 1997 · N2817W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72E972030Sill · corrodedC2 DOOR SILL WAS FOUND CORRODED ON THE OUTBD FLANGE. CORROSION CONFINED TO THE UPPER SURFACE OF OUTBD FLANGE. CUT OUT IN FLANGE IS 6.125 BY 1.625. REPAIRED PER ERA 330801-14.Oct 8, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E972035Sill · corrodedC2 DOOR SILL WAS FOUND CORRODED AT THE OUTBD CHORD AT FS 980. REPAIRED PER ERA 330800-14.Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E972034Skin · corrodedFUSELAGE SKIN BUTT SPLICE AND STRINGER WERE FOUND CORRODED AT S29R AND FS 1010. REPAIRED PER ERA 330802-14.Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E972032Frame · crackedWHILE ACCOMPLISHING EO 4-61247-12AD, A 0.75 CRACK WAS FOUND IN THE WEB OF THE NR 2 CARGO DOORWAY AFT FRAME. REPAIRED PER ERA 330827-14AD.Oct 7, 1997 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR 97FDEA00708Fire Loop · dirtyNR 2 FIRE PROTECTION SYS FAULT ILLUMINATED AND HORN SOUNDED INTERMITTENTLY AT THE TOP OF DESCENT. REMAINED OUT FOR THE REST OF THE FLIGHT. FOUND FIRE LOOP CONNECTIONS ON NR 2 ENG TO BE EXTREMELY DIRTY. REMOVED ALL FIRE LOOP AND HARNESS CONNECTIONS ON NR 2 EOct 7, 1997 · N233FE · Boeing 727247 · Fire DetectionSDR DL72W972106Skin · crackedDURING VISUAL INSPECTION, TPA MTC FOUND THREE CRACKS EMANATING FROM THE LAP JOINT BOLT HOLES. THESE CRACKS ARE .125, .25 AND .25 IN LENGTH. ALL CRACKS ARE CONFINED TO STA 594, STR 26L. THE REPAIR WILL CONSIST OF STANDARD SRM REPAIR PROCEDURES PER SRM 53-30-Oct 4, 1997 · N2811W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W971990Bulkhead · crackedA 2 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8.0 AND WL 180. THIS ER/A WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AIRWORTHINESS DIRECTIVE 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FWD SIDOct 3, 1997 · N2816W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W971970Stringer · crackedVERT STAB STR 9L IS CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.Oct 3, 1997 · N2811W · Boeing 727247 · Vertical StabilizerSDR DL72W971969Skin · crackedFOUND DURING D2 LETTER CHECK, .5 INCH CRACK RT ELEVATOR LOWER SKIN FWD OF ACCESS PANEL 9414. REPAIRED PER SRM 55-20-3.Oct 3, 1997 · N2811W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W971968Stringer · crackedFOUND DURING D2 LETTER CHECK, VERT STAB STR 9L CRACKED AT FIN STA 133.800. REPAIRED PER M/M 55-30-0.Oct 3, 1997 · N2811W · Boeing 727247 · Vertical StabilizerSDR DL72W971945Stringer · crackedFOUND DURING A2 LETTER CHECK, VERT STAB STR 96 CRACKED AT FIN STA 180.6. REPAIR PER M/M 55-30-0.Oct 1, 1997 · N296WA · Boeing 727247 · Vertical StabilizerSDR DL72W971944Angle · crackedFOUND AT A2 LETTER CHECK, GUSSET ANGLE CRACKED RT SIDE STA 1263 BELOW STAIR ACTUATOR PAD. REPLACED ANGLE PER SRM 53-10-10.Oct 1, 1997 · N296WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W971939Light · inoperativeRT OVERWING EXIT FWD CENTER AISLE AND AFT RT EXTER FAIRING EMERGENCY LIGHT INOP.Sep 30, 1997 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W971912Battery Pack · dischargedEMERGENCY LIGHT FLASHING DURING TEST. REPLACED BATTERY UNIT IN M1095, CHECKS GOOD.Sep 27, 1997 · N296WA · Boeing 727247 · Emergency LightingSDR 97FDEA00694Doubler · crackedCRACK IN HAT SECTION OF STR 13L AT BS 1330. STOP DRILLED CRACK AND INSTALLED 7075T-6 .063 DOUBLER.Sep 26, 1997 · N235FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 97FDEA00693Stringer · corrodedBS 730 TO 734 ON STRINGER 28 LT CORRODED. REMOVED CORROSION, TREATED AND PRIMED STRINGER. INSTALLED .050 7075T-6 STRAP PER EA 7-5310-29227.Sep 24, 1997 · N235FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W971877Skin · crackedA/C WAS FOUND IN LGA ON 9-17-97 WITH A 3 CRACK IN THE FUSELAGE SKIN AT S20R BETWEEN STA 660 AND 680 AND OIL-CANNING CONDITION AT THE SAME STATION IN THE FIVE STRINGER BAYS BELOW THE CRACK. CRACK WAS REPAIRED PER SRM AND THE OIL-CANNING CONDITION WAS AUTHORIZESep 19, 1997 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W971823Bracket · crackedNR 6 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED I/B SIDE AT MOUNT BOLT HOLES. REPAIRED PER MM 57-20-21.Sep 18, 1997 · N2817W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W971822Stiffener · crackedFOUND DURING A-1 LETTER CHECK, 1.5 INCH CRACK L/E SPAR STIFFENER AT NR 2 SLAT I/B TRACK ROLLER BOX I/B SIDE. REPAIRED PER M/M 57-20-21.Sep 18, 1997 · N2817W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W971813Skin · crackedFOUND CRACK IN SKIN AFT OF FWD CARGO DOOR WITH EXTENSIVE OIL CANNING. REPAIRED PER ERA 362766-14.Sep 17, 1997 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E971950Frame · crackedFUSELAGE FRAME CRACKED AT STA 930 STR 13 AND 14 LT SIDE. REPAIRED PER M/M 53-10-4 FIG 25 AND ERA 330775-14.Sep 14, 1997 · N2829W · Boeing 727247 · Fuselage Main, FrameSDR DL72E971855Rib · crackedRIB IS CRACKED AT ACTUATOR ATTACH HOLE I/B RIB. PLATE AT ATTACH HOLE IS WORN ON SAME RIB. SMALL LEG ON RIB IS MISSING THAT ATTACHES CHORD ANGLE. REPAIRED PER MM 57-54-00 PG 805 ITEM 2, REPLACED PLATE PER SRM 51-00.Sep 14, 1997 · N2829W · Boeing 727247 · Leading Edge DevicesSDR DL72E971854Rib · crackedRIB IS CRACKED AT NUT PLATE O/B RIB AT ACTUATOR ATTACH HOLE ON NR 4 SLAT. REPAIR DOUBLER IS CRACKED ON SAME RIB. REPAIRED PER MM 57-54-0 PG 805.Sep 14, 1997 · N2829W · Boeing 727247 · Leading Edge DevicesSDR DL72E971881Skin · corrosionDURING INSPECTION OF THE LOWER WIND SKIN PER EO 4-37113-3, CORROSION WAS FOUND ON THE SKIN AT APPROX FS 825 AND LBL 32.2. THE DAMAGE CUTOUT MEASURED 7.5 (IB/OB) BY 6.125 (FORE/AFT). REPAIRED PER ERA 330730-14AD.Sep 12, 1997 · N831WA · Boeing 727247 · Wing, Plate/SkinSDR DL72E972129Spar · crackedCRACK AFT SPAR 53 FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0.Sep 11, 1997 · N2829W · Boeing 727247 · Trailing Edge FlapsSDR DL72E971878Blkhd Stiffener · crackedAN EXISTING REPAIR WAS FOUND ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THIS REPAIR WAS REMOVED AND A 2.5 CRACK WAS DISCOVERED IN THE IB FLANGE-TO-WEB RADIUS. S/B 727-53-0175 WHICH IS REQUIRED BY AD 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND Sep 10, 1997 · N831WA · Boeing 727247 · Fuselage Main, BulkheadSDR 97FDEA00634Actuator · leaksNR 1 SYS-A HYDRAULIC PRESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. WHEN GEAR LEVER WAS POSITIONED TO UP NR 2 SYS-A LIGHT ILLUMINATED AND HYDRAULIC QUANTITY RAPIDLY FELL TO 0 GALLONS. PRESSURE DROPPED TO 0 PSI. ACCOMPLISHED APPROPRIATE ABNORMAL PROCEDURES.Sep 5, 1997 · N236FE · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W971770Web · crackedLOWER LT TORQUE BOX WEB CRACKED AT LIGHTENING HOLES STA 1223 AND 1263. REPAIRED BOTH CRACKS PER MM 53-11-0.Sep 3, 1997 · N290WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W971660Light · inoperativeAFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WOULD NOT TEST. REPLACED LIGHT ASSY.Aug 25, 1997 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W971657Web · crackedFOUND DURING B-2 LETTER CHECK, VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 CRACKS AT LT SIDE. ONE CRACK AT LWR CORNER AND ONE APPROX 6.5 INCHES ABOVE LWR CORNER. REPAIRED PER M/M 53-11-0.Aug 25, 1997 · N294WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E971644Act Bracket · crackedNR 5 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED AT O/B UPPER CORNER. INSTALLED DOUBLER PER M/M 57-20-21.Aug 21, 1997 · N2829W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E971643Act Bracket · crackedA 2 INCH CRACK AT NR 8 L/E SLAT ACTUATOR ATTACH BRACKET O/B SIDE. INSTALLED DOUBLER PER M/M 57-20-21.Aug 21, 1997 · N2829W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E971586Skin · dentedTHE FUSELAGE SKIN WAS FOUND DENTED ON THE C2 DOOR CUTOUT LOWER EDGE AT APPROXIMATELY STA 970. DAMAGED PARTS WERE THE UPPER SKIN, THE LOWER SKIN, AND THE BEAR STRAP. A CUTOUT WAS MADE THROUGH ALL THREE LAYERS WHICH MEASURED 1 BY 2. A REPAIR SCHEME WAS MADE UAug 12, 1997 · N830WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W971561Line · leakingSYSTEM B LOW PRESS LIGHT 2 EACH CAME ON AND QUANITY WENT TO 0. FOUND NR 2 A/C HYD PUMP PRESS AND RETURN LINES WITH A SMALL HOLE IN THEM, THE PRESS LINE MADE THE HOLE IN THE RETURN LINE. REPLACED LINES.Aug 8, 1997 · N2814W · Boeing 727247 · Hydraulic System, MainSDR DL72W971575Skin · corrosionCORROSION WAS DISCOVERED ON THE INNER SURFACE OF THE FUSELAGE SKIN AROUND THE RT WING SCANNING LIGHT CUTOUT. A 3 BY 2 REGION AROUND THE AFT TOP CORNER OF THE CUTOUT WAS BLENDED TO A MAXIMUM DEPTH OF 0.032. A SECOND BLEND AREA ALONG THE LOWER EDGE OF THE CUTOAug 7, 1997 · N295WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W971573Skin · corrodedTHE FUSELAGE SKIN BETWEEN STA 680 AND 700 AND BETWEEN STR 26L AND 26R WAS FOUND WITH TWO SPOTS OF CORROSION WHICH REQUIRED CUTOUTS. ADDITIONALLY, TWO EXISTING DOUBLER REPAIRS ARE IN THE AREA WITH LESS THAN 1 SEPARATION. ALL DAMAGE WAS REMOVED BY SPLICING IN Aug 4, 1997 · N295WA · Boeing 727247 · Fuselage Main, Plate/Skin
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