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 UPS96221254Angle · corrodedINSPECTION TYPE: C. CORROSION ON SUPPORT ANGLE STA 610-613 RBL 13 WL 158. REMOVED, FABRICATED AND REPLACED ANGLE IAW SRM'S 51-30-2, 53-10-2 AND MM 57-20-31.Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221253Splice · corrodedINSPECTION TYPE: C. CORROSION ON STR 27R SPLICE STA 675-685 AREA MARKED. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-1, 51-10-6, AND 51-10-5 AND 51-30-2.Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221252Splice · corrodedINSPECTION TYPE: C. CORROSION ON STR 28R SPLICE STA 675-685 WL 149. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-6, 51-10-1, 51-30-2, AND 51-10-5.Sep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221251Shear Tie · corrodedINSPECTION TYPE: C. CORROSION ON FRAME AROUND FASTENERS AT BS 950F RBL 3 WL 151. REMOVED CORROSION FROM FRAME AT STA 950F RBL 3 WL 151. REWORKED FRAME FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1, HOWEVER, CORROSION WAS FOUND ON SHEAR TIE OUT OF LIMITS IAW SRSep 30, 1996 · N211UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221250Shear Tie · corrodedINSPECTION TYPE: C. CORROSION ON SHEAR TIE STA 500 RBL 17-22 WL 150. MECH REMOVED CORROSION FROM SHEAR TIE AT STA 500 RBL 17-22 WL 150. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.Sep 30, 1996 · N211UP · Boeing 727247 · Wing Miscellaneous StructureSDR UPS96221249Rib · crackedINSPECTION TYPE: C. RT WING INBOARD MIDFLAP HAS CRACKED NOSE RIB IN L/E AT CENTER FOREFLAP TRACK INBOARD OF TRACK. REMOVED DAMAGED RIB, INSTALLED NEW RIB, ALL WORK DONE PER SRM'S 51-30-2 AND 51-30-5.Sep 27, 1996 · N211UP · Boeing 727247 · Trailing Edge FlapsSDR UPS96221134Shear Tie · corrodedINSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. MECHANICALLY REMOVED CORROSION FROM SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPAIRED SHEAR TIE/FRAME IAW SRM 53-10-4.Sep 19, 1996 · N207UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221133Frame · crackedINSPECTION TYPE-C, RIGHT HAND AFT SERVICE DOOR FORWARD FRAME LOWER HINGE CUTOUT UPPER I/B CORNER IS CRACKED .35 LONG. REMOVED AND REPLACED AFT SERVICE DOOR FORWARD FRAME IAW SRM 51-10-1, 51-10-2, MM 51-20-151, 52-14-00.Sep 19, 1996 · N207UP · Boeing 727247 · Service DoorsSDR UPS96221135Bullnose · corrodedINSPECTION TYPE-C, CORROSION ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. MECHANICALLY REMOVED CORROSION ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. REWORKED DEEMED OUT OF LIMITS IAW SRM ADDENDUM B727-5740-3980A. REPAIRED Sep 18, 1996 · N207UP · Boeing 727247 · Leading Edge DevicesSDR UPS96221131Rib · crackedINSPECTION TYPE-C, WHILE WORKING WINGS 162 FOUND CRACKED RIB ON NR 5 SLAT O/B OF ROD END DUE TO OTHER DAMAGE TO NR 5 SLAT. THE SLAT IS BEING REPLACED ON NRC 607692 AND INSTALLED ON NRC 607694.Sep 18, 1996 · N207UP · Boeing 727247 · Leading Edge DevicesSDR UPS96221165Frame · corrodedINSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 970 FRAME RBL 8 WL 149. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGE AND REPLACED PER SRM 53-10-4.Sep 17, 1996 · N207UP · Boeing 727247 · Fuselage Main, FrameSDR UPS96221164Shear Tie · corrodedINSPECTION TYPE-C, CORROSION ON AFT SIDE OF SHEAR TIE AT BS 720C WL 149 RBL 10. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED SHEAR TIE IAW SRM 51-20-1, 51-30-2 AND MM 51-20-151.Sep 17, 1996 · N207UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W962109Battery · dischargedFOUND AFT AIRSTAIR_EMERGENCY EXIT LIGHTS AND LIGHT BELOW FLIGHT ATTENDANT PANEL INOP. REPLACED BATTERIES, RELAMPED, REPLACED EMERG. LIGHT ASSY AND RESECURED WIRES TO THE LIGHT ASSY BELOW FLT ATT PNL.Sep 14, 1996 · N2810W · Boeing 727247 · Emergency LightingSDR DL72W962103Gasper Fan · failedSTRONG BURNING SMELL IN COCKPIT REPLACED GASPER FAN. OPERATIONAL CHECKS GOOD.Sep 12, 1996 · N2812W · Boeing 727247 · Air Distribution FanSDR DL72W962008Light · inoperativeAFT AREA EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY EMERGENCY LIGHTS, CK OK.Aug 29, 1996 · N2813W · Boeing 727247 · Emergency LightingSDR UPS96220969Skin · delaminatedINSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 AREAS OF DISBOND UPPER SURFACE. REPAIRED PER SRM 51-40-6.Aug 25, 1996 · N212UP · Boeing 727247 · Trailing Edge FlapsSDR UPS96220968Skin · delaminatedINSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 INCH AREA OF DISBOND, LOWER SURFACE. REPAIRED PER SRM 51-40-6.Aug 25, 1996 · N212UP · Boeing 727247 · Trailing Edge FlapsSDR UPS96220967Shear Tie · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1166 BETWEEN STR 28 AND 29 LT. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE AT STA 1166 IAW SRM 51-30-1.Aug 25, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220974Shear Tie · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01. 02-02) ON SHEAR TIE STA 1130 BETWEEN STR 28 TO 29 RT. CORROSION REMOVAL WAS OUT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED. ALL WORK DONE IAW SRM 53-10-1, 53-10-4, 51-30-2, 51-10-02.Aug 23, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220972Blkhd Stiffener · corrosionINSPECTION TYPE-C, 740 BULKHEAD VERTICAL STIFFENER HAS CORROSION ON BOTTOM AROUND FASTENERS, RBL 25 WL 146. REMOVED CORROSION AND FOUND OUT OF LIMITS. STIFFENER WAS REMOVED AND INSTALLED NEW STIFFENER. ALL WORK ACCOMPLISHED PER SRM 53-10-11, 51-30-5, 51-20-Aug 23, 1996 · N212UP · Boeing 727247 · Fuselage Main, BulkheadSDR DL72E962049Door Frame · elongated holesFOUR FASTENER HOLES FOUND ELONGATED ON THE STA 760.95 RT OVERWING EXIT FRAME. THESE HOLES WILL BE OVERSIZED PER B727 S/B 53-01-97, REVISION 2.Aug 23, 1996 · N283WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220976Shear Tie · corrosionINSPECTION TYPE-C, SHEAR TIE IS CORRODED AND FOUND OUT LIMITS. WHILE REMOVING SHEAR TIE FOUND FRAME SPLICE PLATE TO BE CRACKED. RECEIVED AND INSTALLED NEW SHEAR TIE AND FABRICATED NEW FRAME SPLICE PLATE AND INSTALLED. ALL WORK ACCOMPLISHED PER SRM 51-10-6, Aug 22, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220975Support · crackedINSPECTION TYPE-C, NR 2 SLAT I/B TRACK SUPPORT, O/B RIB IS CRACKED. REMOVED AND REPLACED NR 2 SLAT ASSY PER M/M 27-81-11.Aug 22, 1996 · N212UP · Boeing 727247 · Leading Edge DevicesSDR UPS96220973Shear Tie · corrodedINSPECTION TYPE-C, CORROSION (C530113-01.00-01) CORROSION ON SHEAR TIE AND WEB STA 600, LBL 19 TO 22 WL 146. CORROSION REMOVAL OUT OF LIMITS ON SHEAR TIE, WEB WAS WITHIN LIMITS. FABRICATED NEW SHEAR TIE AND INSTALLED. FOUND CRACKED SKIN UNDER SHEAR TIE, REMAug 22, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221031Stringer · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8, WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 INCH BY 1 INCH AREA, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS96220979Stringer · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8 WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 BY 1 AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS96220977Shear Tie · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1070 BETWEEN STR 29 TO 30 LT. CORROSION FOUND OUT OF LIMITS, DUPLICATE WRITE-UP OF NRC 584267, ALL WORK TO BE ACCOMPLISHED ON NRC 584267.Aug 21, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220990Stiffener · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-02) ON SHEAR TIE STA 969.5 WL 149 LBL 2, LBL 10 AREA MARKED. REMOVED CORROSION AND FOUND STIFFENER OUT OF LIMITS, SHEAR TIE CORROSION WAS WITH IN LIMITS. REMOVED AND REPLACED STIFFENER. ALL WORK IAW SRM 51-10-6, 5Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220980Support · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-01) AROUND BOTTOM OF NUTPLATES STA 520 TO 540. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, FLOOR SUPPORT WILL BE REPLACED ON NRC 584590.Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220978Clip · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON STRINGER CLIP STA 1040, STR 29 RT. STRINGER CLIP CORRODED OUT OF LIMITS. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-10-1, 51-19-6 AND 53-10-1.Aug 20, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96220971Frame · corrodedINSPECTION TYPE-C, CORROSION ON STIFFENER AND FRAME BS 990 WL 139 LBL 7 TO 13. REMOVED CORRODED AREA OF FRAME AND REPAIRED PER SRM 53-10-04.Aug 16, 1996 · N212UP · Boeing 727247 · Fuselage Main, FrameSDR UPS96220970Shear Tie · corrodedINSPECTION TYPE-C, CORROSION SHEAR TIE BS 950A BETWEEN STR 28 TO 29 RT. REMOVED SHEAR TIE AND REPLACED PER SRM.Aug 16, 1996 · N212UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS96221007Fitting · corrodedINSPECTION TYPE: C. LT INBOARD TAB FITTINGS CORRODED AILERON SIDE. REMOVED AND REPLACED LT INBOARD TAB FITTINGS AILERON SIDE PER SRM 51-30-2.Aug 15, 1996 · N212UP · Boeing 727247 · Aileron TabsSDR DL72E961901Light · inoperativeFOUND AFT STAIR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.Aug 13, 1996 · N830WA · Boeing 727247 · Emergency LightingSDR DL72W961798Batteries · dischargedON LAYOVER, FOUND FORWARD CROSS-AISLE CEILING LIGHT FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, LIGHTS CHECK GOOD.Jul 27, 1996 · N297WA · Boeing 727247 · Emergency LightingSDR DL72W970183Rib · crackedDURING INITIAL INSPECTION, RIB NR 4 AND RIB NR 5 WERE FOUND CRACKED. THEY WERE REPAIRED PER SRM 57-50-3.Jul 26, 1996 · N2817W · Boeing 727247 · Leading Edge DevicesSDR DL72W961762Bulkhead Web · crackedFOUND CRACK AT RBL 27 OF BS 1183 BULKHEAD WEB. THE DAMAGE CONSISTED OF A .75 INCH CRACK AT WL 170. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY S/B 727-53-171. REPAIRED PER B727 SRM 53-10-9, FIG. 4.Jul 23, 1996 · N2819W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W961732Frame · crackedR2 DOOR FWD FRAME CRACKED AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-02 FIG 4.Jul 10, 1996 · N297WA · Boeing 727247 · Service DoorsSDR DL72W961723Skin · crackedTHE FUSELAGE SKIN WAS INITIALLY CRACKED AT STA 1095.9 OUTBOARD OF STR 1. THE DAMAGE WAS REPAIRED WITH A TIME LIMITED DOUBLER. WHEN THE PERMANENT REPAIR WAS BEING INSTALLED, TWO ADDITIONAL DAMAGE LOCATIONS WERE FOUND. A NEW PERMANENT REPAIR DOUBLER WAS INSTAJul 9, 1996 · N297WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E961629Skin · corrosionTHE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR STR 28R. THE SKIN IS MANUFACTURED FROM CLAD 2024-T3 CHEM-MILLED WITH A LOCAL THICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DISCOVERED, STR 28R AT FSJul 9, 1996 · N2829W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961599Bracket · crackedFOUND ON B1 LETTER CK, NR 1 SLAT ACT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21.Jul 3, 1996 · N290WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W961598Bracket · crackedFOUND ON B-1 LETTER CK, NR 2 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED AT THE UPPER CORNER. REPAIRED PER MM 57-20-21.Jul 3, 1996 · N290WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W961597Engine · flame-outNR 1 ENGINE SHUTDOWN ON T/O ROLL AT AT 40 KTS. REPLACED NR 1 ENGINE FUEL PUMP.Jul 3, 1996 · N295WA · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W961565Generator · failedNR 1 GEN ALREADY ON MCO NR 2 GEN FAILED. NR 2 ENGINE CSD/ GEN CHANGE IN PROGRESS.Jul 1, 1996 · N2820W · Boeing 727247 · AC Generator-AlternatorSDR DL72E961567Skin · crackedFOUND ON D2 LETTER CK, .4687 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER MM 53-30-0.Jul 1, 1996 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E961566Skin · crackedFOUND ON D2 LETTER CK, AFT AIRSTAIR DOOR CUTOUT RT FWD RADIUS CRACKED. REPAIRED PER MM 53-30-0.Jul 1, 1996 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961557Tr Unit · burntVISIBLE SMOKE EXHAUSTING FROM E/E COMP WITH ESS TR C/B POPPED, SMELLS ELECTRICAL. FOUND AND REMOVED ESS T/R AND REPLACED NR 3 TR, OPS OK.Jun 29, 1996 · N2815W · Boeing 727247 · DC Rectifier/ConverterSDR DL72W961544Web · crackedTORQUE BOX WEB CRACKED .5 INCH IN ADJACENT RT HAND RAIL STA 1233. INSTALLED DOUBLER PER MM 53-11-0.Jun 27, 1996 · N2810W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E961711Spar Web · damagedUPPER SPAR WEB FLANGE DAMAGED BY STOP DRILLING RIBS NR 11 AND NR 12. MANUFACTURED DOUBLER, REPAIRED PER SRM 57-50-3 FIG 4.Jun 25, 1996 · N282WA · Boeing 727247 · Leading Edge DevicesSDR DL72E961710Rib · crackedLOWER FLANGE OF RIB NR 18 CRACKED IN RADIUS. STOP DRILLED CRACK AND REPAIRED PER SRM 57-54-0.Jun 25, 1996 · N282WA · Boeing 727247 · Leading Edge Devices
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