Boeing 727-2S2F
Service difficulty reports · 842
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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 = '7272S2F' 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 = '7272S2F' 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 FDEA201009173521Web · crackedAFT AIRSTAIRS LT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1220. TRIMMED OUT DAMAGED AREA DIM. 3/4" X 3/8" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 0.032" DIM. 4" X 2" IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DSDR FDEA201009163511Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. FABRICATED NEW STUB FRAME FROM 7075 0 .040" DIM 22" X 5" IAW SRM 51-10-3 AND 51-20-1 FIG 7 REV 103. REMOVED SHEAR TIE AT BS 950E BETWEEN STR 29R AND 28R IAW SRM 51-30-2 AND REINSTALLED SHEAR SDR FDEA201009153526Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 400 BETWEEN LBL 45 AND 25 UPPER I BEAM TOP AND BOTTOM SURFACE IS CORRODED. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3. FABRICATED REPAIR PARTS. INSTALLED REPAIR IAW SRM 53-10-8 FIG 3 AND 51-10-2.SDR FDEA201009143414Frame Splice · damagedUPON FRAME REMOVAL, FOUND DOUBLE DRILLED HOLES IN FRAME SPLICE, STA 950B, STR 24L. REMOVED PRODUCTION SPLICE/DOUBLER IAW SRM 51-30-2 FORMED NEW DOUBLER IAW SRM 51-20-1 FIG 7 INSTALLED NEW DOUBLER IAW SRM 51-30-2 REV 103.SDR FDEA201009133422Floorbeam · corrodedCORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 344 FROM LBL 10 TO RBL 10. REMOVED DAMAGED AREA 8' SECTION IAW SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR TEE SECTION, ANGLES, AND SHIMS IAW SRM 53-10-8 FIG 9 DETAIL 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 5SDR FDEA201009103343Attach Angle · crackedLT WING FALSE SPAR ATTACH ANGLE IS CRACKED WBL 118. REMOVED DOUBLER AND CUT OUT LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED REPAIR ANGLES, NEW WEB, NEW I/B CHORD SECTION, NEW STRAP, RADIUS FILLERS, AND NEW WEB IAW DRAWING SR 27-57-038 REV C. INSSDR FDEA201009093329Keelbeam · crackedRT WW, RT KEEL BEAM IS CRACKED AT BS 875 RBL10 TRIMMED OUT DAMAGED AREA AT LOWER CHORD OF KEEL BEAM STA 875 RBL 6 IAW SRM 51-10-1. FABRICATED DOUBLER FROM PN 15-5PH 0.071" DIM. 8.6250' X 4" AND INSTALLED DOUBLER IAW EA 7-5310-135591.SDR FDEA201009083316Stringer · corrodedCORROSION ON STRINGER 29L BETWEEN BS 950D AND 950E. REMOVED AND REPLACED STRINGER 29L FROM BS 950 - 1010 IAW B727 SRM 53-10-2 FIG 9, 51-30-5 AND 51-30-2 REV 103SDR FDEA201009043277Skin · corrodedUPON REMOVAL OF STRINGER SECTION, FOUND SKIN CORRODED, BS 1030 AFT OF FRAME AT STRINGER 26R. CUT OUT DAMAGED AREA AT BS 1045 DIM 9" X 3" IAW B727 SRM 53-30-3 FIG 5 FABRICATED DOUBLER, FILLER, AND SKIN FILLER IAW 53-30-3 FIG 5 REV 103, INSTALLED REPAIR SDR FDEA201009033341Skin · corrodedSKIN BULGE STA 1173 AT LAP SEAM STR 20R. COMPLIED WITH EA 7-5330-135593.SDR FDEA201009033269Stringer · corrodedSTRINGER 26L AT BS 1040-1055 IS CORRODED AT LOWER SURFACED. CUT OUT DAMAGED STRINGER FROM STA 1040 TO 1055 IAW SRM 53-10-1 FIG 1. FABRICATED STRINGER FROM BAC1498-147 7075T6 DIM 15 7/8" AND 2EA SPLICES FROM BAC1498-131 7075T6 DIM 12 1/4". INSTALLED REPAIRSDR FDEA201009033266Web · crackedAFT AIRSTAIRS RT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1303. TRIMMED OUT DAMAGED AREA DIM. 1" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.SDR FDEA201009033265Web · crackedAFT STAIRWELL LT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1223. TRIMMED OUT DAMAGED AREA DIM. 1/2" X 1/4" AND 1/2" X 1/8" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLERS. IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLERS IAW SSDR FDEA201009033268Skin · bulgedSKIN BULGE STA 1052, STR 26L, LAP SEAM. CUT OUT LOWER SKIN DIM. 2" X 2" AT STA 1052 STR 26L LAP SEAM. FABRICATED REPAIR FROM 2024T3 0.071" DIM. 9.750" X 9", DOUBLER FROM 2024T3 0.063" DIM. 11" X 5", AND FILLER FROM 2024T3 0.050" DIM. 2" X 2". IAW SRM 53-30-SDR FDEA201009023342Skin · crackedRT LOWER AFT FUSELAGE AT BS 1010 STR 28R EXTERIOR SKIN IS CRACKED AND BULGING. CUT OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3A REV 103. FABRICATED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592. INSTALLED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592.SDR FDEA201009023272Skin · bulgedSKIN BULGE STA 1045 STR 26R LAP SEAM. REMOVED CORRODED STRINGER SECTION FROM BS 1026 TO 1070, STR 26R IAW SRM 51-30-2. FABRICATED 3 (EA) STRINGER SECTIONS FROM BAC1498-147 7075 T62 DIM 19" AND 4 (EA) SPLICE SECTIONS FROM BAC1498-131 7075 T6 DIM 9" IAW SRM 53SDR FDEA201009023245A/C Pack · failedON TAKEOFF FROM DSM ,THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN THE COCKPIT. QRH PROCEDURES ELIMINATED THE SMOKE & REESTABLISHED THE LT PACK. GIVEN THE OUTSIDE ASDR FDEA201009013243Fan · failedON TAKEOFF FROM DSM, THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN THE COCKPIT. QRH PROCEDURES ELIMINATED THE SMOKE & REESTABLISHED THE LT PACK. GIVEN THE OUTSIDE ASDR FDEA201008283173Gasper Fan · damagedCREW SMELLED SMOKE-LIKE ODOR ENTERING THE COCKPIT. ISOLATED ODOR TO GASPER FAN. ODOR WAS NOT PRESENT WITH GASPER FAN OFF. LEFT THE GASPER FAN OFF FOR REMAINDER OF THE FLIGHT. AFTER T/S FOUND THE GASPER FAN TO BE THE MAIN ISSUE. R & R GASPER FAN IAW MM 2SDR FDEA201008263157Unknown · smokeAIR TURN BACK, SMOKE IN COCKPIT SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT.SDR FDEA201008263156Unknown · odorAIR TURNBACK, SMOKE IN COCKPIT, SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT. VISIBLY CHECKED FWD NOSE COMPARTMENT WIRING, LIGHT BALLAST AND UNDER QUADRANT AREA, FOUND NO EVIDENCE OF FAULT. CHECKED AVIONICS BAY, WIRING, BOXES, FOUND LIGHTS ON EPGSDR FDEA201007202607Regulator · inoperativeON CLIMBOUT, SMOKE IN COCKPIT STARTED AND CONTINUED TO GET WORSE. "AIR RETURNED" AND SHUTDOWN ON TAXIWAY. SMOKE LESSENED WHEN THROTTLES WERE RETARTED TO ILDE AND COMPLETLY WENT AWAY AFTER SHUTDOWN. R & R HYD AIR PRESSURE REGULATOR IAW SMP. RAN ALL ENGINES SDR FDEA201005081496Engine · leakingOIL QUANTITY DECREASED AFTER TAKEOFF. WITH .8 GAL INDICATED, BEGAN TO DECREASE IN OIL PRESSURE, AND WENT TO ZERO WITH LO PRESS/ FILT BYPASS LT ON. SHUTDOWN TIME 2040Z, ENGINE 2 WINDMILL AT 18 PERCENT N2 AND 13 PERCENT N1 TILL LANDING AT 2103 Z WITH 0 OIL PRESDR FDEA201005071486Gearbox · leakingDURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN IAW RED TABS DID NOT LOOSE OIL QTY. ENGINE CONTINUED TO WINDMILL AFTER SHUTDOWN. R & R THE NR 3 SDR FDEA201005071497Warning Light · illuminatedLEFT A/C PACK TRIP LIGHT ILLUMINATED FOLLOWED BY EXCESSIVE CABIN ALT. COMPLETED QRH FOR PACK TRIP LIGHT ILLUMINATED. PACK RESTORED AFTER CHECKLIST. PERFORMED OPS CHECK OF PACK, NORMAL OPERATION CHECK'S NORMAL PERFORMED OPS CK OF SINGLE PACK PRESSURIZATION ISDR FDEA201004221291Stringer · corrodedSTRINGER 29L IS CORRODED AROUND FASTENERS FROM BS 950A TO 950E. R & R STRINGER 29 LT FROM PN65-56441-7 BETWEEN BS 950 TO BS 1008 IAW DWG 65-56441 AND IAW SRM 51-30-2.SDR FDEA201004171217Switch · corrodedWHILE CLIMBING THROUGH 6-7000 FT AFTER TAKEOFF, AMBER AFT AIRSTAIR LIGHT ON S/O PANEL CAME ON. RAN QRH & RETURNED TO DEPARTURE. LIGHT REMAINED ON UNTIL JUST AFTER LANDING WHEN ACFT DEPRESSURIZED. RELEASED FOR SERVICE FOUND MARGINAL ADJUSTMENT ON S395 (AFTSDR FDEA201004011045Clamp · missingON CLIMB-OUT NR 3 FIRE HANDLE AND WARN LIGHT, AND BELL CAME ON. ON LEVEL OFF THRUST LEVELS PULLED BACK LIGHTS (FIRE) WENT OUT. SHUT DOWN ENGINE, FIRE WARNING TEST WAS GOOD. REMOVED AND INSPECTED THE CHIP DETECTORS AND REPLACED THE OIL FILTER IAW P&W JT8DSDR FDEA201003140818Controller · failedNR 3 ENG FIRE INDICATION CLIMBING THRU 10,000. PULLED FIRE HANDLE AND FIRE INDICATION CEASED. DID NOT DISCHARGE FIRE BOTTLE. NOTE: DELAYED STARTING NR 3 ENG ON TAXI OUT ENG OIL TEMP REQUIRED 5 MINUTES TO REACH GREEN BAND ALL OTHER ENG INDICATIONS NORMAL. SDR FDEA201001050009Transmitter · failedNR 2 EPR GAUGE FAILED ON T/O. ABORTED T/O. RAN REJECTED T/O CHECKLIST. WAITED REQUIRED 16 MINUTES FOR BRAKE COOLING. AFTER SUBSEQUENT T/O EPR GAUGE BEGAN TO OPERATE NORMALLY 20 MINUTES INTO FLIGHT. NR 2 ENG EPR LINE PURGED WITH NITROGEN IAW MM REF: 77-11-SDR FDEA200912084385Actuator · malfunctionedDURING T/O AND FLAP RETRACTION AMBER FLAP LIGHT REMAINED ON AT FLAPS 2. SLATS 2367 WERE OUT AND THE AMBER LIGHT UNDER NR 6 SLAT POS ON SO PANEL WAS ON. ATTEMPTED TO RECTIFY WITH THE QRH. NO LUCK. PUT FLAPS BACK TO 5 AND LANDED AT BIL IAW GOC DIRECTIVES. RASDR FDEA200911284211Apu · burnedON BLOCK-IN APU WAS SMOKING FROM EXHAUST-PIPE. UPON ENTERING COCKPIT FOUND EGT INDCATOR RISING RAPIDLY WENT BACK OUTSIDE AND SAW FLAMES AROUND 6 TO 12 INCHES COMING FROM TAIL PIPE, NOTIFIED FLIGHT CREW OF FIRE AND TO BLOW FIRE BOTTLE. AROUND 1 TO 2 MINUTESSDR FDEA200910153577Switch · failedAILERON SYS A ANNUNCIATOR LIGHT ON F/O PANEL CAME ON 30 AFTER LEVEL OFF, NO LOSS OF A SYS A HYD FLUID. REMOVED AND REPLACED AILERON "A" SYS HYD LOW PRESSURE WARNING SWITCH IAW AMM 27-10-144-4, OPS CHECKED GOOD.SDR FDEA200909113306Skin · delaminatedNR 10 SPOILER HAS DELAMINATION, COMPLIED WITH PART 1 OF EA 7-5770-134135. . REMOVED AND REPLACED SPOILER WITH 2 DIFFERENT SPOILERS, SAME RESULTS. INSTALLED ORIGINAL SPOILER REPLACEMENT FOR EVALUATION. NO BOLTS, PINS SAFTIED. COMPLETED INSTALLATION OF SPOILERSDR FDEA200909113305Skin · delaminatedNR 14 SPOILER PANEL HAS DELAMINATION. COMPLIED WITH PART 1 OF EA 7-5770-134135. NO FURTHER DAMAGE FOUND, APPLIED TAPE TO CRACK ON T/E OF SPOILER, OK TO CONTINUE. PART 2 TO BE ACCOMPLISHED WITHIN 2 FLIGHT CYCLES. OIL 11SEP09 22:33 COS R NO RESTRICTION SDR FDEA200908283116Seat Track · gougedGOUGED FLOATING SEAT TRACK BS 740-BS 760 LBL 24.5. REMOVED DAMAGED SEATTRACK AT BS 740 TO BS 760 LBL 24.5 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM BAC 15201431 PO NR 6360180 APPROX DIM: 18 INCH IN LENGTH IAW SRM 53-10-2 FIG 7 AND SRM 51-30-5, TREATED SDR FDEA200908263103Skin · crackedRT INBD FOREFLAP WBL 22, CRACK ABOVE CARRIAGE ATTACH FITTING, L/E SKIN. CHEMICALLY REMOVED PAINT IAW MM 51-20-001-7 STOP DRILL CRACK 2 EA DIM: .250 IAW SRM 51-10-1 HFEC SHOW CRACK END ON STOP DRILLS IAW NDTM PT6 51-00-00, FIG 23 FABRICATED DOUBLER REPAIR FRSDR FDEA200908263098Fitting · crackedMCD LWR AFT LOCK ACT BS 615 ROD END BEARING HAS PLAY, CAM ACTUATOR FITTING CRACKED AND MISSING BOLTS. REMOVED AND REPLACED MCD LWR AFT HOOK AND CRANK ASSY IAW MM 52-34-031-4. OPS CHECK GOOD IAW MM 52-34-000-5.SDR FDEA200908263097Crank Assy · wornMCD LWR AFT LOCK ACT BS 615 ROD END BEARING HAS PLAY, CAM ACTUATOR FITTING CRACKED AND MISSING BOLTS. REMOVED AND REPLACED MCD LWR AFT HOOK AND CRANK ASSY IAW MM 52-34-031-4. OPS CHECK GOOD IAW MM 52-34-000-5.SDR FDEA200908203059Structure · damagedCRACK LWR CHORD RT WING INBD MIDFLAP INBD SIDE. REMOVED SEAL RETAINER FOR ACCESS IAW SRM 51-30-2, CUT-OUT DAMAGE ON RT WING INBD MID FLAP INBD SIDE IAW SRM 51-40-4 FIG 1, FABRICATED NEW PARTS IAW SRM 51-40-4. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2, ISDR FDEA200908183052Bracket · crackedLT WING NR 1 SLAT OB ACT ATTACH BRACKET INSIDE PLATE IS CRACKED. REMOVED OTBD AND INBD STEELS DOUBLERS AND WEBS AND FABRICATED WEB DOUBLERS IAW S/B 727-57-0130 AND EA NR 7-5750-126843 HEAT TREATED WEBS TO T6 CONDITION IAW FASI ENGINEERING REPORT NR 2-32153-80SDR FDEA200908183045Skin · damagedLT IB MIDFLAP LWR SURFACE WBL 85 HAS ELONGATED FASTENER HOLE. EVALUATED FASTENER HOLE FOUND TO BE OUT OF LIMITS IAW SRM 57-50-01. CUT-OUT DAMAGED AREA APPROX 1 INCH X .5 INCH IAW SRM 57-50-4 FIG 3 FAB REPAIR DOUBLER FROM 2024T3 .125 PO NR 290757Y DIM 13 INSDR FDEA200908183044Frame · gougedAFT CARGO COMPT. BS 1130 FRAME, PREVIOUS REPAIR DOUBLER IS GOUGED ABOVE STR 27R. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, FABRICATED ANGLE REPAIR FROM 7075 "O" .063 PO NR 9008655 DIM 12 INCH X 6 INCH IAW SRM 53-10-2, 51-30-5, 51-20-5 HEAT TREATED ANGLE FROMSDR FDEA200908183043Structure · crackedLT, IB. MIDFLAP T/E LWR CHORD, WBL 103 IS CRACKED ON IB CORNER. OPENED MID FLAP ACCESS PANEL IAW SRM 51-30-2, REMOVED LWR CHORD PREVIOUS REPAIR IAW SRM 51-30-2 FABRICATED NEW T/E LWR CHORD FROM BAC1503-100046 7075 PO NR 29057145 DIM: 49 INCHES IAW SRM 57-50-2SDR FDEA200908173053Angle · crackedCRACKED ANGLE CHORD AT NR 7 SPOILER BRACKET FALSE SPAR. REMOVED NR 7 SPOILER FITTING & SUPPORT, REMOVED DOUBLER, REMOVED DOOR STOP FITTING ON NR 7 SPOILER, TRIMMED OUT WEB DIM: 9.5 INCH, CUT OUT DAMAGE CHORD ANGLE SECTION, FABRICATED INBD WEB, FRABRICATED CHSDR FDEA200908163040Web · damagedAFT AIRSTAIR AREA- RT LWR TORQUE BOX LIGHTING HOLE IS ROUTED OUT BEYOND LIMITS. FABRICATED DOUBLER REPAIR IAW SRM 53-10-2 AND 51-40-2. ALODINE AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-40-3.SDR FDEA200908163042Door · crackedRT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT. REMOVED FASTENERS AND COVER PLATE AT RT MLG WING DOOR IAW SRM 51-30-2. FAB NEW COVER PLATED AND FILLER, MAT USED 2024 T3 .040 PO NR 9008655, DIMENSION 14.8750 INCH X 8.1250 INCH AND FILLER 10.3750 INCH X 5.750SDR FDEA200908163041Door · crackedLT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT. FABRICATED NEW SKIN AND DOUBLER FROM 2024T3 .040 PO NR 9008655 APPROX DIM: SKIN 5.5 INCH X 10 INCH, DOUBLER 13.5 X 8 INCH AND INSTALLED NEW SKIN AND DOUBLER AT LT MLG WING DOOR IAW SRM 51-30-2 DWG NR 65C27128.SDR FDEA200907092560Angle · crackedNR 4 SLAT AFT LOWER ANGLE IS CRACKED BELOW T-DUCT. REMOVED NR 4 SLAT INNER PANELS IAW SRM 51-30-2. REMOVED LOWER ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 57-50- 2. TREATED AND PRIMED. REPAIR PARTS IAW SRM 51-10-2 INSTALLED ANGLE IAW SRM 51-SDR FDEA200907072520Spar · crackedLT WING T/E FALSE SPAR, INBD END REPAIR DOUBLER IS CRACKED. WBL 118 REMOVED NR 7 SPOILER FITTING AND SUPPORT IAW SRM 51-30-2. REMOVED PREVIOUS DOUBLER, TRIMMED OUT WEB AND REMOVED PREVIOUS CHORD REPAIR IAW DWG SR 27-57-038 REV C. FABRICATED NEW WEB FROM 7
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