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.
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
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 DL72W990147Frame · dentedBS 1030 FRAME I/B OF LBL 40 WAS FOUND DENTED AT THE TOP AND EXCEEDED SRM ALLOWABLE LIMITS. A CUT OUT WAS NECESSARY. REPAIRED PER ERA 332661-14SDR DL72W990145Skin · corrodedSKIN WAS FOUND CORRODED AND THREE ADDITIONAL REPAIRS REMOVED AND ALL DAMAGE INCORPORATED INTO ONE REPAIR. DAMAGE IS LOCATED AT BS 673, S28L. REPAIRED PER ERA 303790-14, REV C.SDR DL72W990144Bulkhead Web · crackedBS 178 BULKHEAD WAS FOUND WITH CRACKS IN THE TYP LOCATIONS AS SHOWN IN THE BACO SRM 53-10-9, FIGURE 14. ADDITIONAL CRACK FOUND OUTSIDE THE TYP LOCATION. REPAIRED PER ERA 332712-14.SDR DL72W990143Stringer · damagedWEAR WAS FOUND ON THE S7L ON THE VERT STAB. DAMAGE IS TO THE O/B SURFACE OF THE UPPER FLANGE AT APPROX FIN STA 230. REPAIRED PER ERA 332689-14.SDR DL72W990142Spar Chord · crackedTHE FRONT SPAR CHORD WAS FOUND WITH CRACKS IN THE FWD FLANGE AT A FASTENER HOLE AT APPROX WS 333. REPAIRED PER ERA 332687-14.SDR DL72W990141Frame · misdrilledMTC DISCOVERED TWO MISDRILLED HOLES IN THE I/B CHORD OF THE BS 560 FRAME NEAR S27R. REPAIRED PER ERA 332713-14.SDR DL72W990140Skin · crackedFOUR HOLES WERE DISCOVERED CRACKED IN THE SKIN AT BS 940. THE HOLES WERE O/S THRU THE SKIN, STRINGER (18A) AND FITTING. FINAL HOLES ARE SHOWN ON FIGURE 1 OF ERA 332686-14. REPAIRED PER ERA 332686-14.SDR DL72W990081Connector · dirtyOUTBOARD FLAPS INDICATED ONLY 1 DEG. WHEN FLAPS LEVER WAS AT FIVE. POSITIONED FLAP LEVER BACK UP. FOLLOWED POM PROCEDURE FOR TRAILING EDGE O/B FLAP MALFUNCTION. BROKE SAFETY WIRES ON GPWS AND ALTERNATE FLAP SWITCH. TRIED O/B FLAP INDICATOR NO HELP. CLEANESDR DL72W990051Circuit Breaker · trippedAFT GALLEY FORWARD COFFEEMAKER HAD MILD ELECTRICAL BURNT SMELL. TURNED OFF GALLEY POWER AND PULLED AFT GALLEY C/B. SMELL DISSIPATED. MTC FOUND COFFEEMAKER INTERNAL C/B POPPED. REPLACED SAME, ALL CHECKS NORMAL.SDR UPS99228327Light · inopINSPECTION TYPE:N/A E/E/L INOP BY CREW ENTRY DOOR R/R FWD E/E/L WITH ROBBED PART FROM A/C 910 OPS CHECK GOOD. S/N ON 2841-8 S/N OFF 6508SDR DL72W990036Trunnion · corrodedAT MV2 FOUND BOLT BORE CORRODED LT TRUNNION CAP FWD BORE NLG. REMOVED HOLE TO .892 TO REMOVE CORROSION PER MM 53-40-0, OK TREAT/PAINT HOLE.SDR DL72W990035Trunnion · corrodedFOUND AT MV2 BOLT BORE, CORROSION RT NLG TRUNNION CAP FWD BORE. REAMED HOLE TO 0907 TO REMOVE CORROSION PER MM 53-40-00 TREAT/PAINT.SDR DL72W990026Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A CRACK AT WL 169 AND RBL 25. THE CRACK WAS REPAIRED WITH A DOUBLER ON A TIME LIMITED BASIS UNTIL THE FULL BAC S/B 727-53-0215 IS ACCOMPLISHED AT NEXT HMV. THE REPAIR WAS ACCOMPLISHED PER ER/A 366415-14.SDR 98FDEA00768Shear Tie · corrodedCORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 520, STR 27-28 RT. *S/D* REMOVED AND REPLACED SHEAR TIE BS 520, STR 27-28R IAW FEDEX 51-30-2 AND DWG NR 65-15929.SDR DL72W982652Bolt · missingON APPROACH, LEADING EDGE FLAP NR 3 UNSAFE HAD AMBER LIGHT, ON GO-AROUND FLAPS WENT GREEN. SAFE INDICATION ON LANDING. AFTER LANDING FLAPS TO 25 DEGREES, FLAP INDICATION WENT TO AMBER. FOUND ACTUATOR DISCONNECTED FROM FLAP, BOLT MISSING. DAMAGE TO FLAP COSDR DL72W982637Skin · crackedTHE UPPER FUSE SKIN AT BS 351 ON THE UPPER ROW OF THE S24R LAP SPLICE WAS FOUND CRACKED. THE CRACK EXTENDED THRU THREE CONSECUTIVE FASTENERS WITH A TOTAL LENGTH OF 3. REPAIRED PER ERA 366371-14.SDR DL72E982643Battery Pack · dischargedEMERG EXIT LIGHT SIGN ON FACE OF LIFE RAFT COMPARTMENT, MAIN CABIN INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK.SDR DL72W982611Skin · corrodedFUSELAGE SKIN, FS 660-681 STRINGER 26R, REPAIR FOR CORROSION AT SKIN LAP. THE UPPER SKIN AT THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH CORROSION BETWEEN FS 660-665. THE SKIN WAS CUTOUT OVER A 4 BY 4 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS ADJACENTSDR 98FDEA00756Stringer · corrodedCORROSON ON STR 28L, BS 580. *S/D* REPAIRED STRINGER 28L AT BS 580 PER FEDEX SRM 53-10-3.SDR DL72W982587Battery Pack · dischargedLEFT AFT EMERGENCY OVERWING LIGHT INOP IN CABIN. REPLACED BATTERY RACK M1090, CKS OK.SDR DL72W990068Angle · corrodedCORROSION ON SECONDARY HEAT EXCHANGER CLOSE OUT PANEL ATTACH ANGLE LT SIDE I/B ANGLE. INSTALLED REPAIR PER MM 53-30-1.SDR 98FDEA00747Clip · corrodedCORROSION (C53-224-03-1/2) ON STRINGER CLIP STR 26L, BS 440 (MARKED). *S/D* REMOVED AND REPLACED WITH NEW CLIP TO FRAME, NEW STR CLIP WAS INSTALLED IAW FEDEX SRM 51-10-1, 51-30-2 AND FEDEX MM 51-20-0.SDR DL72W990042Angle · crackedA 2 INCH VISIBLE CRACK RT LOWER TORQUE BOX SUPPORT ANGLE BELOW AIRSTAIR ACTUATOR ATTACH FITTING STA 1263 RT (MARKED). REPLACED PART PER SRM 53-10-10.SDR DL72W982645Rib · crackedFOUND DURING MV2/F-1 LETTER CHECK, .75 INCH CRACK AT NR 2 SLAT NOSE RIB O/B SIDE OF ACTUATOR AT AFT LWR CORNER. REPAIRED PER M/M 57-54-0.SDR DL72W982589Rib · crackedFOUND DURING MV2/F 1 LETTER CHECK, .75 INCH CRACK AT NR 3 SLAT NOSE RIB O/B SIDE OF ACTUATOR AFT LWR CORNER. REPAIRED PER M/M 57-54-0.SDR 98FDEA00748Beam · corrodedWHILE WORKING FEDEX EO NR 7-5300-7-2305 L3 PT 2 CORROSION ON G-BEAM BS 268, LBL 3, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM BS 26.75, LBL 8 TO RBL 18, WL 208 IAW FEDEX DWG 65-17593 AND FEDEX SRM 51-30-2, 53-10-1.SDR 98FDEA00745Skin · corrodedNR 0167 - CORROSION (C53-224-05) WING CTR SECTION UPPER SKIN, UPPER SURFACE BS 760, RBL 65, WL 204. REMOVED AND REPLACED CORROSION AT BS 758, RBL 62.64, WL 204 UP TO .039 OF MATERIAL IN A 1 BY 1 AREA. UPPER SKIN WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 57SDR 98FDEA00743Shear Tie · corrodedNR 581 CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 720F, LBL 9, WL 149. *S/D* REMOVED AND REPLACED SHEAR TIE BS 720F, LBL 9, WL 149 IAW FEDEX SRM 53-10-4 FIG 15.SDR DL72W982656Bulkhead Angle · crackedREF NR 214, 215, 216, 217, 218 AND 219 REPAIRED STA 178 BLKHD AND REPLACED UPPER AND LWR ANGLES PER SRM 53-10-9 FIG 14. COMPLETED AND FORWARDED DATA RETRIEVAL.SDR DL72W982556Battery Pack · dischargedEMERG EXIT LIGHT ABOVE L1 DOOR WEAK DURING TEST. REPLACED BATTERY PACK.SDR 98FDEA00741Skin · crackedNR 369 FCD INNER SKIN IS CRACKED 8 INCHES FWD OF AFT FRAME 1 INCH ABOVE NR 3 TRANSVERSE BEAM. *S/D* REMOVED DAMAGE AT FCD INNER SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 52-00-3 FIG 3.SDR 98FDEA00738Frame · crackedNR 564 - AFT CARGO BAY BS 970 FRAME IS CRACKED AT STR 26L. REMOVED AND REPLACED FLOOR SIDEWALL SUPT AT BS 950C TO BS 1000, LBL 24, WL 146 IAW FEDEX SRM 51-30-2. REPAIRED FRAME. AFT CARGO BAY PER FEDEX SRM 51-40-3.SDR 98FDEA00737Chord · corrodedNR 186 - CORROSION C53-224-08 ON 1176, REINFORCEMENT CHORD LBL 56-LBL 16 AND CORROSION AND MECHANICAL DAMAGE RBL 24-LBL 18, WL 208, BS 1176. REMOVED AND REPLACED CORROSION PER FEDEX 727 SRM 53-10-1, 51-10-2, 51-10-6, 57-30-2 AND FEDEX MM 57-20-151.SDR 98FDEA00736Floorbeam · corrodedNR 195 - WHILE WORKING NR 195, FOUND CORROSION ON BS 1130 FLOORBEAM RBL 22-30, WL 208. REPAIRED FLOORBEAM IAW FEDEX EA NR 7-5310-43176A.SDR 98FDEA00735Stringer · dentedNR 145 BS 380+9 STR 24 RT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE, FAB, ALODINED, PRIMED AND INSTALLED REPAIR PER FEDEX MM 51-20-151 AND FEDEX SRM 53-10-3, FEDEX EA NR 7-5310-43150.SDR 98FDEA00734Floorbeam · corrodedNR 187 CORROSION C53-224-04 ON FLOORBEAM UPPER CHORD BS 1110, LBL 11 TO RBL 43, WL 208. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED ALODINED, PRIMED, PAINTED AND INSTALL FLOORBEAM SEGMENT AND REPAIR PARTS IAW FEDEX SRM 53-10-8, 51-30-2 AND FEDEX MM 51-20-151SDR 98FDEA00733Frame · corrodedNR 163 CORROSION C53-113-01(2) AFT CARGO BAY STUB FRAME AT BS 950E+6 STR 29R. REMOVED AND REPLACED AFT CARGO BAY STUB FRAME IAW FEDEX SRM 51-30-2 AND FEDEX DWG 65-56129.SDR 98FDEA00732Stringer · damagedNR 144 BS 380+12, STR 23 LT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REPAIRED STR IAW FEDEX SRM 53-10-3, FEDEX EA 7-5310-43152.SDR 98FDEA00731Shear Tie · corrodedCORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 380, LBL 4 RBL 4, WL 148. *S/D* REMOVED AND REPLACED SHEAR TIE BS 580 IAW FEDEX SRM 53-10-4, DWG 65-15932.SDR DL72E982492Web · crackedREF SHIP 576 TPA LTR CHK C2 12-03-98, .25 INCH CRACK IN TORQUE BOX VERT WEB RT SIDE STA 1243, .5 INCH CRACK IN TORQUE BOX VERT WEB LT SIDE STA 1323. REPAIRED BOTH ITEMS PER MM 53-11-0.SDR DL72W982475Skin · corrodedFUSELAGE SKIN FS 720A-720B, STRINGER 27R-28R. REPAIR FOR CORROSION CUTOUT. THE FUSLAGE SKIN WAS FOUND CORRODED BETWEEN FS 720A AND FS 720B BETWEEN STRINGERS 27R AND 28R. THE CORROSION WAS REMOVED WITH A 3 BY 3.75 CUTOUT AND A 7.5 BY 3 CUTOUT. THE CUTOUTS WSDR DL72W982474Fitting · crackedFUSELAGE RT STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG FITTING AREA WAS INSPECTED PER BAC S/B 727-53-0141. CORROSION AND CRACK INDICATIONS WERE FOUND IN THE FITTING, STRINGER, AND SKIN. THE DAMAGED AREA OF SKIN WAS CUTOUT ANDSDR DL72W982473Fitting · crackedFUSELAGE STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG ATTACH FITTING WAS INSPECTED PER BAC S/B727-53-0141 (LT SIDE). TWO FASTENER HOLES COMMON TO STRINGER 18-A WERE FOUND TO HAVE CRACK INDICATIONS. THE HOLES WERE OVERSIZED TO REMSDR DL72W982445Actuator · damagedNR 3 L/E SLAT ACTUATOR CASE FAILURE, RESULTING IN LOSS OF A-SYS HYD POWER. REPLACED ACTUATOR.SDR DL72W982411Battery Pack · dischargedON L/O, FOUND INTERNAL OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK, EMERGENCY LIGHTS NOW CHECK NORMAL PER M/M.SDR UPS98228229Fuel Pump · failedINSPECTION TYPE-N/A, CLIMBING OUT OF 700 FT AGL NR 1 ENGINE FAILED. CHECKLIST RUN ENGINE WAS IN RESTART ENVELOPE, RESTART ATTEMPT UNSUCCESSFUL OIL PRESS AND INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 FUEL CONTROL AND FUEL PUMP PER MM 73-21-1 AND 73-11-1, SDR DL72W982434Panel · punctureFOUND DURING MV2 CORROSION VISIT NRC 330, HOLE IN LT ELEVATOR BALANCE BOARD ACCESS PANEL NR 9119. REPAIRED PER SRM 55-20-3 FIG 1.SDR DL72E982394Battery Pack · dischargedLT CTR OVERWING EMER LIGHT INOP. REPLACED BULB AND BATT PACK, NO HELP. REPLACED CHARGING RACK, CKS OK.SDR DL72W982373Battery Pack · dischargedRT WING FWD EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK.SDR DL72W982368Angle · crackedFOUND ON D2 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT THE I/B STOP PAD. REPAIRED PER MM 57-54-0.
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