Boeing 727-247
Service difficulty reports · 2,669
Newest first. General aviation reporting is voluntary.
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 DL72E952458Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON SEAT TRACK AT RBL 45 BETWEEN STA 1070 AND 1090. REPAIRED SEAT TRACK AS PER SRM 53-10-5 FIG 7.SDR DL72E952457Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON SEAT TRACK RBL 56 FROM STA 344 TO 380. REPAIRED PER SRM 53-10-5 FIG 9.SDR DL72E952456Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON SEAT TRACK LBL 24 AT STA 380. REPAIRED BY REPLACING SEAT TRACK FROM STA 380 TO 400 PER SRM 53-10-5 FIG 7.SDR DL72E952880Skin · oil cannedOUTER SKIN OIL CANNING AND DENTED 58 INCHES FROM IB END. REPAIRED AS PER 57-50-03 FIG 1 AND IN REFERENCE TO ERA NR 271165-14 FOR NR 5 L/E SLAT, DURING SHOP INSPECTION.SDR DL72E952503Le Skin · damagedFOUND ON CV2 CHECK DAMAGE TO L/E SKIN OF NR 3 FOREFLAP O/B OF NR 5 FLAPTRACK. REPAIR: REPAIRED PER SRM 57-50-4.SDR DL72W952278Eel Battery · dischargedDURING PREFLIGHT CHECK, CABIN OVERHEAD EMERGENCY LIGHT AT FS 480 WERE FOUND INOP. REPLACED BATTERY, OPERATION NORMAL.SDR DL72E952879Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804.SDR DL72E952878Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIB NR 2 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804.SDR DL72E952877Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 12 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804.SDR DL72E952876Skin · dentedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E SKIN DENTED AT 36 FROM I/B END. REPAIRED PER SRM 57-50-1.SDR DL72E952874Ribs · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIBS NR 3 AND 4 CRACKED. REPAIRED PER SRM 57-50-4.SDR DL72E952329Eel Battery · dischargedDURING LAYOVER, FOUND FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACE RACK AND BATTERY. OPERATION NORMAL.SDR UPS203280Switch · inopWHILE IN C CHECK, MAINTENANCE FOUND CRACK ON LT WING, I/B MID FLAP, LWR T/E CHORD AT THE I/B AFT FLAP, I/B TRACK CUTOUT, I/B AFT FLAP ACTUATING MECHANISM CUTOUT AND THE AFT FLAP I/B CENTER TRACK CUTOUT. REPLACED CHORD PER SRM 51-30-2, 51-40-4, OHM20-50-01.SDR UPS203279Rib · crackedWHILE IN C CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT ACTUATOR ROD END SUPPORT RIBS, I/B AND O/B SIDES IN SLAT COVES. INSTALLED REPAIR PER SRM 51-30-2, MM27-80-00, OHM 20-50-01.SDR DL72E952875Le Skin · dentedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E OUTER SKIN DENTED. REPAIRED PER SRM 57-50-3 FIG 6.SDR DL72E952634Rib · crackedDURING SHOP INITIAL INSPECTION, CRACK FOUND ON THE O/B RIB OF THE O/B SLAT TRACK RIB. A REPAIR WAS INSTALLED PER THE M/M CHAPTER 57-54-00 FIG 814, FOR NR 5 SLAT.SDR UPS203267Te Wedge · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON T/E WEDGE, LT WING I/B IN FLAP. INSTALLED REPAIR PER SRM 51-30-2.SDR UPS203266Attach Rib · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT ACTUATOR ATTACH RIB, O/B SIDE. REPLACED RIB PER SRM 51-30-2, MM 27-81-32.SDR UPS203265Skin · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP, JUST ABOVE THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR B727-57-1361.SDR DL72E952164Fire Loop · shortedAFTER TAKOFF, NR 3 ENGINE B FAULT DETECTOR LIGHT CAME ON. COMPLIED WITH POM, APPROXIMATELY 15 MINUTES LATER B-LOOP ILLUMINATED, SHUTDOWN ENGINE AND DISCHARGED BOTH BOTTLES. INDICATION REMAINED UNTIL SHUTDOWN AT GATE. FOUND LOWER FIRE DETECTOR LOOP SHORTED. SDR DL72E952146Angle · crackedFOUND ON C2 LTR CK, NR 1 SLAT O/B STOP CASTING LOWER CHORD ANGLE CRACKED .25 INCH VISIBLE. REPAIRED LWR CHORD ANGLE PER M/M 57-54-0.SDR DL72E952144Le Rib · crackedFOUND ON C2 LTR CK, .5 INCH CRACK AT LEADING EDGE NOSE RIB ON 6 SLAT INBOARD OF ACTUATOR. REPAIR PER M/M 57-54-0.SDR DL72E952143Angle · crackedFOUND DURING C-2 LETTER CHECK, LWR COVE PANEL ATTACH ANGLE CRACKED NR 3 L/E SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0.SDR DL72E952142Clip · crackedFOUND DURING C-2 LETTER CHECK, SKIN CLIP CRACKED AT STA 1263 LT SIDE. REPAIRED PER MM 54-11-0 PG 825.SDR DL72E952595Angle · crackedDURING LETTER CHECK INSPECTION, THE RH TORQUE BOX FORWARD TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. ALSO, THE FWD TRANSVERSE BEAM WAS FOUND CRACKED. IN ACCORDANCE WITH B727 S/B 53-0129 REV 4, BOTH THE BEAM AND THE ANGLE WERE REPLACED.SDR DL72E952113Stringer · corrodedFOUND ON CV2 CK - CORROSION INSIDE STR 30 AFT OF SIDE STA 1010 JUST AFT OF FACTORY SPLICE - REPAIR - REPAIRED PER ERA 301748-14.SDR DL72E952112Clip · corrodedFOUND ON CV2 CK - CORROSION ON FUSELAGE FRAME TO SKIN ATTACH CLIP FWD SIDE STA 1010 BETWEEN STR 30/29R - REPAIR - REPLACED SKIN CLIP PER M/M 53-11-0.SDR DL72E952594Skin · corrodedDURING CORROSION VISIT INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1010, BETWEEN STRINGER 29L AND STRINGER 30. A 2.5 BY 2.5 CUTOUT IN THE SKIN WAS REQUIRED, STRINGER 30 WAS CUT AFT OF THE FACTORY SPLICE. BOTH DAMAGE LOCATIONS WILL BE REPAIREDSDR DL72E952082Flange · crackedFOUND ON A1 LTR CK, NR 7 SLAT CRACKED FLANGE TWO PLACES UNDER ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0 P 802.SDR DL72W952141Skin · wornLE SKIN WAS FOUND WORN APPOX 16 INCHES FROM IB END. DAMAGE WAS REPAIRED PER SRM 57574, BY INSTALLING A REPAIR DOUBLER. ALL THE ABOVE ACTION WAS DURING A SHOP VISIT, FOR NR 3 FORE FLAP.SDR DL72W952130Skin · corrodedDURING LETTER CHECK, FOUND LOWER FUSELAGE SKIN AT FS 720 BETWEEN STR 28L AND 28R WITH CORROSION DAMAGE THAT REQUIRED AN 8.5 INCH X 3 INCH SKIN CUT-OUT. AN EXTERNAL DOUBLER WAS INSTALLED PER DL ERA 301729-14 AD.SDR DL72E952593Skin · corrodedDURING CORROSION VISIT INSPECTION, THE LOWER FUSELAGE SKIN BETWEEN STA 700 TO 720 AND S-28L AND S-28R WAS FOUND TO HAVE CORROSION THAT REQUIRED A 33.0 BY 17.5 SKIN CUTOUT. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH AD 91-09-09, AND THE SDR DL72E952034Frame · crackedFOUND ON CV2 CHECK, FRAME CRACKED STA 720 5 INCHES ABOVE STRINGER 28L. REPAIRED PER SRM 53-10-4 FIG 26.SDR DL72E951982Balance Board · crackedFOUND ON CV-2 CHECK, .8125 CRACK AT LT INBD BALANCE BOARD ACCESS PANEL 9114. REPAIRED AS PER 55-10-3 FIG 3.SDR DL72W951988Skin · damagedFOUND ON B2 LTR CK, .75 BY .625 HOLE LOWER SKIN RT ELEVATOR AFT NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3.SDR DL72W951981Skin · crackedFOUND ON B-2 LETTER CHECK, .25 INCH CRACK VERTICAL STABILIZER EXTERIOR SKIN AT RT SIDE FWD OF ACCESS PANEL 9524 NR 2 ENGINE INTAKE COWL. REPAIRED PER SRM 54-30-01.SDR DL72W951980Web · crackedFOUND ON B-2 LETTER CHECK, .5 INCH CRACK TORQUE BOX VERTICAL WEB STA 1213 LT ABOVE AFT STAIRS STEPS CLOSE-OUT PANEL. REPAIRED PER M/M 53-11-0 PG 832.SDR DL72W951979Skin · crackedFOUND ON B-2 LETTER CHECK, .375 CRACK AT VERTICAL STABILIZER EXTERIOR SKIN RT SIDE STR 910 AT BASE OF VERTICAL. REPAIRED AS PER M/M 55-30-0 PG 801.SDR DL72W952321Skin · wornTHE LE WAS WORN 51 INCHES FROM THE I/B END. AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 57-50-4 FIG 1 DURING SHOP INSPECTION OF NR 2 FORE FLAP.SDR DL72W952319Skin · wornTHE LEADING EDGE HAD A WORN AREA APPROX 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE AREA WAS REPAIRED PER SRM 57-50-4 FIG 1, FOR NR 2 FLAP PANEL DURING SHOP INSPECTION.SDR DL72W951928Skin · crackedFUSELAGE SKIN CRACKED 1 INCH LONG STA 684 ONE INCH ABOVE STR 18R. CUT OUT SKIN DAMAGE 2.5 LONG BY 1.0625 WIDE, .5 INCH RAD TYP, USING THE SRM 53-30-3 PAGES 6 AND 7.SDR DL72W952320Skin · wornTRANSFER FROM N/R CARD NR 6348, THE L/E WAS WORN 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE WRONG TYPE OF RIVETS WERE INSTALLED ON THE ORIGINAL DOUBLER. CARD 6477 WAS ISSUED TO CORRECT THIS ACTION. THE REPAIR WAS PER SRM 57-50-4 FIG 1.SDR DL72E952032Splice · corrodedFOUND ON CV2 CHECK, CORROSION ON STRINGER SPLICE STR 26L AFT OF STA 480 FORMER. REPAIRED PER SRM 53-10-3 FIG. 1.SDR DL72E952008Clip · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD STA 700 INBD OF STR 28R W/W 257. REPAIRED PER M/M 53-11-0 PG 825.SDR DL72E952007Clip · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD OF STA 700 INBD OF STR 28L. REPAIRED PER M/M 53-10-0 PG 825.SDR DL72E952006Former · corrodedFOUND ON CV2 CHECK, CORROSION ON FORMER FWD SIDE STA 740 BETWEEN STR 28R TO 27R. REPAIRED FORMER PER M/M 53-11-0 FIG 826.SDR DL72E951984Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON I/B SEAT TRACK RBL 24 BETWEEN STA 400 AND ST 420. REPAIRED PER SRM 53-10-5 FIG 7.SDR DL72W951993Angle · crackedFOUND ON LTR CK, NR 8 SLAT ANGLE CRACKED JUST I/B OF I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.SDR DL72W951860Web · crackedFOUND DURING F-1 LETTER CHECK, 1.5 INCH CRACK AT MAIN ENTRY DOOR UPPER AFT CLOSE-OUT WEB. SPLICED IN NEW SECTION OF DOOR FRAME PER MM 52-11-1.SDR DL72W951856Skin · crackedFOUND DURING LETTER CHECK, FUSELAGE SKIN BULGED AND SKIN CRACKED EXTENDING FROM RIVET HOLES .0625 INCH 2 EA AT STA 530 AT FUSELAGE LAP JOINT STRINGER 26R. REPAIRED PER SRM 53-30-3.
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