Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 97FDEA00555Bellframe · dentedNR 0332 71C209-02 - FWD CARGO BS 660, STR 22-25 LEFT, BELLFRAME UPPER LEG DENTED 5 PLACES. INSTALLED DOUBLER AT BELLFRAME AT STA 660, STR 22-25 LEFT PER SRM 51-40-3.SDR 97FDEA00554Bellframe · dentedNR 0743 71C209-02 - FWD CARGO BS 540, STR 22-25 LEFT, 3 DENTS ON TOP SURFACE OF BELLFRAME. REPAIRED BELLFRAME AT STA 540, STR 22-25 LEFT IAW SRM 51-40-3 FIG 1.SDR 97FDEA00553Bellframe · dentedNR 0744 71C209-02 - FWD CARGO BS 520, STR 23-25 LEFT 6 DENTS ON TOP OF BELLFRAME. REPAIRED BELLFRAME PER SRM 51-40-3.SDR 97FDEA00552Bellframe · dentedNR 0746 71C203-02 - FWD CARGO BS 500 - 3 DENTS ON TOP SURFACE OF BELLFRAME STR 22-23 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3.SDR 97FDEA00551Bellframe · dentedNR 0326 71C209-02 - FWD CARGO BS 720, STR 23-24 LEFT BELLFRAME DENTED UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3.SDR 97FDEA00546Bellframe · dentedNR 0319, NR 0525 71C209-02 - FWD CARGO BS 720A, STR 24-25 RT: 2 DENTS IN TOP LEG OF BELLFRAME. DYE CHECKED DENTS, NO CRACKS FOUND PER BACOHM 20-20-02. INSTALLED REPAIR DOUBLER PER 51-40-3.SDR 97FDEA00506Frame · dented71C209-02 NR0330 - FOUND FWD CARGO BS 680, STR 23 - 24LT, HAS 3 DENTS IN UPPER LEG OF BELLFRAME. CUT OUT DAMAGED SECTION OF BELLFRAME, PER SRM 51-40-3, FIG 1. INSTALLED DOUBLER PER SRM 51-40-3.SDR 97FDEA00544Floorbeam · corrodedNR 0381 72C237-02 - CORROSION AT TOP OF UPPER LOBE FLOORBEAM STA 1070, RBL 55. REMOVED CORROSION PER SRM 51-10-6. INSTALLED FLOORBEAM REPAIR PER AARD 53-10-07-2 FIG 2.SDR 97FDEA00494Uplock Sensor · out of adjustAFTER TAKEOFF LEFT GEAR RED LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP POSITION. RECYCLED GEAR PER RED TABS, GEAR LIGHT REMAINED ON (RED LIGHT). GEAR DOOR LIGHTS (FIRST OFFICER'S AND SECOND OFFICER'S) SIDE PANEL OUT. FLEW TO IND WITH GEAR HANDLE IN USDR CA970806003Indicator · faulty(CAN) DURING CLIMB OUT, THE INBOARD FLAP POSITION INDICATOR FAILED TO MOVE WHEN FLAP WERE SELECTED FROM 5 DEGREES TO 2 DEGREES. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT INCIDENT. THE FAULT COULD NOT BE DUPLICATED DURING POST FLIGHT TROUBLESHOOTING. SDR 97FDEA00438Tailskid · damaged97-0133 TAILSKID DID NOT RETRACT AFTER TAKEOFF. CYCLING GEAR HAD NO EFFECT. REPLACED TAILSKID LOWER HOUSING WITH CARTRIDGE IN ACCORDANCE WITH MAINTENANCE MANUAL 32-71-00. FUNCTIONAL CHECKED OK IN ACCORDANCE WITH MAINTENANCE MANUAL 32-71-01.SDR 97FDEA00428Access Door · looseNR 2 ENGINE ACCESS DOOR LIGHT CAME ON DURING DEPARTURE ROLL. RELATCHED BOTTOM LATCH LIGHT WENT OUT. WIGGLED LATCH AND COULD NOT GET LIGHT AGAIN.SDR AALA971248Skin · corrodedTUL - OUTER SKIN OF NR 2 TANK CORRODED ABOVE PRIMARY HEAT EXCHANGE LT A/C BAY, 2 EACH PLACES. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER SRM 57-30-03. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971247Skin · corrodedTUL - OUTER SKIN OF NR 2 TANK CORRODED ABOVE PRIMARY HEAT EXCHANGE RIGHT A/C BAY IN PREVIOUSLY REWORKED AREA. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER SRM 57-30-03. TST: 55,772. CYCLES: 34,468. (X)SDR AALA971246Stringer · crackedTUL - STRINGER CRACKED STA 344, STR 5R. REPAIRED STRINGER IAW SRM 53-10-3, FIG 3, PAGES 5, 6, 7, AND 8. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971245Skin · gougedTUL - GOUGE IN SKIN STA 498 ABOVE STR 27L. INSTALLED REPAIR PER SRM 53-30-3. DOUBLER, TRIPLER, INCLUDING PREVIOUS REPAIR. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971244Skin · crackedTUL - THREE SMALL CRACKS IN FUSELAGE SKIN COMING OUT OF RIVET HOLE AT FS 1090 AND STR 1. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SB 727-53A0204 REV 3 DATED AUG 15, 1991. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971243Stringer · crackedTUL - BOTH ENDS OF STR 15L BUTTING UP TO ICE LIGHT CRACKED AT FASTENER BETWEEN BS 720B AND BS 720C. BOTH ENDS CRACKED PAST FIRST FASTENER. REMOVED ENDS OF STR 15L AT ICE LIGHT AND SPLICED IN NEW STRINGERS IAW SRM 53-10-3, FIG 1, PAGE 4B. TST: 55,772 HOURS.SDR AALA971241Beam · corrodedTUL - VERTICAL BEAM AT FS 1183, LBL 36, INBOARD SIDE, HAS .50 INCH CRACK IN AFT RADIUS AT WL 235. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 727-53-0192, REV 1, DATED MAY 30, 1991. TST: 55,772. CYCLES: 34,468. (X)`SDR AALA971240Stringer · crackedTUL - TOP 5TH, 6TH, AND 7TH AFT STRINGER TABS CRACKED AT THE BULKHEAD ATTACH BOLTS. STOP DRILLED AND REPAIRED PER BOEING SB 727-57A 159, 3 EACH PLACES. TST: 66,772 HOURS. CYCLES: 34,468. (X)SDR AALA971239Skin · corrodedTUL - WEB CORRODED AT TORQUE BOX OUTBOARD ATTACH POINT CASTING, LT SIDE WEB STA 289. INSTALLED DOUBLER PER SRM 53-10-9. TST: 56,772 HOURS. CYCLES: 34,468. (X)SDR AALA971238Casting · corrodedTUL - INBOARD AILERON QUADRANT CASTING CORRODED AROUND LOWER BUSHING. BOTH UPPER AND LOWER. REMOVED AND REPLACED QUADRANT. CORROSION BEYOND MANUAL LIMITS. TST: 56,772 HOURS. CYCLES: 34,468. (X)SDR AALA971237Casting · corrodedTUL - CASTING CORRODED LEFT SIDE OF STR 30 AT STA 950 ATTACH. REMOVED AND REPLACED CASTING, 51-10-1.SDR AALA971235Splice Plate · corrodedTUL - LEFT AFT WING SPLICE PLATE AT STA 870 HAS CORROSION IN 2 OUTER HOLES OF PLATE AND LOWER WING SKIN. REPLACED SPLICE PLATE AND RE-WORKED HOLES IN LOWER WING SKIN PER ESO 11697 DATED 6-24-97. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971234Stringer · corrodedTUL - CORROSION ON STR 22R INSULATION TIE DOWN STAND-OFF IN FRONT OF STA 720C. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3. TST: 55,772 HOURS. CYCLES: 34,468. (X)SDR AALA971233Stringer · corrodedTUL - STR 26R SHEAR TIES AND STRINGER CLIP CORRODED AT STA 1148. REMOVED DAMAGED AREA OF STRINGER AND SHEAR TIE, AND CLIPS. INSTALLED STRINGER REPAIR PER SRM 53-10-3, PAGE 4B. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971232Floor Beam · corrodedTUL - FLOOR BEAM CORRODED AROUND FASTENER HOLES, BOTTOM SIDE OF TOP FLANGE, STA 1110, LBL 21 INCHES TO BL ZERO INCH. REMOVED CORROSION, STA 1110 LBL 21, AND REPAIRED FLOOR BEAM IAW SRM 53-10-8, FIG 1. TREATED AND PRIMED. (X)SDR AALA971231Frame · corrodedTUL - LOWER 3 INCHES OF BELL FRAME CORRODED STA 372 INBOARD OF STR 17R (JUST FORWARD OF FORWARD GALLEY DOOR). REMOVED CORROSION AND REPAIRED PER SRM 51-40-4, LOWER 3 INCHES OF BELL FRAME ST STA 372, STR 17R. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971230Skin · corrodedTUL - CORROSION UNDER LEVELING COMPOUND AT SKIN LAP ABOVE STR 26R AND STA 680 TO STA 695. INSTALLED SKIN FILLERS AND DOUBLER PER SRM 53-30-3, REPLACED STRINGER AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPLACED INTERCOSTAL PER SRM 51-10-1. TST: 66,772 SDR AALA971228Stringer · corrodedTUL - STR 29L CORRODED AT BS 950 - BS 1007. CLEANED STRINGER, INSTALLED REPAIR STRAP PER ESO 11697 DATED 6-13-97 AT STA 950E TO STA 980, AND REPAIRED STRINGER PER SB 727-53-0179 FROM STA 980 TO STA 1007. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971227Shear Tie · corrodedTUL - SHEAR TIE CORRODED UNDER LEVELING COMPOUND AT INTERCOSTAL ALONG STR 26R, STA 550. INSTALLED MANUFACTURED PART PER SRM 51-10-1. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971226Intercostal · corrodedTUL - CORROSION ON WEB BETWEEN STA 540 - STA 560, STR 26R. REPLACED WEB WITH MANUFACTURED PART PER SRM 51-10-1. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971225Jamb · corrodedTUL - FORWARD EXTENSION OF LOWER DOOR JAMB WEB HAS DOUBLER ON WEB CORRODED OUT, INBOARD SIDE. REPLACED DOUBLER WITH MANUFACTURED PART PER SRM 51-10-1. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971224Angle · corrodedTUL - HEAVY CORROSION ON UPPER HORIZONTAL CHORD AT UPPER FORWARD CORNER OF RIGHT TRUNNION WELL BELOW WALKWAY WEB. REMOVED AND REPLACED CHORD ANGLE PER SRM 51-10-1. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971223Support · corrodedTUL - CORROSION IN U-CHANNEL SUPPORT FOR RT TRUNNION CASTING, STA 306. INSTALLED NEW U-CHANNEL SUPPORT FOR RT NOSE GEAR TRUNNION CASTING AT STA 306. TST: 55,772 HOURS. CYCLES, 34,468. (X)SDR AALA971222Stiffener · corrodedTUL - CORROSION AT UPPER NUTPLATE ON VERTICAL STIFFENER. REMOVED AND REPLACED CORRODED STIFFENER PER SRM 51-10-4, PAGE 4. TST: 53,888 HOURS. CYCLES, 34,468. (X)SDR 97FDEA00364Floorbeam · corrodedSTA 1070, RBL 24 CORROSION ON FWD LEG OF FLOORBEAM INBD SIDE OF TIE DOWN TRACK. CORROSION EXTEND BENEATH TRACK. REMOVED CORROSION PER SRM 51-10-6, CUT OUT AREA THAT WAS BEYOND LIMITS. REPAIRED FLOORBEAM PER AARD 53-10-07-2 SRM 53-10-07-2.SDR 97FDEA00327Floorbeam · corrodedNR 0604 71C205 00, UPPER CARGO; CORROSION ON FLOORBEAM AT STA 720A, BL 0 TO 25 LBL. CORROSION REMOVED AND ANGLE REPAIR INSTALLED PER SRM/AARD10H 53-10-07-2 FIG 2.SDR 97FDEA00296Floorbeam · corrodedNR 0260 CORROSION ON LOWER FLANGE OF UPPER LOBE FLOORBEAM AT STA 1070, RBL 26-30 IN AFT CARGO COMP. REMOVED CORRODED FLANGE AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8 AT STA 1070 FROM LBL 5 TO RBL 45.SDR 97FDEA00281Bleed Air Valve · malfunctionNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON DURING FLIGHT. ISOLATED TO FUSELAGE SIDE. FOUND NR 1 BLEED AIR VALVE LEAKING AIR DIRECTLY ON NR 1 STRUT OVERHEAT WARNING SYSTEM. REPLACED BOTH CLAMPS. LEAK CHECK NORMAL. OK FOR SERVICE.SDR 97FDEA00295Skin · crackedNR 0246 71C721-03 FUSELAGE SKIN DENTED AND CRACKED AT NR 2 LWR CARGO DOOR CUT OUT, IN THE LWR AFT CORNER, STA 984, BETWEEN STR 26R-27R. CUT OUT DAMAGE AND TRIMMED AREA. VISUALLY INSPECTED FOR CORROSION OF THE BONDED DOUBLER. NO CORROSION NOTED. FABRICATEDSDR 97FDEA00294Skin · crackedNR 1109 76C003-00 RT WING, OUTBD MID FLAP UPPER SKIN CRACKED, (3 EA.) AT INBD END OF FLAP, ABOVE REAR SPAR. HFEC'D MARKED ENDS OF CRACKS. CUT OUT DAMAGED AREA OF UPPER SKIN. FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 57-50-4, FIG 8.SDR 97ZZZM721Turbine Blade · failedDURING TAKEOFF FROM MIAMI, THE NR 3 ENGINE COMPRESSOR STALLED, THE ENGINE FAIL LIGHT ILLUMINATED. EPR WS 2.13, EGT WAS 595 DEGREES. THE CREW REDUCED POWER ON THE NR 3 ENGINE AND RETURNED TO MIAMI FOR AN UNEVENTFUL LANDING. AIRCRAFT WAS TWO ENGINE FERRIED FRSDR 97FDEA00268Retract Mech · malfunctionedLANDING GEAR LEVER FAILED TO RAISE PAST THE OFF POSITION AFTER TAKEOFF. LANDING GEAR LEVER LATCH/LIGHT CIRCUIT BREAKER WAS PULLED AND RESET IN ACCORDANCE WITH RED TABS AND LANDING GEAR WAS NORMALLY RAISED AFTER. INSTALLED GEAR PINS, OPERATED GEAR HANDLE SEVSDR 97ZZZM720Engine · malfunctionedDURING TAKEOFF FROM MIAMI, THE NR 3 ENGINE EGT WENT TO 595 DEGREES. THE CREW REDUCED POWER ON THE NR 3 ENGINE AND RETURNED TO MIAMI FOR AN UNEVENTFUL LANDING. MAINTENANCE IS TROUBLESHOOTING.SDR 97FDEA00255Pack · failedON DEPARTURE CLIMB-OUT, NOTICED NON ELECTRICAL BURNING SMELL/ODOR, NR 1 BLEED AND LEFT PACK OPEN AND ON. SELECTED LEFT NR 2 BLEED, ODOR CONTINUED. SELECTED LEFT PACK AND LEFT NR 2 BLEED. ODOR/SMELL ABATED, SELECTED RIGHT NR 2 BLEED AND DESELECTED NR 3 BLEEDSDR CA970527005Turbine Blade · failed(CAN) ON TAKEOFF ROLL THE #3 ENGINE DEVELOPED A SEVERE VIBRATION AND EGT INDICATION WAS AT THE RED LINE, THE TAKEOFF WAS ABORTED. PRELIMINARY INDICATIONS INDICATE A CATASTROPHIC FAILURE CAUSED BY A T1 DISC BLADE FAILURE APPROXIMATELY AT MID-FOIL. NOTE: E.C.M. SDR CA970520005Turbine Blade · failed(CAN) INSPECTION FOUND A T1 BLADE HAD FAILED.SDR 97FDEA00252Chord · corrodedNR 0149 010, CORROSION ON LONGITUDINAL BS 760-848, LBL 25, WL 208 UNDER NUTPLATES AND EMANATING UNDER TRACK. REMOVED AND REPLACED LONGITUDINAL BEAM BS 760-848, LBL 25, WL 208 PER FED-EX SRM 51-10-1 AND 51-30-2.SDR 97FDEA00250Stringer · dentedNR 0569 008 WHILE WORKING NR 0296, FOUND STRINGER TO BE DAMAGED OUT OF LIMITS BS 565, STR 28 LT. REMOVED AND REPLACED DAMAGED STRINGER 28 LT, BS 565 IAW FED-EX SRM 53-10-2, 53-10-3.
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