Boeing 727-233
Service difficulty reports · 3,034
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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 = '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 FDEA200812245281Shear Tie · damagedMISDRILLED STRINGER SHEAR TIE AT 9G BULKHEAD AND STR 12R REMOVED STR SHEAR TIE ON 9G BULKHEAD, STR12R IAW SRM 51-30-2. FABRICATED PART OF STRINGER TIE FROM 2024T3, 0.032 AND FRAME REPAIR PART FROM 7075O AND HEAT TREATED TO 7075T6 IAW SRM 51-20-1, 51-10-3 ANSDR FDEA200812245279Skin · dentedEXT FUSELAGE, SKIN DENTED AT STA 700 STR 24L FOUND DENT OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-10-2 FIG. 1 AND 53-30-2 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PASDR FDEA200812245278Channel · corrodedFWD CARGO CORROSION AT STR 27R AND STA 680 ON STRINGER CHANNEL REMOVED CORRODED CHANNEL IAW SRM 51-30-2. FABRICATED NEW CHANNEL IAW SRM 51-10-2. INSTALLED NEW CHANNEL AT FWD CARGO STRINGER 27R, STA 680 IAW SRM 51-30-2SDR FDEA200812245277Strap · corrodedFWD CARGO BAY CORROSION AT AFT OF STA 680, STR 26R TO STR 26L REPAIRED (REMOVED & REPLACED) TEAR STRAP AT FWD PIT STA 680 BETWEEN STR 26R AND 26L IAW DRAWING 65-56238 REV. B AND SRM 51-30-2.SDR FDEA200812245276Hinge · crackedEXTERIOR FUSELAGE AFT SEGMENT OF MCD HINGE, FUE SIDE, HAS A LOBE CRACKED STA. 680-720 REMOVED AFT SECTION MAIN CARGO DOOR HINGE IAW SRM 51-30-2. FABRICATED NEW HINGE IAW SRM 51-30-5 AND 51-10-1. TREATED AND PRIMED NEW HINGE IAW SRM 51-10-2. INSTALLED NEW MSDR FDEA200812245275Stringer Clip · damagedMISDRILLED STRINGER CLIP AT 9G BULKEAD, STR 4R REMOVED STRINGER CLIP ON 9G BULKHEAD STR 4R IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 53-10-4. FABRICATED PARTS OF STRINGER CLIP IAW SRM 51-20-1 AND 51-10-3. FABRICATED FRAME REPAIR PARTS AND HEAT TREATED IAWSDR FDEA200812245274Skin · dentedGOUGE AND DENT IN UPPER SURFACE SKIN OF LT ELEVATOR, O/B END OF CONTROL TAB CUTOUT, AT JOINT OF ELEVATOR T/E WEDGES. BLENDED AND SMOOTHED GOUGE AREA IAW SRM 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 55-20-3. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTASDR FDEA200812245273Web · crackedAFT AIRSTAIRS LT LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA 1203 AND STA. 1223 REMOVED PANEL AT AFT AIRSTAIRS LT VERTICAL WEB FOR ACCESS IAW SRM 51-30- 2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PARTSDR FDEA200812245270Web · crackedAFT AIRSTAIRS, RH LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA. 1203 AND STA 1223 REMOVED PANEL AT AFT AIRSTAIRS RH VERTICAL WEB FOR ACCESS IAW SRM 51-30-2 CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART ASDR FDEA200812245269Web · crackedAFT AIRSTAIRS, LT TORQUE BOX I/B VERTICAL WEB IS CRACKED AT BS.1225, WB 190 APROX REMOVED AFT AIRSTAIRS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART AND FILLER IAW SRM 53-10-2 FIG 6 ANSDR FDEA200812245280Frame · gougedGOUGED FRAME ON STA 580, STR 3L REMOVED FASTENERS IAW SRM 51-30-2, BLENDED OUT DAMAGE AREA IAW SRM 51-10-1. UT AREA IAW NDTM 51-00-00 FIG 2 PT 4. HFEC AREA IAW NDTM 51-00-00 FIG 23 PT 6. NO DEFECTS NOTED. FOUND TO BE OUT OF LIMITS IAW FDX SRM 53-10-1 FIG 1ASDR FDEA200812245268Indicator · failedASSYMETRIC OUTBOARD TRAILING EDGE FLAPS DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS 0. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR AND PERFORMED OPERATIONAL CHECK IAW AMM 27-52-021-2 ALL CHECK GOOD. OK FOR SERVICE. R/I FROM FACT PREMATURE REMOSDR FDEA200812215254Skin · bulgedSKIN BULGE STA 650 STR 29R. CUT OUT STR DAMAGE AND REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-30-1. CUTOUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER , FABRICATED STR REPAIR AND SPLICE, INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-30-3 AND 53-10-3.SDR FDEA200812195243Skin · bulgedEXTERIOR FUSELAGE SKIN BULGE SAT 185, STR 24L CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 14. FABRICATED REPAIR PART AND DOUBLER IAW SRM 53-30-3 FIG 14. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2.SDR FDEA200812195244Frame · corrodedCORROSION ON FRAME REPAIR 1070 AND 27L REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATE REPAIR PART, IAW SRM 53-10-2 FIG 5, AND 54-40-3 FIG 1. HEAT TREATED IAW ER 2-37153-801 REV A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW FRAME REPAIR IAW SRM 5SDR FDEA200812185225Skin · dentedDENT STA 720D, STR 18L. CUT OUT DAMAGED AREA DIM (1 7/8" X 7/8") IAW SRM 53-10-3 FIG 2. REMOVED FLOORBOARDS ROW "A" STA 720A TO 740 IAW SRM 51-30-2. FABRICATE REPAIR PARTS DOUBLER AND FILLER IAW SRM 53-30-2 FIG 2 AND 53-30-3 FIG 2. TREATED AND PRIMED IAW SRM 5SDR FDEA200812165177Skin · gougedPREVIOUS REPAIR AT BS 312 STR 24R HAS IMPROPERLY INSTALLED FASTENERS, AND FOUND GOUGES, AND TOOLING MARKS. REMOVED PREVIOUS REPAIR AT BS 312 STR 24R IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. CUT OUT DIMENSIONS 3.8" X 4.1". FABRICATED REPAIR FILSDR FDEA200812165176Sill · corrodedC-2 DOOR SILL CHORD O/B FLANGE CORRODED. REMOVED CORROSION PER B727 SRM 51-10-6 AND PERFORMED UT INSP OF AREA IAW NDTM 51-00-00 FIG 3 PART 4. (ORIG: .220 REMAIN : .170 LOSS: .050). REPORTED FINDINGS TO ENGINEERING AND EA 7-5310-126874 DATED 15 DEC 08 ISSUESDR FDEA200812165183Web · crackedAFT AIR STAIRS, LT LOWER TORQUE BOX INBD VERTICAL WEB IS CRACKED AT LIGHTNING HOLE BETWEEN STA 1263-1283. TRIMMED OUT DAMAGED AREA IAW SRM 51-40-2, FIG 1. FABRICATE REPAIR IAW SRM 51-40 -2 FIG 1, AND 53-10-2 FIG 6. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLSDR FDEA200812125129Skin · crackedSKIN BULGING AND CRACKED STA 1010 STR 27L CUT DAMAGE AREA IAW SRM 53-30-3 , FIG 3A. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3A. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.SDR FDEA200812125128Spar · crackedCRACKED CHORD FALSE SPAR UNDER NR 7 SPOILER FITTING. REMOVED LOWER SECTION OF CHORD IAW DRWG SR27-57-038 REV C AND FABRICATED NEW LOWER SECTION, 2 REPAIR ANGLES, 1 REPAIR STRAP, AND WEB IAW DWG SR27-57-038 REV C. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1SDR FDEA200812125127Spar · crackedFALSE SPAR CHORD CRACKED UNDER NR 8 SPOILER . TRIMMED INBRD WEB SECTION IAW DRAWING SR 27-57-038 REV C. TRIMMED LOWER STRUCTURE IAW DRAWING SR 27-57-038. LOCATED, DRILLED, DEBURRED LOWER ANGLE IAW 51-30-5 & DWG SR 27-57-038 REV C. FABRICATED 2 EA ANGLES ASDR FDEA200812045082Floorbeam · corrodedSTA 1166 FLOORBEAM, LOWER FLANGE CORRODED RBL 53-57 AT ADEL CLAMP. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS. REFERENCE SRM 53-10-8/ FIG 8. THIS IS CLASSIFIED AS A MAJOR REPSDR PCSA2008120301Blade · brokenAMERIJET FLIGHT SXM - SJU NUMBER ONE ENGINE VIBRATION FOLLOWED BY HIGH FUEL FLOW. PERFORMED A PRECAUTIONARY SHUTDOWN. MAINTENANCE DISCOVERED A BROKEN C2 BLADE AND COMPRESSOR DAMAGE.SDR FDEA200812025040Indicator · failedREJECTED T/O AT 90KTS DUE TO NO AIRSPEED INDICATION ON CAPT SIDE. REMOVE AND REPLACED CAPTAINS AIRSPEED INDICATOR. REMOVE AND REPLACED CAPTAINS AIRSPEED INDICATOR.SDR FDEA200810294619Fan · failedSLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING DESTINATION. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY LANDED AT RWY 9 WITH FIRE TRUCKS IN TOW. SDR 08FDEA04619Gasper Fan · malfunctionedAT FL 350 A SLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING MEMPHIS. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY AND LANDED. AT GATE SHUTDOWN ACFT SDR 08FDEA04554Skin · misrepairedREPAIR AT STA 440 STR 10L NOT IAW SRM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGED AREA DIMS 12" BY 9" IAW WITH EA 7-5330-126855 HFEC INSPECTED EDGE OF CUTOUT AND .040 INSURANCE CUT AND EXISTING HOLES FREE OF CRACK INDICATIONS IAW NDTM 51-00-00. FABRICATED DOSDR 08FDEA04380Skin · damagedCABIN STA 440 STR 10L HAS MIS-DRILLED FASTENER HOLES. CUT OUT DAMAGED AREA DIMS 2 INCH BY 7/8 INCH. FABRICATED DOUBLER USING 2024-T3 .090 PO NR 9007561 DIMS 12 5/8 BY 9 1/2 INCH, FILLER USING 2024-T3 .190 PO NR 314676 DIMS 2 INCH BY 7/8 INCH, IAW B727 SRM 53SDR 08FDEA04355Stringer Clip · crackedMAIN CABIN UPPER LOBE STA 680 STR 4L CLIP CRACKED REMOVED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. INSTALLED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA04354Stringer Clip · corrodedFWD PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 700, STR 26L, WL 153. REMOVED STRINGER CLIP, CORROSION ON CLIP WAS EXFOLIATED BEYOND REPAIR. FABRICATED, TREATED, AND PRIMED NEW CLIP, P/N 69-47375-2. INSTALLED CLIP REF SRM 51-30-2, PG 1-4/BOEING DWG NR 69-4SDR 08FDEA04340Structure · crackedCRACK ON AFT STRUCTURE OF RT INBD FLAP WBL 114.2 FABRICATED AFT STRUCTURE REPAIR FILLER, ANGLE SPLICE, INSTALLED REPAIR SPLICE AND FILLER ON RT INBD FLAP IAW SRM 57-50-2, SRM 51-40-4, AND SRM 51-30-2.SDR 08FDEA04309Stringer · corrodedCORROSION ON S29R AT BS 970-990. BLENDED OUT S29R FLANGE AS NECESSARY TO REMOVE CORROSION, REMAINING THICKNESS DIMENSIONS MAINTAIN A 20-1 BLENDOUT RATIO WITH A MIN 1.0: RADIUS PER MESSAGE 1-1013418906-2,3,4,5,6, AND ARE WITHIN LIMITS. ACCOMPLISHED HFEC AND SUSDR 08FDEA04308Lever · gougedLEFT AND RIGHT WHEEL WELL MLG DOOR RELEASE HANDLES ARE GOUGED. REWORKED GOUGED AREAS ON LH AND RH WHEEL WELL MLG DOOR REALEASE HANDLES IAW B727 SRM 51-10-1, PERFORMED DYE PENETRANT INSPECTION IAW SOPM 20-20-02 NO DEFECTS NOTED TREATED AND PRIMED AREAS. ALLSDR 08FDEA04304Spar · crackedCRACK ON WING CENTER SECTION REAR SPAR WEB STA 870 LBL 13 TO 16.SDR 08FDEA04292Frame · chafed9G BULKHEAD CONTACTING FRAME AT STA 344 AND STR 5L. TRIMMED OUT FRAME AND FABRICATED FRAME REPAIR, INSTALLED FRAME REPAIR IAW B727 SRM 51-30-2, 53-10-2 FIG 3 AND SRM 53-10-4 FIG2.SDR 08FDEA04280Web · damagedAFT AIRSTAIR AREA LT LOWER TORQUE BOX HAS IMPROPER REPAIR AT LIGHTNING HOLE BS 1240. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-40-2, FABRICATED DOUBLER REPAIR IAW SRM 51-30-5, 53-10-2 AND 51-40-2, INSTALLED REPAIR IAW SRM SDR 08FDEA04271Seat Track · corrodedCORROSION ON SEAT TRACK STA 1060 TO 1090 RBL 45. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 1040 TO 1130 RBL 45 IAW SRM 51-30-2, FABRICATED SECTION OF SEAT TRACK IAW SRM 53-10-5, INSTALLED NEW SEAT TRACK IAW SRM 53-10-5.SDR FDEA200810074263Transmitter · failedNR 1 ENG SHUTDOWN IN FLIGHT FOR HIGH OIL PRESSURE (60 PSI) IAW QRH. WINDMILLED FOR 15 MINUTES IN GREEN BAND AND BELOW. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER BOEING MM 79-33-001-4 RAN ENGINE FOR LEAK CHECK AND PRESSURE CHECKS. CHECK OIL PRESSURE SDR 08FDEA04263Transmitter · failedNR 1 ENGINE SHUTDOWN INFLT FOR HIGH OIL PRESSURE (60 PSI) IAW QRH. WINDMILLED FOR 15 MINUTES IN GREEN BAND AND BELOW. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER MM 79-33-001-4. RAN ENGINE FOR LEAK AND PRESSURE CHECKS. CHECK OIL PRESSURE WITH DIRECT SDR 08FDEA04257Seat Track · wornWORN SEAT TRACK RBL 45 STA 1130. REMOVED SEAT TRACK, 2 EACH DOUBLERS AND BEAM EXTENSION, FOUND DAMAGED AREA ON WEB, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-30-2 AND 51-40-2 FABRICATED WEB FILLER, 2 STRAPS, BEAM EXTENSION, BEAM STRAP AND EXTENSION SUPPORT FILSDR 08FDEA04237Skin · gougedSKIN GOUGED BS 990 S24L. BLENDED OUT AREA AND FOUND MATERIAL LOSS OUT OF LIMITS. CUT OUT DAMAGED AREA IAW SRM 53-30-3, FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 AND 53-30-3. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2.SDR 08FDEA04245Skin · gougedSKIN SCRATCHED BELOW COOLING BLOWER STATIC PORT RT FWD FUSELAGE BS 435 ABOVE S21R. BLENDED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLERS IAW SRM 53-30-3, INSTALLED REPAIR PARTS IAW SRM 53-30-3.SDR 08FDEA04241Seat Track · corrodedCORROSION ON SEAT TRACK ON INBD VERTICAL SIDE FWD OF BS 1070 RBL 25. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SEAT TRACK FROM BS 950 TO 1134 RBL 25, FABRICATED 2 SEAT TRACK SECTIONS, 4 ANGLE SPLICES, 2 STRAPS AND IAW SRM 53-10-5. INSTALLED REPAIR PARTS ISDR 08FDEA04240Skin · misalignedCARGO DOOR SKIN AT BS 650 S25L HAS 2 FASTENERS WITH NOT ENOUGH SPACING. CUT OUT DAMAGED STRINGER AT BS 650 AND S25L , FABRICATED STRINGER REPAIR SPLICE FABRICATED FILLER, CUT OUT DAMAGED EXT SKIN DIMS .755" FABRICATED FREEZE PLUG, FABRICATED EXT SKIN DOUBLERSDR 08FDEA04242Seat Track · corrodedCORROSION ON SEAT TRACK LBL 25 BS 560-720. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATED 2 SECTIONS, SPLICE ANGLELS AND 2 STRAPS IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW SRM 53-10-5.SDR 08FDEA04239Structure · crackedLEFT WING INBD MIDFLAP CRACKED 2 PLACES AT CUTOUTS. REMOVED DAMAGED AREA AND FABRICATED NEW ANGLES AND SPLICE REPAIR IAW SRM 57-50-2 AND 51-40-4. INSTALLED REPAIR PARTS IAW SRM 51-30-2.SDR 08FDEA04238Skin · gougedSKIN GOUGED STA 700 STR 28R. CUT OUT DAMAGED SKIN AND FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, 53-30-2 AND SRM 51-30-2.SDR PCSA2008093001Actuator · leakingLOST A HYDR SYS AFTER FLAP RETRACTION DEPARTING. ON APPROACH TO POS NR 7 L/E SLAT FAILED TO EXTEND. LANDING GEARS WERE EXTENDED MANUALLY, THE AC LANDED SAFELY AND WAS TOWED FROM THE RUNWAY. MAINT DISCOVERED THE NR 7 L/E ACTUATOR BODY HAD FAILED CAUSING A LOSSDR 08FDEA03984Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1765 AND STA 1785, LBL 106. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00. FABRICATED CHANNEL IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21- 01. INSTALLED CHANNEL REPAI
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