Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 06FDEA0342Skin · misdrilledDOUBLE DRILLED HOLE AT NUT PLATE IN LOWER SKIN OF LEFT WING BULLNOSE 9 INCHES I/B OF NR 3 SLAT O/B SLAT TRACK. *S/D* REPAIRED LOWER SKIN OF LEFT WING BULLNOSE IAW EA 7-5710-91433.SDR 06FDEA0341Fitting · gougedWHILE WORKING N01382 FOUND NUMEROUS NICKS AND GOUGES IN RT 870 TERMINAL FITTING INNER BORE. *S/D* ACCOMPLISHED EA 7-5710-96554.SDR 06FDEA0345Repair · misinstalledEXISTING REPAIR ON NR 3 CARGO DOORFWD TO AFT EDGE EXTERNAL SKIN DOES NOT COMPLY WITH EXISTING FAA DATA. REMOVED OLD DOUBLER AND DAMAGED SKIN IWA SRM 51-30-2 & 52-00-3 FIG3 INSTALLED REPAIR PARTS IAW SRM 51-30-2. REINSTALLED REMOVED FOR ACCESS IAW SRM 51-30-2SDR 06FDEA0344Skin · chafedRT WING FIXED TRAILING EDGE HAS CHAFE MARK AND SPOTS OF GOUGES FROM WS 224.5 TO WS 625.0 (SKIN UNDER FWD END OF SPOILER.) FABRICATED AND INSTALLED NEW STRAPS IAW SRM 57-30-2 REPLACEMENT PARTS FABRICATED ON TRAVELERS T5/564670,T5/564665,T5/564668,T5/564644,SDR 06FDEA0343Flange · wornAFT LWR. FUSELAGE FLANGE FOR NR 2 ENG LWR COWLING FWD EDGE CONTACT IS WORN. REMOVED AREA OF DAMAGE SRM51-10-01 &51-30-2.FABRICATED REPLACEMENT STRUCTURE P/N 65-23687-21 & SPLICE PARTS FABRICATED ON TRAVELER T5/565148. LOCATED DRILLED AND INSTALLED IAW SRM 51SDR 06FDEA0319Stringer · crackedSTA 720B PLUS 3 STR 15R CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3.SDR 06FDEA0318Stringer · crackedSTA 720B PLUS 3, STR 15L CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3SDR 06FDEA0317Housing · crackedFWD CARGO COMPT CEILING LIGHT HOUSING CRACKED IN SEVERAL PLACES AT BS 608 LBL 32 WL 202. REMOVED AND REPLACED FWD CARGO COMPT. CEILING LIGHT HOUSING AT BS 608 LBL 32 WL 202. IAW IPC 33-30-00-02.SDR 06FDEA0316Repair · mismanufacturedDOUBLER REPAIR AT FLOOR SUPPORT STRUCTURE STA 577 TO 595 LBL 9.00 LWR FWD CABIN REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED DOUBLER REPAIR AT FLOOR SUPPORT STRUCTURE BS 577-595SDR 06FDEA0315Beam · corrodedWHILE WORKING FEDEX WORK CARD S00004 FOUND CORRODED T/E PANEL ATTACH BOLT HOLES IN THE MLG BEAM, 14 EA ON THE AFT SIDE OF THE BEAM AND 12 EA ON THE FWD SIDE. REPAIRED RT MLG BEAM T/E PANEL ATTACH BOLT HOLES IAW FED EX SR27-57-012 REV A.SDR 06FDEA0314Skin · corrodedWHILE WORKING CARD N00378 FOUND CORROSION ON SKIN AT BS 720F TO 740 BETWEEN STRINGER 2 LT TO 3 RT. ACCOMPLISHED REPAIR AT B.S. 720F TO 740 BETWEEN STRINGERS 2L TO 3R IAW FED EX EA 7-5330-96543.SDR 06FDEA0313Shroud · corrodedBS 1070, WL 205 WHILE WORKING CUSTOMER CARD N00935 FOUND CORROSION ON OUTBOARD SIDE OF FUEL LINE SHROUD BS 1070 RBL 60 WL 205. REPAIRED FUEL LINE SHROUD AT BS 1070 RBL 60 WL 205 IAW FED-EX E.A. 7-2822-96553.SDR 06FDEA0312Skin · crackedVERTICAL FIN SKIN HAS POSSIBLE CRACK RT SIDE STR 10 ABOVE BODY TORQUE BOX BS 1342. REPAIRED RT VERTICAL FIN SKIN PER FED-EX E.A. 7-5540-96829.SDR 06FDEA0310Wire · corrodedPDIS 262 26-12 0007718 20JAN06 AFW OPEN R LOGPAGES: 01310127 MAIN CARGO SMOKE ZONE 5 LIGHT AND MASTER FIRE WARNING LIGHTS CAME ON PASSING 5000FT IN CLIMB AND ON TOUCHDOWN. BLEW OUT LINE FROM NR 5 DETECTION UNIT LINE AFT FOR DE BRIS. NOTHING NOTICABLSDR 06FDEA0309Actuator · weakNR 2 LE FLAP WOULD NOT RETRACT WITH FLAPS SELECTED UP. INSPECTED IND SWITCH AND LINKAGE NO DEFECTS NOTED. OPS CHECK SEVERAL TIMES AND ALL IND WERE NORMAL.CREW NOTED THAT SYSTEM WORKED CORRECTLY INITIALLY BUT THAN GOT YELLOW FLICKER. ALSO FLIGHT CREW INDSDR 06FDEA0303Floorbeam · corrodedN00441 CORROSION (C53-111-01) ON FLOORBEAM LWR FLANGE BS 720 LBL30-RBL37. ** SD ** COMING ALL WORK TO BE DONE ON CUSTOMER ID #N01427SDR 06FDEA0301Skin · chafedEXTERNAL FUSELAGE, BS 980-990, S24L, SKIN CHAFED BY FAIRING. REPAIRED SKIN CHAFF AT BS 980-990 S24L IAW SRM 53-30-1, 53-30-3.SDR 06FDEA0300Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED BS 220 WL 218 LT SIDE. REPAIRED PER SRM 53-30-3, 53-30-1, 53-30-2, MAJOR REPAIRSDR 06FDEA0307Beam · damagedWHILE WORKING CARD N01210 (TAIL 5142), FOUND VERTICAL FIN T/E BEAM, UPPER SPICE FITTINGS, 8 EA I/B BUSHINGS WORN. REPAIRED VERTICAL FIN T/E BEAM IAW FED-EX EA 7-5530-96556.SDR 06FDEA0306Beam · damagedWHILE WORKING CARD N01209, FOUND VERTICAL FIN UPPER SPLICE BEAM, BUSHING BORE OVERSIZED & GOUGED. REPAIRED VERT. FIN UPPER SPLICE BEAM BUSHING BORE IAW EA 7-5530-96537.SDR 06FDEA0305Tie · misalignedFOUND THE AFT VERTICAL BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING TO BE MISALIGNED. REPAIRED THE AFT VERT. BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING IAW EA 7- 5530-96550.SDR 06FDEA0302Trunnion · misdrilledNLG RT TRUNNION SUPPORT FITTING FWD LOWER HOLE HAS MISDRILLED HOLE. REPAIRED NLG RT TRUNNION SUPPORT FITTING IAW FED EX EA 7-5310-96601.SDR 06FDEA0299Skin · corrodedCORROSION ON FUSELAGE SKIN FROM BS 681 - 740 STRINGER 4 LT TO STRINGER 4 RT. REPLACED SKIN PANEL PER SRM 51-30-2. (CLOSED)SDR 06FDEA0276Panel · crackedPANEL 9220 IS CRACKED. *S/D* REPLACED PANEL PER FED EX EA 7-5510-96548.SDR 06FDEA0275Web · chafedRIGHT ELEVATOR NR 1 BALANCE PANEL BAY I/B WEB IS CHAFED. *S/D* REMOVED AND REPLACED WEB PER FED EX EA 7-5510-96545.SDR 06FDEA0285Frame · dentedFRAME DENTED BS 680 STR 25 RIGHT. REPAIRED FRAME AT BS 680 STR 25RT IAW SRM 51-40-3.SDR 06FDEA0284Tear Strap · mismanufacturedBS 640 STR 4R TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. COMPLIED WITH FED EX EA 7-5330-98632.SDR 06FDEA0283Sill · mismanufacturedBS 570.5 LBL 10 MCD CUTOUT I/B SILL HAS FASTENER HOLE WITH NO EDGE MARGIN. HOLE LOCATED AT SILL SPLICE. COMPLIED WITH FED EX EA 7-5310-98588.SDR 06FDEA0282Skin · mismanufacturedBS 479 STR 4L-5L SKIN HAS HOLES WITH LESS THAN 4D FASTENER SPACING. REMOVED DAMAGED SECTION OF SKIN BS 680 STR 4L TO 10L AND REPAIRED PER FED EX EA 7- 5330-98633.SDR 06FDEA0281Skin · scheduled maintBS 480-680 STR 4L-4R, REPLACEMENT SKIN REQUIRES REMOVAL OF TEAR STRAPS TO ACCOMMODATE STRUCTURE OF MCD CUTOUT FROM STR 3L TO LT EDGE. REPAIRED PER SRM 51-10-2 AND DWG 53FX1380.SDR 06FDEA0279Tear Strap · mismanufacturedBS 460 STR 4R TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. REPAIRED TEAR STRAP, BS 460, STR 4R PER FED-EX EA 7-5330-98631.SDR 06FDEA0278Tear Strap · mismanufacturedBS 460 STR 4L TEAR STRAP HAS HOLES WITH LESS THAT 4D FASTENER SPACING. REPAIRED PER FED EX EA 7-5330-98634.SDR 06FDEA0277Sill · mismanufacturedBS 640 MCD CUTOUT O/B SILL LOWER SURFACE HAS PILOT HOLE WITH LESS THAN 4D FASTENER SPACING FROM INNER WEB FASTENER LOCATION. COMPLIED WITH FED EX EA 7-5310-98630.SDR 06FDEA0273Stringer · crackedLEFT WING STA 686.5 UPPER STRINGER 13 HAS A CRACK IN THE LOWER TAB SECTION THAT ATTACHES TO THE RIB PROTRUDING FROM UNDER RADIUS FILLER, REMOVE DAMAGE AND REPAIRS IAW BOEING S/B 727-57A159.SDR 06FDEA0268Bear Strap · corrodedBEAR STRAP CORRODED AT BS 720A BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION ON BONDED DOUBLER IS IN LIMITS IAW SRM 53-30-01.SDR 06FDEA0267Skin · unknownAFT CARGO BAY SKIN REQUIRES REPLACEMENT FROM BS 950 TO BS 1009, STR 26 LT TO STR 26 RT. *S/D* REMOVED AND INSTALLED AFT CARGO BAY SKIN FROM BS 950 - BS 1009, STR 26L-26R IAW EA 7-5310-96541.SDR 06FDEA0270Skin · bulgedBS 212, STR 26-27R, BULGE IN SKIN. REPAIRED BULGE IN SKINJ PER SRM 53-30-3.SDR 06FDEA0269Bear Strap · corrodedBEAR STRAP CORRODED AT BS 720 BETWEEN STR 2R AND STR 4 RT. REMOVED CORROSION ON BONDED DOUBLER AT SB 720 BETWEEN STR 2 RT AND 4 RT IAW SRM 53-30-1.SDR 06FDEA0258Stringer · crackedLT WING, STA.629.00 THIRD STRINGER FROM REAR SPAR IS CRACKED. *S/D* REPAIRED LT WING, STA 629.00 THIRD STRINGER FROM REAR SPAR PER EA 7-5710-96299.SDR 06FDEA0265Skin · gougedAFT LOWER CARGO DOOR OUTER SKIN IS GOUGED ON LOWER EDGE. REPAIRED AFT LWR CARGO DOOR SKIN IAW SRM 52-00-3.SDR 06FDEA0259Flange · corrodedCORROSION E-BAY RT MID CHORD FOR NWW HOR. FLANGE LWR SURFACE STA 312 - 328 RBL 16 WL 168 AND ON VERTICAL FLANGE STA 302 RBL 15 WL 170. REMOVED AND REPLACED NOSE WHEEL WELL R/H MID CHORD IAW SRM 51-30-2, 51-30-5.SDR 06FDEA0244Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 720A STR 3 RT. *S/D* REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2.SDR 06FDEA0243Stringer Clip · crackedINTERIOR FUSELAGE STRINGER CLIP 7L IS CRACKED BS 680. *S/D* REMOVED AND REPLACED STRINGER CLIP 7L AT BS 680 IAW SRM 51-30-2.SDR 06FDEA0242Rib · chafedWHILE WORKING VERTICAL CLOSE FOUND L/E ATTACH RIB AT LEADING EDGE FIN STA 55.8 CHAFED.SDR 06FDEA0241Repair · unknownEXTERNAL DOUBLER AROUND LT BLOW-OUT PANEL AT BS 1323, BELOW STR 14L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR DETERMINED NOT TO BE PER FAA APPROVED DATA AND TO BE A MAJOR RSDR 06FDEA0222Bear Strap · corrodedBEAR STRAP CORRODED AT BS 720B BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION AND IS IN LIMITS IAW SRM 53-30-01.SDR 06FDEA0218Bear Strap · corrodedBEAR STRAP CORRODED AT BS 700 BETWEEN STR 2 RT AND STR 4 RT. *S/D* REMOVED CORROSION AND IS IN LIMITS IAW SRM 53-30-01.SDR 06FDEA0221Skin · corrodedCORROSION ON INTERNAL SKIN BS 640-680 STR 4-5 RT. *S/D* REPAIRED PER SRM 53-10-1.SDR 06FDEA0233Angle · crackedCRACKED, NOSE LANDING GEAR WHEEL WELL TOP-AFT ANGLE, BS 351.2, LBL 4 TO RBL 4, WL 181 (CRACKED AFT UPPER CHORD) FX SNRM N00174. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW CHORD ALL IAW BAC DWG 65-18417 AND FX B727 SRM'S 51-30-2, 51-10-2.SDR 06FDEA0232Skin · gougedGOUGE IN FUSELAGE SKIN AT STA 294 AT STRINGER 25R. FX SNRM N00075. REMOVED DAMAGED AREA OF SKIN, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ALL IAW FX B727 SRM 53-30-3 FIG 1 & 4, 53-30-1 FIG 1, 53-30-2 FIG 4, 51-30-2 AND 51-10-2.
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