Boeing 727-227
Service difficulty reports · 5,082
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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 = '727227' 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 = '727227' 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 DHLA200800049Warning System · malfunctionedFLT NR 589 MACH AIRSPEED WARNING ACTIVATED AT 70 KNT. PUMPED UP MACH AIRSPEED SYSTEM PER MM 34-14-00, SYSTEM OP'S CK NORMAL. NO DEFECTS NOTED AND 34-11-00 PITOT TEST. AIRCRAFT WAS GROUNDED.SDR DHL2008784002Skin · crackedNR 3 L/E K-FLAP HAS SMALL CRACK ON THE BOTTOM I/B CORNER.SDR DHL2008784001Support Bracket · crackedNR 5 K-FLAP ACTUATOR BOX HAS SMALL CRACK ON THE O/B SUPPORT BRACKET L/E STA 243.977 CRACK LOCATED AT LOWER FWD CORNER OF BRACKET.SDR 08FDEA01362Web · corrodedMAIN DECK FLOOR SHEAR WEB IS CORRODED/MISDRILLED, BS 1130-1177, RBL 16-64, WL 208. REMOVED CORRODED/MISDRILLED RT SHEAR WEB. RECEIVED NEW SHEAR WEB, DRILLED AND INSTALLED. REFERENCE SRM 51-30-2/PAGE NR 2 CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA01309Seat Track · corrodedMAIN DECK, SEAT TRACK I/B FLANGE CORRODED, BS; 1110 - 1130, RBL 45 REMOVED CORROSION AND SEAT TRACK IS OUT OF LIMITS. FABRICATED NEW SEAT TRACK, DRILLED, TREATED AND PRIMED AND INSTALLED. REFERENCE BOEING DOCUMENT NR 65-86245/ID 000 FRAME NR 2 SRM 51-10-2SDR 08FDEA01301Floor Support · corrodedMAIN DECK FLOOR SUPPORT, BS 1166 - 1177, RBL 45, UPPER SURFACE HAS CORROSION AND VERTICAL FLANGE IS GOUGED. REMOVAL AND INSTALLATION OF FLOOR SUPPORT BETWEEN STA 1166 - 1177/RBL 45 IS ON SNRM NR N00493/JPF LINE ITEM NR 178 AND 179. FABRICATED FLOOR SUPPORT ASDR 08FDEA01300Seat Track · corrodedAFT CABIN SEAT TRACK, (STA 1130 - 1168) RBL 45 IS CORRODED REMOVAL AND INSTALLATION OF RBL 45 SEAT TRACK FROM STA 1130 - 1177 IS ON SNRM NR N00493/JPF LINE ITEM NR 66 AND 67. FABRICATION OF SEAT TRACK IS ON SNRM NR N00839. DRILLED, TREATED AND PRIMED SEAT TRSDR 08FDEA01204Intercostal · corrodedMAIN DECK FLOORBEAM U CHANNEL INTERCOSTAL IS CORRODED, BS 1133, RBL 62, WL 208. REMOVED CORROSION AND FOUND CHANNEL TO BE OUT OF LIMITS. RECEIVED NEW CHANNEL/SUPPORT AND DRILLED HOLES, REFERENCE BOEING DOCUMENT NR 65-19606/ITEM -109, CLASSIFIED AS A MINOR RESDR 08FDEA01184Floorbeam · damagedMAIN DECK FLOORBEAM BS 1166, RBL 44-50, WEB HAS SEVERAL DOUBLE DRILLED HOLES. REMOVED AND REPLACED. FABRICATED REPAIR PARTS AT LT AND RT FUEL SHROUD CUT OUTS AND INSTALLED. REFERENCE EA 7-5310-113796. CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA01177Floorbeam · damagedMAIN DECK FLOORBEAM UPPER FLG IS DAMAGED BS 1148, RBL 43-49 , WL 208. REMOVED SURROUNDING STRUCTURE, REMOVED UPPER T-CAP, PREFORMED 10X VISUAL INSPECTION OF TRIMMED TREATED, PRIMED AREA. FABRICATED SURROUNDING STRUCTURE. REF SRM 51-30-2 PG 2. SRM 53-10-08SDR 08FDEA01080Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK, BS 1124 - 1125, LBL 45 - 46, HAS CORROSION AROUND FASTENER HOLE, UPPER AND LOWER SURFACE. REMOVED AND REPLACED SEAT TRACK, IAW SRM 53-10-5. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00796Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CAP LOWER SURFACE IS CORRODED NUTPLATE BS 1130, LBL 28-38. COMPLIED WITH EA 7-5310-113971 PART 1. CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA00795Frame · corrodedMAIN BODY FRAME ASSY CORRODED, BS 1166, STR 17L, WL 208. REMOVED CORROSION FROM BS 1166, S17L FRAME AND FOUND TO BE OUT OF LIMITS, REMOVED FRAME AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS MAJOR REAIRSDR 08FDEA00783Frame · corrodedBODY TO WING FAIRING PANEL, NR 3218 BETWEEN PRIMARY HEAT EXCHANGER RT O/B FRAME WEB HAS CORROSION ON MATING SURFACE AT FS 825, RBL WL 138. RT O/B FRAME WEB FOUND TO HAVE 50 PERCENT MATERIAL LOSS, OUT OF LIMITS REF SRM 51-10-01. REMOVED AND REPLACED FRAME WEBSDR 08FDEA00747Bulkhead · chafedNOSE W/W BS 351 BULKHEAD RBL 6", SKIN IS WORN FROM CONTACT WITH HYD HOSE CLAMP. BLENDED DAMAGE AREA AT NOSE W/W BS 351 BULKHEAD RBL 6. SKIN REF SRM 53-10-1 FIG 1, MEASURED THICKNESS, ORIGINAL "T" .073", MATERIAL REMAINING .058", FOUND TO BE WITHIN LIMITS REFSDR 08FDEA00702Support · corrodedCORROSION AND CRACK ON SIDEWALL "T" FRAME SUPPORT STA 1030 TO 1050, LT LOWER AFT PIT. REMOVED CORROSION ON "T' FRAME SUPPORT. REMOVED .022 INCH FROM ORIGINAL THICKNESS OF .065", REMAINING .043 INCH IS OUT OF LIMITS PER SRM 53-10-1 FIG 1. RECEIVED NEW PART, SDR 08FDEA00701Skin · damagedAFT FUSELAGE BS 1166 BETWEEN S19L S20L, FRAME AND SKIN HAVE OVER SIZED HOLE (APPROX 3/8 DIA.) NDT TO VERIFY MATERIAL THICKNESS .050". REMOVED DAMAGE ON SKIN. FABRICATED REPAIR DOUBLER AND FILLER 2024-T3 .063" A87331/P0 NR 1032671. OVERSIZED LAP SEAM HOLESSDR 08FDEA00699Angle · crackedMAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED, BS 1177 - 1183, RBL 47-64", WL 208. REMOVED RT DITCHING PAN ASSY. FABRICATED ANGLES WITH PART NR`S 65-29548-11 AND 65-29548-55. FABRICATED AND HEAT ATTACH ANGLES (SHOP NR N00880/8130 FORM SDR 08FDEA00698Attach Angle · crackedINTERCOSTAL LOWER ATTACH ANGLE HAS ELONGATED HOLES, CRACK AND CORRODED AT 1110 TO FS 1130, BL 0. FABRICATED INTERCOSTAL LOWER ATTACH ANGLE AT FS 110 TO FS 1130 BL 0", REF DWG 69-4569. THIS IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA00697Depressor · crackedC2 DOOR FWD SEAL DEPRESSOR, 22 INCHES FROM TOP CORNER IS CRACKED. REPLACED FWD SEAL DEPRESSOR REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00696Depressor · crackedC2 DOOR AFT SEAL DEPRESSOR, 22 INCHES FROM UPPER CORNER IS CRACKED. REPLACED AFT SEAL DEPRESSOR REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00667Angle · crackedMAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED BS 1177 - 1883, LBL 47 -64, WL 208. REPLACED FWD AND AFT CHORD ANGLES IAW DWG 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00666Support · corrodedPANEL "T" SUPPORT BRACKET HAS CORROSION, BETWEEN LEFT AND RIGHT RAM AIR FIBERGLASS DUCTS, BETWEEN STA 720E AND 720F, LEFT SIDE. REMOVED PANELS FOR ACCESS, REMOVED "T" SUPPORT, REMOVED CORROSION, NDT FOR MATERIAL LOSS ORIG .058'", REMAINING .053' INCH, WITHSDR 08FDEA00648Skin · damagedFOUND FUSELAGE SKIN CORROSION AT FS 582, STR 28L, AFTER REMOVING WEB ON SNRM N00557 FOUND SERIES OF MISDRILLED HOLES ALONG INTERCOSTAL NEAR BOTTON EDGE OF MAIN CARGO DOOR DOUBLER COMPLIED WITH EA NR 7-5330-118244 PART NR 1. REMOVED INTERNAL STRUCTURE TO GAIN SDR 08FDEA00633Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLAG IS CORRODED/MISDRILLED BS 1110, LBL 27-34, WL 208. REMOVED CORROSION BS 1110, LBL 27 - LBL 31, MAT. THICK .125". REMOVED .116", REMAINING .009" OUT OF LIMITS REF 727-PF SRM 53-10-1 PG 25-41. AAR TOOL 18172, CAL DATE DUE 10/1SDR 08FDEA00630Skin · crackedLT LWR FUSELAGE EXTERIOR SKIN SURFACE SHOWS CRACK AT STA 520, ABOVE STR 23L, FWD OF THE STATIC PORT. PERFORMED HFEC AND FOUND CRACK 2" IAW B727 NDTM PART 6 51-00-00 FIG23. REPAIRED FUSELAGE, MDCD SURROUND STRUCTURE TRIPLER AT STA 520, STR 23L IAW EA NR 7-533SDR 08FDEA00629Floor Support · corrodedAFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 11 HAS CORROSION ON UNDERSIDE. REMOVED DAMAGE AND FABED CHANNEL AND SPLICE REPAIR AT STA 1144 TO 1166. APPLIED ALODINE, PRIMER AND PAINT. INSTALLED NEW CHANNEL AND SPLICE, REF SRM 51-10-06, 53-10-0SDR 08FDEA00628Intercostal · corrodedVERTICAL WEB AT FS 580 - 600, LBL 15 IS CORRODED REPLACED WEB AT STA 580 - 600, LBL 15 WITH NEW WEN REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00627Frame · corrodedAFT LWR CARGO BAY AT BS 950D BETWEEN STR S-29L AND S-28L, AFT SURFACE OF FRAME AND LWR SURFACE OF LWR CHORD HAVE CORROSION REMOVED FASTENERS FROM STA 950D STR 28L - 30L, BLENDED CORROSION, ORIGINAL MATERIAL .071". REMAINING MATERIAL .058 INCH, MATERIAL REMOVESDR 08FDEA00626Threshold · crackedSEVERAL CRACKS AND DENTS IN THRESHOLD PLATE, FWD LOWER CARGO COMPT. THRESHOLD PLATED REPAIRED ON SHOP N/R N00123. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR DHLA200800018Skin · delaminatedDURING PREFLIGHT WALKAROUND, FOUND TRAILING EDGE OF LEFT WING FLAP SPLIT OPEN. REMOVED AND REPLACED LT WING I/B TRAILING EDGE FLAP, OPS CK GOOD REF 727 MM 27-51-2. AIRCRAFT WAS GROUNDED.SDR 08FDEA00589Channel · corrodedAFT LWR CARGO BAY CENTER LINE FLOOR ANGLE AT BS 1035-1037 HAS CORROSION ON THE UNDERSIDE VERFIED MATERIAL FOR REPAIR PARTS. FABRICATED REPAIR PARTS REF SRM 53-10-5, DWG SR27-53-039. REMOVED CORROSION, FOUND TO WITHIN LIMITS REF SRM 53-10-1 FIG 4. TREATED PRSDR 08FDEA00588Floorbeam · corrodedMAIN DECK FLOORBEAM, UPPER FLANGE IS CORRODED, BS 1070, LBL 47-60, WL 208. REMOVED CORROSION ON MAIN DECK FLOORBEAM UPPER FLANGE, STA 1070, LBL 47"-60". FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR, REF SRM 53-10-08 FIG 1. THIS IS CLASSIFIED ASDR 08FDEA00587Fairing · crackedRT WING O/B JACKSCREW TOP WING PANEL BRACKET CRACKED AT AFT I/B SIDE OF FAIRING. REMOVED FAIRING, REMOVED AND REPLACED DOUBLER ON FAIRING REF SRM 51-30-. REINSTALLED FAIRING REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00586Stringer · corrodedFWD PIT FLOORBOARD SUPPORT STRG AT (STA 645) RBL 12 IS CORRODED (MARKED ) REMOVED DAMAGED AT STA 645 AND FABED A REPAIR. APPLIED ALODINE, PRIMER AND PAINT. REINSTALLED FLOOR SUPPORT AND INSTALLED SPLICE AT STA 670. APPLIED ALODINE, PRIME AND PAINT, REF SRMSDR 08FDEA00585Frame · corrodedFWD LOWER CARGO COMPT FRAME TIE AT STA 580 LBL 20 CORRODED AT END VERIFIED MATERIAL FOR REPLACEMENT FRAME TIE REF DWG 69-14871 .050 7075 T-6. FABRICATED NEW FRAME TIE REF DWG 69-14871. TREATED PRIMED REF SRM 51-10-2. INSTALLED NEW FRAME TIE REF SRM 51-30-2,SDR 08FDEA00583Frame · crackedNR 1 ENG UPPER COWL FWD I/B END FRAME CRACKED REMOVED INB END FRAME. FABRICATED INSTALLED DOUBLER IAW SRM 51-40-2. TREATED PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED STRIKER PLATE IAW SRM 51-30-1. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00582Stringer · corrodedFWD PIT (STA 582) STR 27L CORRODED (MARKED ) REMOVED DAMAGED SECTION OF STR 27L . VERIFIED ORIGINAL MATERIAL AS .040 7075-T6 REF SRM 53-10-2 FIG 9. REPLACEMENT CHANNEL SAME AS ORIGINAL, BAC1498-140, FX1376, PO1013862. VERIFIED MATERIAL FOR REPAIR SPLICES AS SDR 08FDEA00581Frame · corrodedFWD CARGO COMPT CORROSION ON STA 580 TO SKIN, LBL 3" TO LBL 10". REPAIRED SHEAR TIE AT STA 580, LBL 3" TO 10". REF SRM 53-10-4 FIG 15. THIS IS CLASSIFID AS A MAJOR REPAIR.SDR 08FDEA00580Frame · damagedFRAME SHEAR TIE AT FS 600 LBL 12 HAS MISDRILLED HOLES FROM PREVIOUS WORKMANSHIP REMOVED DAMAGED SHEARTIE REF SRM 53-10-4. FABRICATED NEW ANGLE REF SRM 53-10-4, TOP COAT ANGLE REF SRM 51-10-2 MM 51-20-151-7. INSTALLED ANGLE TIE REF SRM 53-10-4 FIG 15. THIS ISDR 08FDEA00570Threshold · crackedAFT ENTRY DOOR THRESHOLD HAS AREAS OF DAMAGE (BOTH BULLNOSE PIECES CRACKED) PARTS OF THRESHOLD SENT TO BE FABRICATED AND HEAT TREATED IN SHOP, 8130-3 TRACKING NR 2008-02-125 AND 126. HEAT TREATED TO T4 CONDITION. THRESHOLD RECEIVED FROM SHOP FABRICATED AND ISDR 08FDEA00568Frame · crackedFWD CARGO PIT, FRAME EXTENSION AT BS 520 IS CRACKED IN UPPER RADIUS, ABOVE STRINGER 22L ON FWD SIDE OF FRAME, MARKED END OF CRACK WITH BLACK DOT, (CIRCLED) GENERATED FROM U/C 53F0020. REMOVED CRACKED FRAME EXTENSION. VERIFIED MATERIAL FOR FABRICATION OF NESDR 08FDEA00521Skin · corrodedFWD PIT BILGE ( STA 720 ), BL 0 LWR SKIN CORRODED UNDER LEVELING COMPOUND. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS OF .028 INCH. FABRICATED DOUBLER AND INSTALLED DOUBLER TO SKIN REF 53-30-3 PG 3-5.SDR 08FDEA00520Frame · crackedLEFT WING OUTBOARD T/E NR 1 TRACK CENTER FAIRING INTERNAL AFT FORMER FRAME IS CRACKED IN CENTER. REMOVED AFT FORMER FRAME, LOCATED AND DRILLED NEW AFT FORMER FRAME AND INSTALLED REF SRM 51-30-2 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00514Frame · crackedFWD CARGO PIT, FRAME EXTENSION AT BS 600 IS CRACKED IN UPPER RADIUS, ABOVE STR 22L ON FWD SIDE OF FRAME. MARKED END OF CRACK WITH BLACK DOT CIRCLE. GENERATED FROM W/C 53F0020. FABRICATED FRAME EXTENSION REF DWG 53FX1350. HEAT TREATED TO T-6 CONDITION ON 81SDR 08FDEA00513Shear Tie · damagedMAIN CARGO BAY BS 680 FRAME SHEAR TIE HAS HAS TOOLING DAMAGE IN THE RADIUS BETWEEN STR S 14L AND S 15L, GENERATED BY 530045 CHECK DAMAGE LIMITS, ORIG MAT'L .045", MAT'L LOSS .007' WITH .038 REMAINING. DAMAGE IS OUT OF LIMITS REF SRM 53-10-2 PG 12A FIG 3. CSDR 08FDEA00512Stiffener · crackedNR 1 ENG UPPER COWL STIFFENER CRACKED BETWEEN 2ND AN 3RD LOWER LATCH CUTOUTS. REMOVED SEAL AND SEAL RETAINER, REMOVED CRACKED COWL STIFFENER, VERIFIED MATERIAL ID. FABRICATED NEW COWL STIFFENER, TREATED AND PRIMED, INSTALLED NEW COWL STIFFENER. REINSTALLED SDR 08FDEA00511Threshold · crackedMAIN ENTRY DOOR CUTOUT LWR AFT SS THRESHOLD CORNER PLATE HAS 2 CRACKS RECEIVED SERVICEABLE THRESHOLD PLATE REF A TAG FEX3650, AND 8130-3 5517-0000, PLATE WILL BE INSTALLED ON EO CARD NR 7-5310-7-3362 P3 CARD 3 STEP C-2, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA00509Stiffener · corrodedA/C EQUIP BAY, FAIRING SUPPORT INTERCOSTAL HAS CORROSION, STA 780, 3 INCHES, BL 0, JUST BELOW DELTA BEAM (STIFFENER). REMOVED CORRODED STIFFENER AND STRAP AT STA 780 + 3". REMOVED CORROSION AND MATERIAL WAS OUT OF LIMITS, BEYOND 10 PERCENT ALLOWABLE DAMAGE. SDR CA080219004Skid · defective(CAN) UPON GEAR RETRACTION, TAIL SKID LIGHT REMAINED ILLUMINATED. A/C RETURNED TO STATION WHERE SKID TIP WAS REPLACED, SWITCH CONTACT CONFIRMED AND A/C RETURNED TO SERVICE. (TC NR 20080219004)
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