Boeing 727-227
Service difficulty reports · 5,082
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 = '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 08FDEA04267Skin · crackedLEFT WING UPPER SURFACE SKIN CRACKED AT NR 4 SPOILER I/B ACTUATOR HINGE CUTOUT REMOVED AND REINSTALLLED NR 4 SPOILER PANEL, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED DOUBLER REF SRM 57-30-4, 51-10-2, 51-30-2 AND MM 51-20-000-7, MM 27-61-081-4. STOPSDR 08FDEA04260Plate · crackedAFT LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND PLATE CRACKED REMOVED AFT CARGO THRESHOLD, WELDED CRACK ON N/R NOO382 REINSTALLED THRESHOLD REF SRM 51-30-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA04261Pan · crackedRT EXT FUSE FWD LAV SERVICE PAN IS CRACKED AT LOOSE DUMP CABLE FEED THROUGH BS 301, S18-20R GAINED ACCESS TO CRACKED AREA CLAENED AND REPAIRED CRACKS BY WELDING REF EA7-5240-114036. THIS IS CLASSIFIED AS A MINOR REPAIR
SDR 08FDEA04259Channel · corrodedA/C BAY FAIRING SUPPORT CHANNEL AT BS 776 LBL9-RBL9 CORRODED ON INNER SURFACE. CORROSION FOUND OUT OF LIMITS REF SRM 53-10-1. REMOVED PANELS 3358L, 3458R & 3217 FOR ACCESS REF SRM51-30-2. REMOVED STIFFNER, BRACKET, & CHANNEL. FABRICATED NEW STIFFNER, BSDR 08FDEA04258Web · crackedLT MED 1L INTERIOR LOWER FWD CORNER BOTTOM WEB CRACKED APPROX 3/4" FROM INNER SKIN. REMOVED DAMAGE REF SRM 51-40-2 VARIFIED DAMAGE REMOVAL PER HFEC NDT MANUAL PART 6, 51-00-00. FABRICATED REPAIR PARTS REF SRM 51-40-2 INSTALLED REPAIR PARTS REF SRM 51-30-2 THSDR 08FDEA04253Seat Track · corrodedCABIN SEAT TRACK, RBL 24, BS 940-950, OB FLANGE HAS LIGHT CORROSION ON UPPER SURFACE REF SNRM N00460 REMOVED AND REINSTALLED FLOOR BOARDS BS 850-950E BL 0 TO RBL 25. REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED, FABRICATED, TREATED, PRIMED, PAINTSDR 08FDEA04252Seat Track · corrodedCABIN SEAT TRACK RBL 45, BS 940-950 OB FLANGE UPPER SURFACE CORRODED REF SNRM N00460 REMOVED AND REINSTALLED FLOOR BOARDS BS 850-950D RBL 24-45 REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS REMOVED, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED SEAT SDR 08FDEA04235Seat Track · corrodedTRACK AT STA 870 TO 890 RBL 24 IS CORRODED. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .100 MATERIAL LOSS .026 REMAINING .074 OUT OF LIMITS. FABRICATED, TREATED, AND PRIMED SEAT TRACK SECTION STA 870-890 RBL 24 SEAT TRACK SECTION TO BE INSTALLED ON NSDR 08FDEA04246Fitting · wornLEFT AFT ENTRY DOOR, FWD LOWER STOP PIN LUG HAS WORN FLAT SPOT REMOVED AND REPLACED L2 DOOR REF AMM 52-14-000-4. REMOVED AND REPLACED FWD LWR STOP FITTING REF SRM 51-30-02. REMOVED AND REPLACED PRESSURE SEAL REF AMM 52-12-011-4 THIS IS CLASSIFIED AS A MAJOR RESDR 08FDEA04224Retainer · crackedRIGHT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HOLE CRACKED OUT, LOWER AFT CORNER DRILLED AND INSTALLED NEW SEAL RETAINER ON RT FWD EMERGENCY EXIT HATCH ON LOWER CORNERS. REF SRM 51-30-2, PAINTED SEAL RETAINER REF MM 51-20-000-7 THIS IS CLASSIFIED AS ASDR 08FDEA04247Attach Angle · corrodedLT MLG WHEEL WELL ABOVE GEAR UPLOCK MECANISM, BS 910 LBL 64 TO LBL 68 WL 194 FWD SIDE OF BOX FRAME LOWER ATTACH ANGLE CORRODED AND CORROSION EMINATING FROM UNDER ANGLE ON LOWER WEB REMOVED ANGLE REF SRM 51-30-2, CLEANED AREA AT SURFACE OF LOWER WEB, NO CORSDR 08FDEA04243Floor Support · crackedCRACKED IN FLOOR BOARD "Z" ANGLE SUPPORT WEB AT FS 950A + 16, LBL 17, WL 144 REMOVED AND REPLACED SUPPORT WEB REF SRM 51-30-2 PG 1-10 THIS IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA04236Angle · corrodedPANEL RACK- AFT PIT "Z" ANGLE BS 950D 10" LT SIDE HAS CORROSION ON TOP SIDE REMOVED CORROSION MATERIAL LOSS OF .015 ORIGINAL THICKNESS .056 REMAINING MATERIAL .041 FOUND OUT OF LIMITS REF SRM 53-10-1. TRANSFERED HOLES TO NEW PART (65-57568-13) AND INSTALLED SDR 08FDEA04231Retainer · corrodedLEFT FWD EMERGENCYEXIT HATCH, SEAL RETAINER ON DOOR HAS CORROSION. REPLACED SEAL RETAINER TOP SIDE OF LT FWD EMERGENCY DOOR REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA04229Web · gougedFWD MAIN ENTRY DOOR FUSELAGE CUTOUT, SILL WEB HAS NUMEROUS GOUGES, UPPER SURFACE BS 320 LBL 64, BLENDED GOUGES GENERATED EA FOR BLEND ALLOWANCE, BLEND IS WITHIN LIMITS REF EA7-5310-123801 TREATED AND PRIMED REF EA 7-5310-123801 THIS IS CLASSSIFIED AS A MINOSDR 08FDEA04226Attach Angle · crackedRIGHT WING, CRACK IN L/E TOP SKIN ATTACH ANGLE ON LEADING EDGE FRAME AT SLAT STATION 0 AT I/B END OF NR 5 SLAT FABRICATED NEW ATTACH ANGLE ON RT WING L/E FRAME AT SLAT STA. 0.296. AT I/B END OF NR 5 SLAT REF DWG 65-16209,TREATED, PRIMED, PAINTED AND INSTALLEDSDR 08FDEA04225Angle · crackedRT MAIN GEAR WHEEL WELL AFT BULKHEAD UPPER OB CORNER BS 950 APPROX RBL 67, PRESSURE DECK ATTACH REPAIR ANGLE CRACKED. REMOVED FLOOR PANEL FOR ACCESS, REMOVED REPAIR ANGLE REF SRM 51-30-2. FABRICATED SPLICE PLATE REF DWG 65-89360. TREATED PRIMED SPLICE PLATE SDR 08FDEA04223Retainer · corrodedRT FWD EMERGENCY EXIT HATCH, SEAL RETAINER LOWER AFT HAS CORROSION. FABRICATED SEAL RETAINER REF DWG 50-07978. DRILLED AND TRIMMED SEAL RETAINER REF SRM 51-30-5, TREATED AND PRIMED REF SRM 51-10-2, PAINTED REF MM 51-20-000-7 LABELED RETAINER 65-07978-69 REF GMSDR 08FDEA04203Retainer · crackedRIGHT AFT EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HAS HOLE CRACKED OUT. REPLACED UPPER SEAL RETAINER ON RT AFT EMERGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 PAINTED SEAL RETAINER REF MM 51-20-000-7 THIS IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA04197Support Angle · corrodedLT MLG WHEEL ABOVE GEAR UPLOCK MECHANISM, INSIDE BOX FRAME FWD LOWER CORNER, BS 910 LBL 64 TO LBL 68, WL 194, HAS CORROSION. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS, REMOVED UP LOCK ACTUATOR. REMOVED WEB AND ANGLE ATTACHED TO FRAME. FABRICATED ANGLE, SDR 08FDEA04200Shear Tie · corrodedAFT CARGO BILGE FRAME SHEAR TIE CORRODED, BS 950B S28R WL 140 . REMOVED CORROSION REF SRM 51-10-1. HFEC ORIGINAL "T" IS .100', LOSS AT DEEPEST POINT IS .018" REMAINING "T" .082", OUT OF LIMITS REF SRM 53-10-1, REMOVED WEB STIFFNER AND CARGO TIE DOWN TO FSDR 08FDEA04199Retainer · crackedNR 1 CARGO DOOR SEAL RETAINER HAS TWO CRACKS, DRILLED NEW SEAL RETAINER, FWD LOWER CORNER OF NR 1 CARGO DOOR. INSTALLATION TO BE COMPLETED ON EO 7-5310-7-3369C, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA04176Fitting · corrodedFWD PIT DOOR CUTOUT LWR SILL BEAM TIE DOWN FITTING ASSY ADAPTER PLATE IS CORRODED, BS 565, STR 26R, WL 155. REMOVED ADAPTER PLATED STA 580 REF 51-30-02 PG 1. MATCHED DRILLED FASTENER HOLES REF SRM 51-30-05 DWG 69-55655, PAINTED ADAPTER REF SRM 51-20-00 PG 7.SDR 08FDEA04174Attach Angle · crackedMAIN ENTRY DOOR, AFT CUTOUT STRUCTURE BS 344 STR 15R INTERCOSTAL FWD ATTACH ANGLE TO FRAME CRACKED. FABRICATED ANGLE REF BOEING DRAWING 69-16970, SOPM 20-42-03 PG 3, SOPM 20-44-04-PG 3. REPLACED ANGLE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA04168Shear Tie · corrodedAFT CARGO PIT BS 1050 AT STRINGER 27L BULGE BETWEEN SKIN AND FRAME REMOVED SHEAR TIE AND FOUND PART TO HAVE EXFOLIATION CORROSION. FABRICATED NEW SHEAR TIE FROM 7075-O AND HEAT TREATED TO T-6. DRILLED FASTENER HOLES. TREATED AND PRIMED AND PAINTED SHEAR TIESDR 08FDEA04167Support Bracket · crackedLEFT WING NR 1 FLAP TRACK - FLAP TRACK TO LOWER TRAILING EDGE PANEL SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED NEW BRACKET REF DWG 65-2289. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA04163Skin · crackedFWD CARGO DOOR (PIT DOOR), EXTERNAL SKIN CRACKED, 30 INCHES AFT OF LEADING EDGE, 3 INCHES ABOVE LOWER EDGE CUTOUT DAMAGE, PERFORMED HFEC INSP OF CUTOUT. NO DEFECTS NOTED. PERFORMED INSURANCE CUT. FABRICATED DOUBLER AND TREATED AND PRIMED REPAIR PARTS AND RESDR 08FDEA04127Floor Support · corrodedAFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A NEW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIMED, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA04126Floor Support · corrodedAFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A NEW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIME THIS IS CLASSIFIED AS A MINOR REPAIRSDR 08FDEA04125Seat Track · corrodedMAIN CABIN BS 1110 SEAT TRACK AT RBL 45 IS CORRODED REMOVED AND REINSTALLED FLOORBOARDS RBL 24 TO RBL 62 STA 1070-1110. REMOVED CORROSION ON SEAT TRACK ORIGINAL MATERIAL THICKNESS .070 MATERIAL LOSS .022. REMAINING .048 OUT OF LIMITS AAR TOOL IN17-0112 CAL DSDR 08FDEA04124Retainer · crackedLT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR HAS SEVERAL HOLES CRACKED OUT. REPLACED AFT ATTACH ANGLE. FABRICATED ATTACH ANGLE REF: DWG NR 50-07978. TREATED, PRIMED AND PAINTED REF:SRM 51-10-2 PG 1-10 AND MM 51-20-151-7 PG 1. INSTALLED REF SRM 51-30-SDR 08FDEA04123Attach Fitting · cracked"PANEL RACK" INBD T/E NR 4 FLAP TRACK AFT FAIRING HAS CRACK IN MOUNT BRACKET AT FWD OUTBOARD END. FABRICATED NEW MOUNT BRACKET AND INSTALLED REF BOEING DOCUMENT 65-21795, SRM51-30-2 PG1-8 GMM 7-0-1001, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1. THIS IS CLASSIFIESDR 08FDEA04078Support · corrodedAFT CARGO PIT STA 1010 SIDEWALL SUPPORT CORRODED AT FASTENER HOLES OVER STRINGER 27-26L. BLENDED CORRODED AREA, ORIGINAL "T" .050, REMOVED .014 REMAINING .036 OUT OF LIMITS. SUPPORT FABRICATED FROM 2024-0-.040, HEAT TREAT T3 CONDITION, APPLIED ALODINE, PRIMESDR 08FDEA04077Flap Track · gougedLEFT WING O/B FLAP TRACK I/B EDGE OF TOP FLANGE GOUGED APPROX 14" AFT OF REAR SPAR. BLENDED GOUGE, MATERIAL REMOVED .015 WITHIN LIMITS. MAGNETIC PARTICLE INSPECTED, FLAP PEENED REWORKED AREA, APPLIED ALODINE & PRIMED REF EA 7-5750-118300 P2 PART 1 CLASSIFIEDSDR 08FDEA04076Stringer Clip · damagedSTRINGER CLIP DAMAGED AT STR 26L, FS 540, LBL 23, WL 152. REMOVED AND REPLACED STRINGER CLIP AT STA 540 STRINGER 26L LBL 23 REF SRM 51-30-2 PG 5. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA04075Stringer · damagedSTRINGER DAMAGED AT BS 540 WL 152 LBL 23. FABRICATED NEW STRINGER SECTION AND TWO SPLICE REPAIRS ON STRINGER 26L BS 540 LBL 23 REF SRM 53-10-3 FIG 1. TREATED, PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2, 51-10-3 FIG 1. THIS IS CLASSIFIED AS A SDR 08FDEA04072Frame · damagedRT AFT EMERGENCY EXIT HATCH CUTOUT, AFT FRAME DAMAGED AT RIVET LOCATION BLENDED AREA OF FRAME, FABRICATED REPAIR PARTS, CAD PLATED, TREATED, PRIMED AS NEEDED. INSTALLED ALL PARTS AND REMOVED FASTENERS AND SIDEWALLS FOR ACCESS REF EA 7-5310-114033.SDR 08FDEA04067Stringer · corrodedAFT CARGO PIT, STA 1150, RBL 24, CORROSION ON UNDER SIDE OF STRINGER 26. REMOVED CORROSION STR 26 R ORIGINAL .090, REMOVED .032, REMAINING .058 OUT OF LIMITS. FABRICATE STRINGER & SPLICES. ALODINED PRIMED PARTS, INSTALLED REPAIR PARTS REF SRM 53-10-1, 53-10SDR 08FDEA04068Retainer · corrodedLT WING SPAR UNDERWING PANEL SEAL RETAINER HAS CORROSION O/B OF APU FIRE BOTTLE AT WS 182 TO 200. FABRICATED SEAL RETAINER REF DWR 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PG 1- 9. INSTALLED SEAL RETAINER REF 51-30-2 P1-3. THIS IS A CLASSIFIED A MINSDR 08FDEA04066Retainer · corrodedLT WING REAR SPAR LWR CHORD APPROX STA 182, SEAL RETAINER CORRODED REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED NEW RETAINER REF DWG 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-3. INSTALLED SEAL RETAINER REF SRM 51-30-2 PG'S 1-3. THIS IS CLASSISDR 08FDEA04038Frame · crackedRT WING, I/B AILERON LOWER T/E PANEL FRAME CRACKED WITH MISSING ATTACH FASTENER AT AFT END OF FRAME 10 INCH O/B FROM I/B END OF AILERON REMOVED DAMAGED PANEL FRAME REF SRM 51-30-2. VERIFIED MATERIAL OF FRAME TO BE BAC1506-1625 7075-T6. FABRICATED REPLACEMESDR FDEA200809213957Hose · leakingTEST FLIGHT, LOST ALL HYD SYS A FLUID UPON RAISING LANDING GEAR. REMOVED AND REPLACED LT MLG ACTUATOR LWR HYD HOSE IAW MM 32-32-000-4. LEAK CHECK GOOD IAW MM 32-32-000-5. PART IS TRACKING LEVEL 0. CLOSED FINAL.SDR 08FDEA03957Hose · leakingTEST FLIGHT, LOST ALL HYD SYS A FLUID UPON RAISING LANDING GEAR. REMOVED AND REPLACED LMLG ACTUATOR LOWER HYDRAULIC HOSE IAW MM 32-32-000-4. LEAK CHECK GOOD IAW MM 32-32-000-5.SDR 08FDEA03933Channel · crackedRT WING, I/B AILERON O/B L/E SEAL MOUNT BRACKET/UNDERWING PANEL MOUNT BRACKET CRACKED 10 INCH I/B FROM O/B END OF AILERON REMOVED SEAL MOUNT BRACKET AND ATTACH ANGLE, FABRICATED NEW "U" CHANNEL. FABRICATED NEW ATTACH ANGLE, HEAT TREATED TO T4 CONDITION. U CHSDR 08FDEA03928Seat Track · corrodedCORROSION ON SEAT TRACK I/B FLANGE FROM FS 1171 - FS 1146, LBL 24, WL 208. REMOVED CORROSION ON SEAT TRACK, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .135 INCH REMAINING .127 INCH MATERIAL LOSS .008 INCH WSDR 08FDEA03927Seat Track · corrodedCORROSION ON SEAT TRACK ATTACH FLANGE, FS 1171 TO 1162, LBL 1, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS. NO DEFECTS WERE FOUND, ORIGINAL THICKNESS .190 INCH, REMAINING .174 INCH, MATERIAL LOSS .016 WITHIN LIMITS, REF EA 7-531SDR 08FDEA03926Seat Track · corrodedCORROSION ON TOP OF SEAT TRACK ATTACH FLANGE, FS 1140-1173, RBL1, WL 208. REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS .190, .175 REMAINING, MATERIAL LOSS .015 WITHIN LIMITS REF EA 7-5310-11403. TREATED ANDSDR 08FDEA03925Seat Track · corrodedSEAT TRACK DAMAGED AT FS 1164 TO FS 1160, BL 0, WL 208 REMOVED DAMAGED, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS .175 REMAINING.167 MATERIAL LOSS .008" WITHIN LIMITS REF EA 7-5310-114031. TREATED AND PRIMED ARESDR 08FDEA03923Seat Track · corrodedCORROSION AT ATTACH FASTENER ON SEAT TRACK, FS 1174, LBL25, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .065 INCH REMAINING .061 INCH MATERIAL LOSS .004 INCH WITHIN LIMITS. REF EA NR 7SDR 08FDEA03922Intercostal · corrodedLWR EXT FUSE WING BODY FRG SUPPORT FRAME INTERCOSTAL ASSY INT SURF IS CORRODED BS 773, LBL9- RBL 9, WL 140. FABRICATED NEW SPLICE PLATE AND INSTALLED, REF BOEING DWG 65-58504. REMOVED FRAME SUPPORT, REMOVED CORROSION ON SLICE PLATE MATERIAL LOSS 50 PERCENT O
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