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 TAOA019604Hose · leakingSYSTEM A-HYDRAULIC QUANTITY LOW ON LANDING. BRAKE PRESSURE FAILED, THEN RECOVERED. REPLACED LEAKING RT ELEVATOR MODULE PRESSURE HOSE. LEAK CHECK AND OPERATIONAL CHECK OK. (X)SDR CAL960060Harness · out of positionIAH - FLT 8950 - THE 'NOSE GEAR DOOR' ANNUNCIATOR LIGHT ON SECOND OFFICER'S PANEL AND THE FORWARD PANEL DOOR WARNING LIGHT ILLUMINATED AFTER GEAR WAS RETRACTED DEPARTING IAH. THE AIRCRAFT HAD A HISTORY OF PROBLEMS WITH THE NOSE GEAR DOOR WARNING LIGHT. GEAR SDR 96FDEA00109Seat Track · corrodedCORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUTHOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05.SDR SCNA96006Gearbox · malfunctionedTHE NR 3 ENGINE SHUT DOWN ON TAXI OUT. FOUND NR 3 ENGINE TO HAVE A GEARBOX PROBLEM, SUN COUNTRY WILL UPDATE THIS REPORT WHEN SHOP FINDINGS ARE AVAILABLE.SDR SCNA96005Engine · malfunctionedDURING CLIMBOUT, THE NUMBER 3 ENGINE FAILED AT FL 210. NO ATTEMPT TO RESTART ENGINE IN FLIGHT WAS MADE. MAINTENANCE ENGINE RUN WAS ACCOMPLISHED PER MM 71-00-30 PAGE 216 AND NO DEFECTS WERE NOTED.SDR 96FDEA00139Stringer · damagedBS 757 TO 759 STR 7L DAMAGE INSIDE STRINGER ABOVE RIVETS THROUGH SKIN. REPLACED STR PER SRM 53-10-3.SDR 96FDEA00138Stringer · damagedUPPER LOBE BS 1072 TO 1090 STR 7R DAMAGE TO STRINGER INSIDE U-CHANNEL ABOVE SKIN RIVETS. INSTALLED REPAIR DOUBLER IAW BOEING SRM 53-10-3.SDR 96FDEA00101K-Flap · corrodedNR 5 K-FLAP O/B LUB O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECK IAW FEDEX MM 27-81-1.SDR CAL960244Act Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN RADIUS OF NR 6 KRUGER FLAP ACTUATOR OUTBOARD MOUNTING BRACKET. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 57-20-2. (X)SDR 96FDEA00141Stringer · damagedUPPER LOBE BS 885 TO 888 STR 7L, DAMAGE TO STRINGER INSIDE U-CHANNEL. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICATED FILLER, REPAIRED PARTS 1, 2, 3. LOCATED AND DRILLED ALL HOLES, TREATED AND PRIMED ALL PARTS AND INSTALLED PER SRM 53-10-3 PAGES 5 TO 8 SDR 96FDEA00140Stringer · damagedUPPER LOBE BS 882 TO 889 STR 7R DAMAGED TO STR INSIDE U-CHANNEL ABOVE SKIN RIVETS. REMOVE DAMAGED STR 7R FROM BS 872 TO 898, FABRICATED PARTS 1, 2, 3 AND 4. DRILLED AND INSTALLED PER SRM 53-10-3 FIG 3.SDR AALA960112Connector · looseDFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR 96FDEA00107Stringer · crackedUPPER LOBE STR 3L STA 440 CRACKED. INSTALLED REPAIR ON STR 3L STA 440 PER MM 53-10-3 PG 5 WITH FAB PARTS ON SHOP ORDER FE7X, FM7K, FM69.SDR MZZA96002Fan · failedFLT NR 926 - SPN - ON DESCENT, SMOKE AND ELECTRICAL SMELL COMING FROM GASPER SYSTEM. STRONGEST AROUND MID CABIN. TURNED OFF RIGHT PACK AND GASPER FAN. PULLED CIRCUIT BREAKER FOR GASPER FAN. MAINTENANCE FOUND GASPER FAN FROZEN. ALSO, CHECKED WIRING AND FOUSDR CAL960123Fitting · corrodedSTATION 31J - INSPECTION FOUND FLOOR SUPPORT FITTING AT BS 420 TO 440, RBL 10 AND AT BS 440 TO 460, RBL 10 CORRODED. THE FLOOR SUPPORT FITTINGS WERE REMOVED. NEW FLOOR SUPPORT FITTINGS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-20-2 AND 51-30-2. (MSDR 96FDEA00108Skin · corrodedFWD CARGO FUSELAGE SKIN CORRODED BETWEEN STR 28 LT AND RT STA 720C PLUS 5. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3.SDR CAL960131Support · corrodedSTATION 31J - INSPECTION FOUND FLOOR SUPPORT OVER PULLEY CORRODED AT BS 1070, RBL 20. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW MM 51-20-2 AND 51-20-11. (M)SDR 96FDEA00057Keel Beam · corrodedCORROSION ON LT KEEL BEAM OUTBOARD FLANGE AT BS 950D PLUS 3, LBL 10. REMOVED CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AND REPAIRED PER FEDEX EA 7-5310-26837.SDR 96FDEA00056Stringer Clip · crackedCRACKED STR CLIP AT BS 440 STR 1L. UPON REMOVAL OF CRACKED STR CLIP FOUND STR NR 1 TO BE DAMAGED AT BS 441. PERFORMED STR REPAIR BS 436 TO 446 STR NR 1 IAW FEDEX SRM 53-10-3 AND INSTALLED NEW STR CLIP BS 440 STR NR 1.SDR AALA960053Wire · looseSJU - FLT 0450 - EN ROUTE MIA/SJU DURING CRUISE AT FL 330, RT MLG RED AND GREEN LIGHTS ILLUMINATED WITH LANDING GEAR HANDLE IN THE OFF POSITION. NO OTHER ABNORMAL INDICATIONS NOTED. DESCENDING THROUGH FL 280 INTO SJU, THE LIGHTS EXTINGUISHED AND THE AIRCRAFTSDR AALA960051Screws · looseIAD - FLT 1267 - AFTER TAKEOFF IAD DURING CLIMB-OUT, FLUID NOTED LEAKING FROM AREA OF LT OUTBOARD AILERON. AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. RETORQUED LOOSE SCREWS AT THIRD FROM WING TIP UNDERWING FUEL TANK ACCESS PLATE. SYSTEM GROUND CHSDR 96FDEA00058Seat Track · corrodedUPPER LOBE FLOOR, OVER WING AREA CORR ON O/B FLANGE FLOOR TRACK LBL 45 STA 804 TO 848 LT. INSTALLED NEW SEAT TRACK AND CHORD PER SRM 51-10-1. INSTALLATION OF FLOATING SEAT TRACK FROM STA 740 TO 760 COVERED ON NR 1415 LBL 45.SDR 96FDEA00040Stringer · corrodedCORROSION (C53-224-01), ON STR FLANGE AT BS 720 STR 4L. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3.SDR CAL960141Gusset · crackedSTATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT OVERWING EXIT GUSSET AT BS 825.95, RBL 50, WL 215 TO 220. A NEW GUSSET WAS DRILLED AND INSTALLED IAW EA SA001-5310-01870. (M)SDR CAL960139Floor · corrodedSTATION 31J - INSPECTION FOUND FORWARD LAV FLOOR PANEL CORRODED. A NEW WEB SECTION AND L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-1, 51-10-2, AND 51-40-3. (M)SDR CAL960134Floor Beam · corrodedSTATION 31J - INSPECTION FOUND FLOOR BEAM LOWER CHORD CORRODED AT FASTENER HOLES, BS 1130, RBL O TO 56. A NEW REPAIR STRAP WAS FABRICATED. THE REPAIR WAS INSTALLED IAW AERO CORP ENGINEERING ORDER 96-250. (M)SDR CAL960129Skin · corrodedSTATION 31J - INSPECTION FOUND SKIN CORRODED AT FS 1010, STRINGER 28L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-30-3, AND 51-10-2. A STRINGER SECTION AND TWO CAP SPLICES WERE FABRISDR 96FDEA00361Bell Frame · crackedCABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. INSTALLED REPAIR PER 51-40-3 PG 1 TO 4.SDR 96FDEA00350Bell Frame · crackedCABIN, BELL FRAME CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER 7075T6.090 PER 53-30-4 FIG 1.SDR CAL960136Support · corrodedSTATION 31J - INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND ANCHOR NUTS AT BS 644 ABOVE STRINGER 28R. THE FLOOR SUPPORT FITTING WAS REMOVED AND REPLACED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-40-2. (M)SDR CAL960132Floor Beam · corrodedSTATION 31J - INSPECTION FOUND FLOOR BEAM CORRODED AT BS 1110, RBL 25. THE FLOOR BEAM UPPER CHORD WAS REMOVED IAW SRM 53-10-8. A NEW FLOOR BEAM UPPER CAP, STRAPS, SUPPORT ANGLES, L-ANGLES, AND STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2. (M)SDR CAL960126Floor Beam · corrodedSTATION 31J - INSPECTION FOUND CABIN FLOOR BEAM CORRODED AT BS 480, RBL 0 TO 60. THE CORRODED CAP WAS REMOVED FROM RBL 0 TO 60. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3, 51-10-1, 51-10-2, AND 51-20-0. (M)SDR CAL960124Floorbeam · corrodedSTATION 31J - INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 440, LBL 20 TO RBL 20. THE CORRODED SECTION WAS CUT OUT. A REPAIR BEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3, 51-30-2, 51-20-4, 51-10-1, 51-30-8, 51-10-2, AND MM 51-20-0. SDR CAL960242Floor Beam · corrodedINSPECTION FOUND THE CABIN FLOOR BEAM CORRODED AT BS 344, RBL 20 TO LBL 60. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW T-CAP WAS DRILLED AND INSTALLED IAW SRM 51-10-1, 51-30-2, 51-10-1, 51-30-2. (X)SDR CAL960151Support · corrodedSTATION 31J - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORT AT BS 418, RBL 20 TO 40. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-6. (M)SDR CAL960140Flange · crushedSTATION 31J - INSPECTION FOUND NR 1 ENGINE LOWER COWL FLANGE ON UPPER INBOARD LONGERON CRUSHED. A 3.5 INCH SECTION OF LONGERON WAS REMOVED. A Z-ANGLE, REPAIR DOUBLER, AND COVER PLATE WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL960127Angle · corrodedSTATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 720F TO 740, BL 0. THE SUPPORT ANGLE WAS REMOVED. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0. (M)SDR CAL960122Support · corrodedSTATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 360 TO 380, RBL 10. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-4. (M)SDR CAL960121Floorbeam · corrodedSTATION 31J - INSPECTION FOUND FLOORBEAM CORRODED AT BS 380, RBL 10 TO 60. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M)SDR CAL960120Support · corrodedSTATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 312 TO 328, LBL 28. THE CORRODED AREA WAS REMOVED. A NEW PART WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND MM 51-20-11. (M)SDR CAL960241Support · corrodedINSPECTION FOUND A 1 INCH CRACK IN RT FORWARD LAV FLOOR SUPPORT AT BS 312, RBL 20. THE CORRODED SECTION OF FLOOR SUPPORT WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-40-3, AND MM 51-20-0. (X)SDR CAL960147Skin · crackedSTATION 31J - INSPECTION FOUND A .5 INCH CRACK THROUGH RIVET HOLE OF R-1 DOOR EXTERNAL SKIN ABOVE LOWER HINGE CUTOUT. THE CRACKED AREA WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2, 51-10-2, AND MM 51-20-2. SDR CAL960146Skin · crackedSTATION 31J - INSPECTION FOUND A 1 INCH CRACK AT RIVET HOLE OF R-1 DOOR AFT LOWER CORNER EXTERNAL SKIN. THE CRACKED AREA OF DOOR WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-00-3 AND 52-00-3. (M)SDR CAL960137Hat Sections · corrodedSTATION 31J - INSPECTION FOUND FLOOR HAT SECTIONS AT LEFT AND RIGHT AFT LAV SIDEWALLS CORRODED. THE FLOOR HAT SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-30-2, AND 51-20-4. (M)SDR CAL960135Blkhd Chord · corrodedSTATION 31J - INSPECTION FOUND BULKHEAD REINFORCEMENT CHORD CORRODED ON RIGHT OUTBOARD END AT BS 1176.9. THE CORRODED SECTION OF CHORD WAS REMOVED. A NEW CHORD ANGLE BRACKET REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-3, 51-40-4, 51-10-1, 51-1SDR CAL960133Support · corrodedSTATION 31J - INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1070-1090, RBL 10. THE FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND MM 51-10-2. (M)SDR 96FDEA00106Stringer · corrodedAFT CX COMP STR 29L IS CORRODED ON O/B SIDE AT BELLFRAME STA 950E, AFT SIDE OF BELLFRAME. BEYOND LIMITS PER SRM 53-10-1, REPAIRED PER FEDEX EA 7-5310-26899.SDR 96FDEA00035Lug · corrodedNR 5 K-FLAP O/B LUG O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECKED IAW FEDEX MM 27-81-1.SDR 96FDEA00034Frame · crackedFRAME CRACKED AT STA 380 WL 278 RBL 65. REMOVED DAMAGED SECTION OF FRAME AT BS 380 WL 278 RBL 65. FABRICATED REPAIR ANGLE AND DOUBLERS, ALODINED, PRIMED AND INSTALLED WET. ALL WORK DONE PER FEDEX SRM 53-10-4.SDR 96FDEA00033Stringer · damagedMECH DAMAGE AND FASTENERS MISSING IN STR 7L BS 757 TO 759. ACCOMPLISHED STR REPAIR AT STA 740 TO 770 STR 7L PER FEDEX SRM 53-10-1, 53-10-2 AND 53-10-3.
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