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 98ZZZX1776Light · inoperativeBOX/PHL - FLT 431 - MID-CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED LOOSE CANNON PLUG ON EXIT FIXTURE.SDR 98ZZZM733Slat Actuator · failedLAS - DURING CLIMB, NR 5 LEADING EDGE SLAT DID NOT INDICATE FULLY EXTENDED AFTER USING ALTERNATE FLAP SWITCH, BOTH POSITION. RETURNED TO LAS. 'A' SYSTEM HYDRAULIC LOSS. FOUND ACTUATOR END CAP SEPARATED FROM HOUSING AND SEIZED ON ACTUATOR SHAFT. REMOVED ANDSDR CALA9800576Skin · debondingINSPECTION FOUND RT WING NR 6 KRUEGER FLAP DEBONDING. A REPAIR WAS ACCOMPLISHED IAW ECRA 5720-01064.SDR CALA9800575Floorbeam · corrodedINSPECTION FOUND TOP FLANGE OF FLOORBEAM CORRODED AT FS 1110, RBL 10 TO RBL 63. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9800574Seat Track · corrodedINSPECTION FOUND TOP AND BOTTOM OF RT OUTBOARD SEAT TRACK CORRODED AT FS 400 TO 440. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.SDR CALA9800572Skin · gougedINSPECTION FOUND A 1 INCH GOUGE IN RT INBOARD FOREFLAP OUTBORD LEADING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED.SDR CALA9800570Flap Track · corrodedINSPECTION FOUND NR 7 FLAP TRACK AFT MOUNT CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.SDR CALA9800569Floorbeam · corrodedINSPECTION FOUND TOP FLANGE UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT FS 360, RBL 10 TO LBL 18. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.SDR CALA9800568Chord · corrodedINSPECTION FOUND TOP AND BOTTOM OF CHORD CORRODED AT FS 310 TO 362, LBL 56. ALSO, DOUBLER AT FS 360 HAD A .5 INCH CRACK. THE CHORD WAS REMOVED, CORROSION WAS REMOVED FROM AREA IAW SRM 51-10-6. A NEW DOUBLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 5SDR CALA9800567Circumferential · crackedINSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3.SDR CALA9800566Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING STA 656.50 STRINGER ON TOP OF CHORD RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW EA 5762-01050.SDR CALA9800565Skin · erodedINSPECTION FOUND RT SIDE OF LOWER RUDDER SKIN EDGE ERODED JUST ABOVE PANEL NR 9901. THE AREA WAS SANDED AND A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-40-8.SDR CALA9800564Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075.SDR CALA9800563Skin · deterioratedINSPECTION FOUND LT LOWER SIDE OF UPPER RUDDER TAB FIBERGLASS REPAIR DETERIORATED. THE FIBERGLASS REPAIR WAS SANDED, REWORKED, AND PRIMED IAW SRM 51-40-9 AND 51-10-6.SDR CALA9800562Skin · crackedINSPECTION FOUND A .625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1.SDR CALA9800561Angle · crackedINSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.SDR CALA9800560Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN J-ANGLE SUPPORT ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. A REPAIR CHANNEL WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914.SDR CALA9800559Flap Track · corrodedINSPECTION FOUND UPPER MOUNT FLANGE OF NR 6 FLAP TRACK CORRODED AT FORWARD ATTACH CLEVIS. THE FLAP TRACK WAS REMOVED AND REPLACED.SDR CALA9800558Attach Fitting · corrodedINSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING AT BOTTOM OF WING CORRODED AT INBOARD FACE. THE FITTING WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 20-50-01.SDR CALA9800557Angle · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT BOLT HOLES OF LT WING LOWER LEADING EDGE SUPPORT ANGLE AT FS 120. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9800556Stiffener · crackedINSPECTION FOUND A .625 INCH CRACK IN STIFFENER AT BOTTOM OF LT WING LEADING EDGE RIB, WBL 92.0. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9800555Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.SDR CALA9800554Skin · dentedINSPECTION FOUND RT OUTBOARD AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED.SDR CALA9800553Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL SUPPORT T-ANGLE. THE CRACK WAS LOCATED AT INBOARD AFT END, OUTBOARD OF NR 1 FLAP JACKSCREW. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-SDR CALA9800552Floorbeam · corrodedINSPECTION FOUND FLOORBEAM TOP FLANGE UPPER AND LOWER SURFACE CORRODED AT FS 360, RBL 10 TO LBL 10. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.SDR CALA9800551Skin · puncturedINSPECTION FOUND A HOLE IN RT OUTBOARD FOREFLAP UPPER INBOARD SURFACE. THE DAMAGED AREA WAS CUTOUT AND A HOT BONDED REPAIR WAS APPLIED IAW SRM 51-40-6 AND 51-10-6.SDR CALA9800550Flap Track · corrodedINSPECTION FOUND RT WING NR 7 FLAP TRACK FORWARD LUGS CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0.SDR CALA9800549Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.SDR CALA9800548Rib · wornINSPECTION FOUND VERTICAL STABILIZER NR 7 RIB WORN AT STRINGER 2R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.SDR CALA9800547Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LT VERTICAL STABILIZER AT STA 1253, JUST ABOVE AND AFT OF PANEL NR 9523. THREE 1 INCH CRACKS WERE FOUND IN THE LT VERTICAL STABILIZER AT STA 1264. THE CRACKED AREAS WERE CUTOUT IAW SRM 54-10-1. FILLER AND DOUBLER REPAIRS WSDR CALA9800546Bulkhead Panel · crackedINSPECTION FOUND THE NLG WHEEL WELL FORWARD BULKHEAD TOP RIGHT PANEL, TOP LEFT PANEL, AND TOP CENTER PANELS CRACKED AT FASTENER HOLES. THE CRACKS WERE .5 TO 1 IN LENGTH. THE CRACKED AREAS WERE CUTOUT IAW SRM 51-40-2. REPAIR DOUBLERS AND FILLERS WERE FABRICASDR CALA9800545Skin · crackedINSPECTION FOUND A .5 INCH CRACK WITH DENT IN AFT BAGGAGE COMPARTMENT DOOR SKIN 23 DOWN FROM TOP AND 16 AFT. THE DENTED AND CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3.SDR CALA9800544Skin · dentedINSPECTION FOUND C-2 CARGO DOOR AFT LOWER EDGE BENT AND CORRODED. THE AFT LOWER FRAME SECTION WAS REMOVED IAW SRM 51-30-2 AND THE SKIN WAS STRAIGHTENED IAW SRM 51-40-1. THE NEW LOWER AFT FRAME SECTION WAS SEALED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9800543Frame · corrodedINSPECTION FOUND FLOOR MOUNT FRAME CORRODED AT AFT BIN STA 1148 TO 1166 BETWEEN STRINGER 26 TO 27R. A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-40-5 AND SRM 51-30-2.SDR CALA9800542Spar Web · crackedINSPECTION FOUND A 4 INCH CRACK IN CENTER WING SECTION AT REAR SPAR WEB UPPER RADIUS ABOVE PRODUCTION PANEL FROM RBL 0 TO RBL 4. THE AREA WAS REPAIRED IAW EA SA004-5710-01843, DRAWING 65C37620, AND SERVICE BULLETIN 727-57A0182.SDR CALA9800541Radome · erodedINSPECTION FOUND THE RADOME EXTERIOR SKIN HAD SOME SPOTS OF EROSION AND A SMALL HOLE. THE RADOME WAS REMOVED AND REPLACED IAW MM 53-15-0.SDR CALA9800540Rib · crackedINSPECTION FOUND A .25 INCH CRACK FROM END OF STRINGER ON TOP OF RIB, SECOND UPPER STRINGER FROM AFT SPAR, WS 656.50, ACCESS 7217. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-01050.SDR CALA9800539Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL SUPPORT RIB JUST INBOARD OF NR 3 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB SUPPORT WAS REMOVED, NEW PARTS WERE INSTALLED IAW SRM 51-10-6 AND 51-10-1.SDR CALA9800535Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL OUTBOARD SUPPORT RIB JUST INBOARD NR 4 SPOILER ACTUATOR IN FLAP COVE AREA. THE RIB AND ROD WERE REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800534Skin · corrodedINSPECTION FOUND BOTTOM OF LT WING NR 7 SPOILER CORRODED. THE SPOILER WAS REPAIRED BY AVIATION COMPOSITES AND IAW WORK CARD 07-5750-1-2717..SDR CALA9800533Skin · separatedINSPECTION FOUND THE LT ELEVATOR CONTROL TAB INBOARD CORNER SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR CALA9800532Skin · separatedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB TRAILING EDGE SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR CALA9800531Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 846, RBL 1. THE FLOOR SUPPORT WAS REMOVED. A DOUBLER AND FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-1.SDR CALA9800530Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, AND 53-10-3, PAGE 43, DETAIL 11.SDR CALA9800529Subfloor · corrodedINSPECTION FOUND FORWARD LAV OUTBOARD SUBFLOOR CORRODED AT FS 294-344, RBL 43-63. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-1.SDR CALA9800528Skin · gougedINSPECTION FOUND AN 8 GOUGE IN RT INBOARD FOREFLAP INBOARD END AT WING ROOT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-50-00.SDR CALA9800527Angle · crackedINSPECTION FOUND A 2 CRACK IN LOWER LEADING EDGE SUPPORT ANGLE INSIDE LT WING LEADING EDGE AFT OF NR 3 LEADING EDGE FLAP AREA, FSS 120. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.SDR CALA9800526Skin · crackedTHE LT WING LOWER LEADING EDGE HAD A .15625 CRACK WITH LOOSE FASTENERS JUST INBOARD OF CUTOUT ABOVE NR 2 SLAT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-1, AND 51-30-2.SDR CALA9800525Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN BRACKET AT OUTBOARD SIDE WHERE LT WING NR 1 SLAT LOWER SKIN ATTACHES TO INBOARD TRACK. THE BRACKET WAS REPLACED IAW SRM 51-10-1.SDR CALA9800524Bracket · crackedINSPECTION FOUND LT WING LOWER TRAILING EDGE LOOSE BETWEEN NR 2 AND NR 3 SPOILER ACTUATOR. ONE AREA INBOARD OF NR 2 SPOILER ACTUATOR WAS LOOSE/WORN. ANOTHER AREA OUTBOARD OF NR 3 SPOILER ACTUATOR HAD A RIB WITH 2 CRACK AND WORN BRACE ROD. THE BRACKETS AND B
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