Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 CALA9801729Panel · corrodedINSPECTION FOUND FORWARD CARGO PIT LT TRANSITION PANEL CORRODED FROM STA 530-550. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.SDR CALA9801728Bracket · crackedINSPECTION FOUND A 2 INCH AND 1.5 INCH CRACK IN CABIN FLOOR SUPPORT BRACKET AT STA 303.9, LBL 12. THE FLOOR SUPPORT BRACKET WAS REMOVED AND NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801727Frame · corrodedINSPECTION FOUND CORROSION AT HOLE OF LT UPPER DOOR FRAME STA 1183, WL 273, LBL 19.22. REPAIRED IAW ECRA 5310-03765.SDR CALA9801726Subfloor · corrodedINSPECTION FOUND FORWARD LAV SUBFLOOR CORRODED AT STA 340, RBL 42-60. THE LAV SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-20-1.SDR CALA9801725Skin · corrodedINSPECTION FOUND LT AND RT NOSE SKIN CORRODED AT STA 227-360, STRINGERS 24-29L AND 24-29R. NEW SKIN SECTIONS WERE INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.SDR CALA9801720Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1213. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.SDR DL72L981909Skin · corrodedTHE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND LOCAL REPAIR DOUBLERS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365577-14, REV C SDR CALA9801724T-Chord · corrodedINSPECTION FOUND LT AND RT FUSELAGE T-CHORDS CORRODED AT STA 259-360. THE T-CHORDS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.SDR CALA9801723Support · corrodedINSPECTION FOUND DRAG BRACE SUPPORT DECK AND SIDE T-CHORDS CORRODED AT STA 344-360. THE SUPPORT DECK AND CHORDS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724.SDR CALA9801722Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN RT FUSELAGE FRAME AT STA 930, WL 230 AND 234. THE FRAME WAS REPAIRED IAW ECRA 5310-01397, SRM 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801721Doubler · separatedINSPECTION FOUND LEFT AFT AIRSTAIR EXTERNAL SKIN REPAIR DOUBLER SEPARATING WITH A LOOSE RIVET. THE SEPARATING AREA WAS REMOVED. DOUBLER, FILLER, AND AN ANGLE WERE INSTALLED IAW SRM 51-10-2.SDR CALA9801719Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN LEFT RIB TO SKIN ATTACH ANGLE AND A 2.5 CRACK IN RIGHT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1203. THE ATTACH ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.SDR CALA9801718Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN BOTH INBOARD AND OUTBOARD RIBS OF NR 4 SLAT AT ACTUATOR ROD END ATTACH POINT. THE ACCESS PANEL ON NR 4 SLAT WAS REMOVED IAW SRM 51-30-2. THE CRACKED RIBS WERE REMOVED IAW SRM 51-30-2. NEW RIBS WERE INSTALLED IAW SRM 51-30SDR CALA9801717Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 380, RBL 44 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION OF FLOORBEAM AND SPLICE ANGLES WERE INSTALLED IAW SRM 53-10-8, FIGURE 9, 51-20-4, AND 51-10-2.SDR CALA9801716Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN OUTBOARD TRAILING EDGE ATTACH ANGLE AT RT WING NR 8 FLAP TRACK. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-40-3, 51-10-2, AND MM 51-20-11.SDR DL72S981888Fire Loop · failedENG NR 2 FIRE WARNING CAME ON DURING CLIMB-OUT SHORTLY AFTER T/O, LIGHT STAYED ON AFTER GOING OUT INITIALLY. FOLLOWING THROTTLE BEING REDUCED TO IDLE. SHUT DOWN ENG. BOTH BOTTLES DISCHARGED. REPLACED FIREWALL LOOP, CKS OK. NO FIRE.SDR DL72S981881Frame · crackedREF SHIP NR 482, TPA, LETTER CHK D2, CRACK AT STA 910 FRAME FWD OUTBOARD RADIUS. REPAIRED PER MM 53-11-0.SDR DL72S981880Rib · crackedLT ELEV HINGE SUPPORT RIB CRACKED, ELEV STA 99.79 AFT I/B END. REPAIRED PER MM 55-10-31 FIG 802.SDR DL72S981876Door · departedNOSE GEAR DOORS TORN FROM ACFT ON GEAR RETRACTION. REPLACED DOORS. REPAIRED NR 2 AND NR 3 SLATS. REPAIRED HOLE IN FUSELAGE. REPLACED CUT TIRE.SDR DL72S981875Duct · bentDOGHOUSE AFT LIP, ON AIRINTAKE DUCT 360 DEGREES AREA, BENT AND DISTORTED. HEAVY ACCUMULATION OF SEALER. REMOVED DAMAGE DOUBLER, BEGAN DRILLING NEW DOUBLER. COMPLETED FABRICATION OF NEW DOUBLER PER SRM 54-10-3 FIG 13 D. OK TO INSTALL DOUBLER. INSTALLED REPSDR CALA9801710Panel · corrodedINSPECTION FOUND RT TRANSITION PANEL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 530-560. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-20-1, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801709Strap · crackedINSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SPLICE STRAP AT STA 930, WL 228. THE SPLICE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801697Skin · crackedINSPECTION FOUND A 1 CRACK IN LEADING EDGE SKIN AT LT WING NR 3 SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801696Bracket · crackedINSPECTION FOUND C2 DOOR FRAME AFT SIDEWALL ATTACH BRACKET CORRODED WITH A .25 INCH CRACK AT RIVET. A REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801688Skin · crackedINSPECTION FOUND A 1.9 CRACK IN R-1 DOOR LOWER AFT CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 51-30-21, 51-10-2, 51-40-5, AND ECRA 5307-01141, FIGURE 4.SDR CALA9801687Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN RT WING J BEAM FORWARD OF SPOILER NR 8 ACTUATOR MOUNT FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-07914.SDR CALA9801683Skin · crackedINSPECTION FOUND A 2.5 CRACK IN LT HORIZONTAL STABILIZER UPPER AFT TRAILING EDGE SKIN AT HS STA 195. A DOUBLER WAS INSTALLED IAW SRM 51-20-1, 51-40-5, 51-30, AND 51-20-4.SDR DL72S981868Stiffener · crackedFOUND ON F1 LETTER CK, NR 6 SLAT O/B TRACK O/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.SDR CALA9801682Angle · corrodedINSPECTION FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STA 1166 IN AFT PIT, LT SIDE. THE CORRODED SECTION OF SUPPORT ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801681Spar · crackedINSPECTION FOUND A 1.5 CRACK IN BRACKET AT RT LOWER VERTICAL STABILIZER FRONT SPAR, FS 1218 AN ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.SDR CALA9801680Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166, STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11.SDR CALA9801660Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT C-1 DOOR FRAME. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR DL72L981864Module · inoperativeLDG GEAR WOULD NOT RETRACT AFTER TAKEOFF. HANDLE WOULD NOT GO PAST OFF POSITION. RESET LEVER LATCH CB AND CENTERED STEERING. SAME RESULT. FOUND LANDING GEAR ELECTRICAL MODULE LEVER LATCH FUNCTION INOP. REPLACED MODULE. RAN TEST/ADJ PER MM 32-09-121 PG 50SDR CALA9801652Angle · corrodedINSPECTION FOUND L-ANGLE ON TOP OF DOGHOUSE CORRODED AT STA 294.5, LBL 12. THE L-ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW L-ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801651Bracket · crackedINSPECTION FOUND CRACKED BRACKETS AT LT LOWER VERTICAL STABILIZER FRONT SPAR FITTING AT FS 1218 AND STA 1228. THE CRACKS WERE 1.5 AND 1 INCH LONG. ANGLES WERE INSTALLED AT BOTH LOCATIONS IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.SDR CALA9801650Strap · brokenINSPECTION FOUND RT VERTICAL STABILIZER SPAR ATTACH STRAP BROKEN IN HALF AT STA 1213. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-40-2 AND MM 51-20-11.SDR CALA9801649Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 360, RBL 24.75. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-08 AND 51-30-02.SDR CALA9801648Support · corrodedINSPECTION FOUND FORWARD PIT FLOOR SUPPORT ANGLE CORRODED AT STA 535, RBL 20. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-11.SDR CALA9801647Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT ANGLE IN AFT PIT CORRODED AT STA 1166, LT SIDE. THE CORRODED AREA OF FLOORBOARD SUPPORT ANGLE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801639Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR DL72S981854Battery Pack · dischargedDURING L/O, FOUND OVERWING EMERGENCY EXIT LIGHTS NOT ILLUM AT LT WING STA 804. REPLACED BATTERY PACK, OP CKS NORMAL.SDR DL72S981847Light · inoperativeEMERGENCY LIGHT EXIT SIGN AT L1 DOOR DIM DURING TEST. REPLACED LIGHT MODULE, CKS OK.SDR DL72S981846Battery · dischargedLEFT WING MID BODY FAIRING EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERY.SDR CALA9801630Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 804.5, STRINGER 14L. A 1.5 INCH CRACK WAS FOUND IN FRAME AT STA 804.5, STRINGER 14R. AN ANGLE WAS INSTALLED AT EACH LOCATION IAW SRM 51-30-2.SDR DL72L981837Bulkhead Fitting · crackedFOUND ON F-2 LETTER CK, RT I/B TENSION TIE FITTING CRACKED AFT OF STA 1183 BULKHEAD. REPLACED FITTING PER BOEING DWG 65-17509 REV M.SDR CALA9801629Seat Track · corrodedINSPECTION FOUND LT FUSELAGE SEAT TRACK CORRODED AT STA 1030 TO 1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-10-5.SDR CALA9801628Floorbeam · corrodedINSPECTION FOUND RT FUSELAGE FLOORBEAM CORRODED AT STA 1070. THE CORRODED AREA WAS CUT OUT, TWO ANGLES AND FILLER WERE INSTALLED IAW SRM 53-10-8, FIGURE 8.SDR CALA9801627Intercostal · gougedINSPECTION FOUND INTERCOSTAL WEB GOUGED AT RT FUSELAGE STA 950B BETWEEN STRINGER 29L AND 30L. THE INTERCOSTAL WEB WAS REMOVED. A NEW INTERCOSTAL AND THREE EACH L-ANGLE STIFFENERS WERE INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-0.SDR DL72S981821Angle · crackedREF SHIP 469 TPA LETTER CHK E-2, VERTICAL ANGLE CRACKED RT WHEEL WELL STA 910. REPAIRED PER M/M 53-11-0.SDR CALA9801623Stringer · corrodedINSPECTION FOUND STRINGER 24R CORRODED AT STA 1166. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10-3, 51-10-2, AND MM 51-20-11.
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