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 DL72S980879Rib · crackedFOUND ON E2 LETTER CK, 2 CRACKS IN NR 7 SLAT NOSE RIB AT THE OUTBD SIDE OF THE ACTUATOR. REPAIRED PER MM 57-54-0.SDR CALA9800701Support · crackedINSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800700Support · crackedINSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800699Frame · crackedINSPECTION FOUND A 1 CRACK IN UPPER FLANGE RADIUS OF FRAME 640, RBL 8, FORWARD BAGGAGE BIN. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-3. A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, SHEET A, SRM 51-10-2, AND 51-30-2.SDR CALA9800698Frame · crackedINSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.SDR CALA9800697Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED AT STA 720D. THE CORRODED AREA OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3.SDR DL72S980924Cowl · wornLT FWD ENG COWL SUPPORT RING LIP WORN AT AFT FWD COWL SUPPORT MATING SURFACE, AFT LT EMPENNAGE 6-11 O'CLOCK. REMOVED DAMAGED AREA, WITHIN LIMITS PER SRM 53-10-1 FIG 1 SECTION AT 6:00 AND 7:00 OUT OF LIMITS. FABRICATED REPAIR PER M/M 53-11-0 PG 801 SECTION 7:SDR DL72K980950Skin · crackedTHREE EACH .125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER MM 54-30-0.SDR DL72S980994Skin · crackedC/W ERA 300554-14 CODE 4-54-31 PERM REPAIR, NACELLES/THINNER SKIN, NR 2 ENG FS 1151.68. TIME LIMITED. REMOVED DAMAGED SKIN, FABD REPAIR PER SRM 54-10-3 FIG 13. DYE CKD AND FOUND TO BE REMOVED PER PS 900-6-3 NR 1 REF N/R 398.SDR DL72S980967Angle · crackedANGLE CRACKED IN WING LEADING EDGE, INBD END NR 3 KRUEGER FLAP. DYE CKD TO CONFIRM CRACK. STOP DRILLED, FABD DOUBLER PER SRM 51-40-3, C/W MM 57-20-21 FIG 807.SDR DL72S980966Bracket · crackedAT HMV, FOUND RW ACTUATOR BRACKET CRACKED NR 6 KRUEGER FLAP ACTUATOR BRACKET LOWER O/B FWD CORNER. REMOVED ACT AND BEAM PER MM 57-20-21, STOP DRILLED CRACK, INSTALLED PER MM 57-20-21.SDR DL72S980961Frame · bentFOUND AT HMV, FRAME BENT STA 950E BETWEEN STR 26L-27L. STARTED REPAIR PER SRM 53-10-4, COMPLETED REPAIR PER SRM 53-10-4.SDR DL72S980959Bracket · crackedACTUATOR ATTACH BRACKET CRACKED FWD LOWER INBD CORNER OF NR 5 KRUEGER FLAP. REPAIRED PER M/M 57-20-21 FIG 807.SDR DL72K980937Floorbeam · corrosionCORROSION FLOORBEAM STA 1030 BL 0. REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-20-11.SDR DL72K980914Bear Strap · crackedFOUND ON MV2 CORROSION VISIT, CRACK IN EDGE OF BEARSTRAP AT RT FWD SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REFERENCE SUPPLEMENTAL CARD FOR SI 4-72762-12 ME-02. REPAIRED PER ERA 364614-14 REV A.SDR DL72K981029Bracket · crackedNR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812.SDR DL72K980902Stringer · crackedFOUND ON MV2 CORROSION VISIT, 1 VISABLE CRACK STR 18A RT, AFT OF STA 940 FITTING UPPER AFT ATTACH BOLT. REPAIRED PER M/M 53-12-0.SDR DL72K980900Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21.SDR DL72K980899Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.SDR DL72K980898Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21.SDR DL72S980839Oven · failedELECTRICAL ODOR IN F/C REPORTED BY F/A. REPLACED FIRST CLASS OVEN.SDR DL72S980838Battery Pack · dischargeEMERG LIGHT IN THE COCKPIT IS INOP. REPLACED BATTERY PACK ASSY AND THE BATTERIES CK OK.SDR DL72S980836Fitting · crackedFOUND ON A1 LETTER CK, UPPER FLANGE OF LT INBD TENSION TIE FITTING CRACKED. REPLACED FITTING PER BOEING DWG NR 65-17509 REV M.SDR DL72S980835Rib · crackedFOUND ON A1 LTR CHECK, NR 4 SLAT NOSE RIB CRACKED 1.5 INCH O/B SIDE OF ACTUATOR ROD END. REPAIRED PER M/M 57-54-0.SDR DL72S980833Aux Spar · chafedFOUND ON A1 LTR CHECK, MLG CHAFING FWD SURFACE OF AUX SPAR I/B END. REPAIRED PER M/M 57-43-0.SDR DL72S980832Stiffener · crackedFOUND ON A1 LETTER CK, 2 SPAR STIFFENERS CRACKED AT NR 7 SLAT INBD AND OUTBD STIFFENERS AT THE OUTBD TRACK. REPLACED STIFFENERS PER MM 57-20-21.SDR DL72K980834Battery Pack · inoperativeLT OVRWING EXIT IDENT EMERG LIGHTS INOP. REPLACED BATT PACK M1090, OPS CHKS GOOD.SDR CALA9800677Spar · corrodedINSPECTION FOUND VERTICAL STABILIZER FRONT SPAR FIN STA 87 TO 100 CORRODED ON RT SIDE. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW ENGINEERING ORDER 98-833.SDR DL72S980816Power Supply · inoperativeFOUND EMERGENCY LIGHT SECTION IN CABIN INOP. REPLACED PWR SUPPLY, SYSTEM CHECKS NORMAL.SDR CALA9800676Chord · corrodedINSPECTION FOUND AFT CARGO THRESHOLD LOWER CHORD CORRODED AT FS 950E TO 1010. THE AREA WAS REPAIRED IAW ECRA 5310-03710.SDR CALA9800675Chord · corrodedINSPECTION FOUND CHORD CORRODED AT FS 1179, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-30-2 AND 51-10-1.SDR CALA9800674Floorbeam · corrodedINSPECTION FOUND UPPER CAP OF FLOORBEAM CORRODED AT FS 1130, LBL 60 TO RBL 60. THE FLOORBEAM WAS CORRODED IAW ECRA 5310-03707.SDR DL72S980810Bulb · failedON L/O, FOUND L1 DOOR EMERGENCY LIGHT OUT. RE-LAMPED, OPS CK-OK.SDR DL72S980807Fitting · crackedFOUND ON B2 LETTER CK, LT INBD VERTICAL STAB TIE BOLT FITTING CRACKED 1 INCH AT THE FIRST FASTENER HOLE AFT OF THE TIE BOLT. REPLACED FITTING PER BOEING DRAWING 65-17509.SDR DL72S980806Access Panel · crackedFOUND ON B2 LETTER CK, 4 INCH CRACK ON BALANCE BOARD ACCESS PANEL 9114. REPAIRED PER SRM 55-20-3.SDR DL72S980795Rack · inoperativeEMERGENCY LIGHT OVER AFT LEFT DOOR INOP. REPLACED RACK, OPN GOOD.SDR DL72L980794Battery · dischargedFOUND L-2 UPPER EMERG LIGHT INOP. REPLACED BATTERY. FOUND L-2 LOWER EMERG LIGHT INOP. REPAIRED GND WIRE.SDR CALA9800652Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1130, LBL 24. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9800651Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1070, RBL 20 TO 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.SDR CALA9800650Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110, RBL 0 TO 60. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.SDR DL72S980797Angle · crackedTHE GUSSET ANGLE AT FS 1273 ON THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK. THE GUSSET ANGLE WAS REPLACED WITH A NEW PART PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 364503-14AD.SDR CALA9800649Seat Track · corrodedINSPECTION FOUND RT AFT LAV SEAT TRACK CORRODED BETWEEN STA 1090 TO 1130, RBL 24. A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, PAGE 1 FIGURE 1, 51-10-2 AND MM 51-20-0.SDR DL72S980778Frame · crackedFOUND ON B2 LETTER CHECK, .125 INCH CRACK IN LIGHTENING HOLE LT SIDE STA 1223. REPAIRED PER M/M 53-11-0.SDR DL72L980780Battery Pack · dischargedAFT LT OVERWING EMER SLIDE LIGHT INOP. REPLACED BATT, OPS OK.SDR DL72S980773Battery · dischargedAFT AIRSTAIR EMER LIGHT INOP. REPL BATT, OPS CK OK.SDR CALA9800646Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1010 TO 1030, RBL 48. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1, 51-10-2 AND MM 51-20-11.SDR CALA9800642Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1110 TO 1130, LBL 12. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.SDR CALA9800641Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1130 TO 1150, LBL 12. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.SDR CALA9800632Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 970 TO 1130, RBL 24. A SEAT TRACK REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-05, FIGURE 7, 51-10-2 AND MM 51-30-11.SDR CALA9800631Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED FROM STA 1110 TO 1130, LBL 45. A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2 AND MM 51-20-0.
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