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 CALA9801274Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.SDR CALA9801273Skin · delaminatedINSPECTION FOUND LT I/B FOREFLAP UPPER SKIN INBOARD END DELAMINATED. THE FOREFLAP WAS REMOVED, REPAIRED AND REINSTALLED IAW WORK CARD 07-5750-1-2801.SDR CALA9801272Rib · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD CABLE ATTACH RIB (MIDFLAP). THE MIDFLAP WAS REMOVED AND REPLACED IAW WORK CARD 07-5750-1-4703.SDR CALA9801290Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 640, STRINGER 27L. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 3 AND 51-10-2.SDR CALA9801287Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 500 STRINGER 28R. THE CRACKED AREA WAS CUT OUT, STRINGER SPLICE AND SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9801286Skin · corrodedINSPECTION FOUND FUSELAGE SKIN AND STRINGER CORRODED AT STA 720, STRINGER 28L. THE CORRODED AREA OF SKIN AND STRINGER WERE CUT OUT IAW SRM 53-30-3 AND 53-10-3. SKIN AND STRINGER SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-30.SDR CALA9801285Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 680, STRINGER 27R TO 28R. THE CORRODED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-3.SDR CALA9801284Bulkhead Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB SKIN AT STA 1183 BULKHEAD, RT SIDE, WL 188. THE CRACKED AREA WAS CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 553A0022.SDR 99ZZZM77Skin · dentedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A DENT .030 DEEP .5 INCH LONG WITH A SHARP CREASE WAS FOUND AT BS 277 S7R. CUT OUT DENTED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727 SRM 53-20-02, 51-10-02 AND MM 51-20-11. SDR 99ZZZM76Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-1 GALLEY INBOARD SEAT TRACK AT RBL 15 WAS FOUND CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-05 FIG 7, 51-30-02, 53-10-01 FIG 7, 51-30-02 AND MM 51-20-22. (M)SDR 99ZZZM75Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-2 INBOARD SEAT TRACK WAS FOUND CORRODED AT THE FRONT OF THE G-2 GALLEY RBL 21. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-05 FIG 3, 51-10-02, 51-30-02 AND SDR 99ZZZM74Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-2 GALLEY FRONT OUTBOARD SEAT TRACK TERMINATING END WAS FOUND WITH CORROSION. REMOVED SEAT TRACK. FABRICATED AND INSTALLED REPAIR IAW B727 SRM 51-40-03, 51-10-02, 51-30-02 AND MM 51-20-11. (MSDR 99ZZZM73Channel · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, BETWEEN BS 1166 AND 1183 UNDER L2 LAVATORY FLOOR WAS FOUND CORRODED AT LBL 35. REMOVED AND FABRICATED AND INSTALLED FLOOR PAN AND TWO HAT SECTIONS IAW B727 SRM 51-40-02, 51-40-03, 51-10-02, 51-30-02SDR 99ZZZM72Pan · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, BETWEEN BS 1166 AND 1183 UNDER L2 LAVATORY FLOOR WAS FOUND CORRODED AT LBL 35. REMOVED AND FABRICATED AND INSTALLED FLOOR PAN AND TWO HAT SECTIONS IAW B727 SRM 51-40-02, 51-40-03, 51-10-02, 51-30-02SDR TAOA079808Bearing · missingFLT 6480 DCA-LGA - INBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF FROM DCA, DIVERTED TO BALTIMORE WASHINGTON INTERNATIONAL AIRPORT. REPLACED RIGHT INBOARD FLAP JACKSCREW CARRIAGE BEARING FOR ELEPHANT EAR, REPLACED INBOARD JACKSCREW END CAP, OPERATIONAL CHECK NSDR CALA9801296Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-32. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-6, AND 53-10-3.SDR CALA9801295Seat Track · corrodedINSPECTION FOUND SEAT TRACKS CORRODED AT STA 1110 TO 1135, RBL 24 AND AT STA 380 TO 420, RBL 27. THE CORRODED SEAT TRACKS WERE REMOVED AND NEW SECTIONS OF SEAT TRACK WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, AND 51-40-5.SDR CALA9801294Seat Track · corrodedINSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1025, RBL 54 AND LT SEAT TRACK WAS CORRODED BETWEEN STA 344 AND 360, LBL 44.SDR CALA9801291Beam · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE FLAP CORE AREA J BEAM JUST FORWARD OF NR 7 SPOILER CASTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914, 51-10-2, AND 51-30-2.SDR CALA9801289Floorbeam · corrodedINSPECTION FOUND FORWARD ENTRANCE WAY FLOORBEAM CORRODED AT STA 344, LBL 29 TO 60. THE CORRODED AREA WAS CUT OUT, A T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9801288Floorbeam · corrodedINSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 1110, RBL 30. THE CORRODED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, PAGE 18 AND 19.SDR 99ZZZM30Cap · missingDURING CRUISE, NR 2 ENGINE OIL PRESSURE DROPPED BELOW 30 PSI WITH LOW OIL PRESSURE LIGHT ON. MAX OIL TEMP 130 DEGREES C. ENGINE WAS SHUTDOWN. DID TURNBACK. FOUND NR 2 ENGINE OIL CAP MISSING. REPLACED CAP AFTER SERVICING WITH 19.5 QTS OF OIL. CHECKED FOR SDR CALA9801219Sequence Vlv · leakingTHE A SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF FROM CRP. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG LOCK SEQUENCE VALVE LEAKING. THE SEQUENCE VALVE WAS REMOVED AND REPLSDR CALA9801297Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN TOP RT NOSE WHEEL WELL PANEL. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9801293Brace · corrodedINSPECTION FOUND FLOORBEAM SUPPORT BRACE AT STA 1070 TO 1110, RBL 64 AND AT STA 1130, RBL 16 CORRODED. THE SUPPORT BRACES WERE REMOVED IAW SRM 51-30-21. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, 51-10-1, AND 51-10-6.SDR CALA9801292Support · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM SUPPORT BRACE AT STA 848, BL 0 AND A 2 INCH CRACK WAS FOUND IN SUPPORT BRACE AT STA 1110 TO 1130, LBL 36. THE SUPPORTS WERE REMOVED IAW SRM 51-10-1. NEW SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-SDR AALA981359Doubler · corrodedTUL - LIGHT HOUSING AND SKIN DOUBLER CORRODED. TREATED AND PRIMED DOUBLER PER SRM 51-20-0, INSTALLED NEW LIGHT HOUSING PER SRM 51-10-1. (M)SDR AALA981324Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 27R OUTBOARD LEG (VERTICAL) AT STATION 620. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PGS 4C-4E. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED AREA. (M)SDR AALA981322Beam · corrodedTUL - FOUND LOWER SKIN ON DELTA BEAM CORRODED AND BLOWN OUT STATION 744 FWD END. REMOVED DAMAGED WEB. INSTALLED WEB REPAIR PER SRM 51-40-2 FIG 1. (M)SDR AALA981321Floorbeam · corrodedTUL - FOUND CORROSION ON TOP FLANGE OF FLOORBEAM STATION 360 LBL 10 INCHES AT NUTCLIP HOLE. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-8. (M)SDR AALA981320Web · corrodedTUL - FOUND CORROSION ON CHORD STATION 1183 RBL 20. FOUDN AFTER FASTENER REMOVAL OF CHORD ANGLE, CHORD ANGLE DISPLACED. REPLACED ALL FASTENERS TO RESTORE STRUCTURE AT HAT CHANNEL FLOOR PANS AND CHORD ANGLE. REPLACED FLOOR PAN AREA COMMON TO CHORD ANGLE IAW SDR AALA981319Fitting · corrodedTUL - STRINGER END FITTING CORRODED, STRINGER 5R STATION 1183. REPLACED END FITTING 65-24276-10, STRINGER 5 NEW END FITTING PER SRM 51-10-1. (M)SDR AALA981317Frame · dentedTUL - DENT IN FRAME AT 950F STRINGER 25 AND 24 RT. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)SDR AALA981316Frame · crackedTUL - FOUND CRACK IN BELTFRAME AT 950F BETWEEN STRINGER 26L AND 27L. STOP DRILLED CRACK. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)SDR AALA981314Stringer · crackedTUL - UPPER STRINGER CRACKED, 3RD TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57 A159 REV 5. (M)SDR AALA981313Stringer · crackedTUL - TOP FORWARD STRINGER CRACKED AT STATION 656.5 OUTBOARD SIDE. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57A159 REV 5. (M)SDR AALA981312Stringer · crackedTUL - FOUND STRINGER CRACKED 4TH TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER SB 727-57A 159 REV 5. (M)SDR AALA981311Stringer · crackedTUL - STRINGER CRACKED 15L STA 720B FORWARD OF ICE LIGHT HOUSING AT END OF STRINGER. REPAIRED STR 15L FORWARD OF ICE LIGHT STA 720B PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X)SDR AALA981310Stringer · crackedTUL - STRINGER CRACKED 15L STA 720C AFT SIDE OF ICE LIGHT AT END OF STRINGER. REPAIRED STR 15 LT AFT SIDE OF ICE LIGHT STA 720C PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X)SDR AALA981309Stringer · crackedTUL - TOP AFT STRINGER CRACKED, STA 656.56 AT FLANGE HOLE. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SB 727-57 A 159 REV 5. TST: 70,062 HOURS. CYCLES: 49,889. (X)SDR AALA981308Web · crackedTUL - TWO EACH CRACKS IN WEB SKIN FORWARD END RT APU CUT-OUT. STOP DRILLED CRACKS. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2. TST: 70,062 HOURS. CYCLES: 49,889. (X)SDR AALA981307Angle · crackedTUL - NR 2 CARGO DOOR FRAME UPPER CHORD ANGLE WORN AND CRACKED JUST AFT STR 26R (MARKED) (FORWARD EDGE OF DOOR). STOP DRILLED CRACK, FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 51-40-4. (X)SDR AALA981305Skin · corrodedTUL - RIVETS PULLING THROUGH, HEADS CRACKED, STA 1143 TO STA 1149, STR 23L, 4 EACH FASTENERS. FOUND CORROSION BETWEEN DOUBLER SKIN (WHEN REMOVING FASTENERS). REMOVED CORROSION, REPAIRED AREA, INSTALLED DOUBLER AND TRIPLER PER ECO 11697 DATED 6-24-98, REVISEDSDR AALA981304Angle · crackedTUL - FOUND CRACK IN CORNER ANGLE INBOARD OF APU AIR BOX FLANGE. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)SDR 98FDEA00428Air Distribution · odor98-0166 STA-IND: SMOKE FUMES IN COCKPIT AT GEAR CONFIGURATION. SMOKE EMANATED INTO COCKPIT. SMOKE AND FUMES CHECKLIST RUN SMOKE NOTED IN COCKPIT AROMA LIKE WOOD BURNING. GASPER FAN SECURED. SMOKE MAY HAVE DECREASED. AIRCRAFT STOPPED AND EMERGENCY EQUIP RSDR CALA9801199Strap · crackedINSPECTION FOUND A 9/16 CRACK IN STRAP AT LT WING LOWER TRAILING EDGE AT OUTBOARD SIDE OF NR 3 FLAP TRACK MOUNT PAD AFT OF FALSE SPAR AREA. THE CRACKED AREA WAS REMOVED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-4SDR CALA9801192Braces · crackedINSPECTION FOUND FLOORBEAM SUPPORT BRACES CRACKED BETWEEN STA 950A-950B, BL 0, STA 970-990, BL 0, AND STA 720-720A, BL 0. THE CRACKS WERE 1-2.5 LONG. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND 51-30-2.SDR CALA9801191Fitting · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 940, STRINGER 18A. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9801190Panel · crackedINSPECTION FOUND A .5 CRACK AT FASTENER HOLE OF NLG WHEEL WELL TOP CENTER PANEL, STA 290, LBL 2. THE CRACKED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR 98FDEA00418Door Light · illuminated98-0161 - STA-PIT - CLIMBING THROUGH FLIGHT LEVEL 290, MAIN CARGO DOOR LIGHT ON CAUTION LIGHT PANEL ILLUMINATED AND REMAINED ILLUMINATED DURING DIVERSION TO PIT. ACCOMPLISHED RED TAB PROCEDURES. FOUND BUS SUPPLY AND BATTERY CHARGER CIRCUIT BREAKERS POPPED.
Back to Boeing 727-227