Boeing 727-251
Service difficulty reports · 1,181
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 = '727251' 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 = '727251' 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 0001202204Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED PER EA22-170787.SDR 0000652204Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM AT BS 1110, LBL 12 TO RBL 23, WATER LINE 208. REPAIRED PER EA22-170790.SDR 0000882297Line · failedIN CRUISE FLIGHT, THE 'B' SYSTEM LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY PRESSURE FLUCTUATIONS. 'B' SYSTEM QUANTITY DROPPED TO ZERO. CREW PERFORMED COM PROCEDURE AND LANDED WITHOUT INCIDENT. DTW MAINTENANCE REPLACED DEFECTIVE FLEX LINE RUNNING FROM RESERSDR 0000502289Brake Assy · fireUPON ARRIVAL AT GATE, GROUND CREW NOTIFIED COCKPIT CREW OF A FLASH FIRE AT THE RIGHT LANDING GEAR. FIRE WAS QUICKLY EXTINGUISHED. DTW MAINTENANCE REPLACED THE NR 4 BRAKE ASSEMBLY. ALL INSPECTIONS OF MAIN LANDING GEAR WERE NORMAL.SDR USAASB00057Lock Actuator · failedIAD - FLT 2722 - ON CLIMB-OUT FROM IAD, CAPT REPORTED THE RT MAIN GEAR WOULD NOT COME UP ON GEAR RETRACTION. CREW CYCLED GEAR BUT RT MAIN GEAR WOULD NOT INDICATE UP AND LOCKED. FLT RETURNED TO FIELD AT IAD AND LANDED W/O INCIDENT. NO EMERGENCY WAS DECLARED.SDR 0000512298Slide · deployedAT GATE, THE CATERING TRUCK OPENED WRONG SERVICE DOOR WHILE SLIDE WAS STILL ACTIVATED. UPON OPENING THE DOOR, THE SLIDE DID NOT DEPLOY. PHX MAINTENANCE FOUND HINGE POPPED OUT OF SLIDE COVER. MAINTENANCE REPAIRED THE COVER AND REINSTALLED SLIDE.SDR GAIA0091Switch · looseFLT 1849 - FWA-SEA - AFTER TAKEOFF FLIGHT, THE DOOR WARNING LIGHT ON BOTH THE FORWARD PANEL AND FE ANNUNCIATOR PANEL ILLUMINATED. SLOWED AIRCRAFT TO 230 KNOTS, CYCLED GEAR AND WHICH RESULTED IN THE SAME INDICATIONS. THE AIRCRAFT CONTINUED ON TO SEA AND LANDESDR 0000402275Pump · leakingON CLIMB-OUT, B SYSTEM NR 2 PUMP LIGHT ILLUMINATED. CREW REPORTED TOTAL LOSS OF B SYSTEM HYDRAULIC FLUID. CREW RETURNED TO MIA AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED 'B' SYSTEM HYDRAULIC PUMP. LEAK AND OPERATIONAL CHECK GOOD.SDR 0000362287O Ring · failedON APPROACH TO MSP, THE 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. FLIGHT LANDED WITHOUT INCIDENT. MSP MAINTENANCE REPLACED BLOWN O-RING ON ELEVATOR/RUDDER FILTER RETURN MODULE. LEAK AND OPERATIONAL CHECK OK.SDR 0000382287Unknown · odorDURING CRUISE, CREW REPORTED A STRONG ELECTRICAL SMELL IN COCKPIT. PILOT NOTED ODOR COMING FROM THE ENGINEER'S CIRCUIT BREAKER PANEL. FLIGHT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED MULTIPLE TERMINALS, CIRCUIT BREAKERS, AND SWITCHES WITHIN THESDR 0000822293Keelbeam · corrodedDURING ''H'' CHECK, FOUND CORROSION ON LT KEEL BEAM AT BS 950B TO 950C, BS 950C+15 AND BS 950D+15 IN AFT CARGO BAY. REPAIRED PER EA22-170766.SDR 0000842293Floorbeam · corrodedDURING ''H'' CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD. REPAIRED PER EA22-170760.SDR GAIA0064Skin · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 312, THE SKIN WAS FOUND GOUGED AND DENTED BETWEEN STRINGER 20L AND 21L. REPAIRED DAMAGE IAW SRM 51-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0065Stringer · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 360 TO 3790, STRINGER S-18 HAS CORROSION. REPAIRED STRINGER S18 IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0066Frame · gougedDURING C-CHECK AT TIMC/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 640, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO BE GOUGED AT STRINGER S-5R. REPAIRED DAMAGED AREA IAW SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0067Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 660, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO BE GOUGED AT STRINGER S-5R. REPAIRED DAMAGED AREA IAW SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0068Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 294.5, THE FLOORBEAM WEB WAS FOUND TO BE CRACKED AT LBL 54.5. CUT OUT DAMAGED PART OF WEB AND FABRICATED WEB AND DOUBLER. INSTALLED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVSDR GAIA0069Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 948, THE CREASE BEAM WEB WAS FOUND TO BE CRACKED AT LBL 66. REMOVED AND REPLACED WEB IAW SRM 51-20-1 AND 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0070Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 720E, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0071Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 848, IT WAS FOUND THAT THE ANGLED STIFFENER AND FLOORBEAM WEB WAS CRACKED THROUGH AT RBL 45. REPAIRED WEB AND REPLACED ANGLE IAW SRM 51-40-2 AND 51-30-2. THE AIRCRAFT WAS RETURNED TO SDR GAIA0072Plate · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 940, THE LEFT GEAR WELL PRESSURE DECK HAD CRACK INDICATION AT LBL 30. REPAIRED CRACK IAW SB 727-53-0149 AND BOEING DRAWING 65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE (M)SDR GAIA0073Frame · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1166, FUSELAGE FRAME WAS FOUND CRACKED AT FLOOR LEVEL ON THE RIGHT SIDE OF AIRCRAFT. REPAIRED CRACKED FRAME IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0074Skin · damagedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 370 TO 380, THE SKIN WAS FOUND TO BE CREASED BETWEEN STRINGERS S-17L TO S-18L. REPAIRED SKIN IAW SRM 53-30-3, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0075Plate · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 940, IN THE RIGHT WHEEL WELL PRESSURE DECK CRACK WAS FOUND AT RBL 30. REPAIRED CRACK IAW SB 727-53-0149 AND BOEING DRAWING PL65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0076Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1070, CORROSION WAS FOUND ON THE FLOORBEAM UPPER CHORD REPAIR AT LBL 6. REPAIRED FLOORBEAM UPPER CAP IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0077Fitting · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 870, THE BULKHEAD FITTING BELOW STRINGER S-18R, OUTBOARD FLANGE HAS CRACK INDICATION. REPAIRED CRACK IAW S/B 727-53-0116. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0078Skin · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 235.8, THE FUSELAGE SKIN HAD A CRACK INDICATION AT WL 215. REPAIRED CRACK IAW SRM 53-30-3, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0079Plate · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 260, THE NOSE WHEEL WELL SIDE WALL HAS CRACK UNDER DOUBLER EXTENDING PAST FASTENER HOLES. INSTALLED DOUBLER IAW SB 727-53-0065. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0080Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 720D, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0081Skin · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 203, A CRACK INDICATION WAS FOUND AT A FASTENER HOLE AT WL 210. REPAIRED IAW SRM 51-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0082Skin · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 251.6, A CRACK INDICATION WAS FOUND AT A FASTENER HOLE AT WL 210. REPAIRED IAW SRM 51-30-3. THE AIRCRAFT WS RETURNED TO SERVICE. (M)SDR GAIA0083Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 620, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S5R. REPAIRED FRAME IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0084Skin · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT AFT CARGO AFT DOOR INNER SKIN CORROSION WAS FOUND. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0085Skin · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 235.8, FIVE EACH CRACK INDICATIONS WERE FOUND SKIN AT WL 210 TO 220 RIGHT SIDE. REPAIRED IAW SRM 53-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0055Floorbeam · crackedDURNG C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 826, THE WEB IN A FLOORBEAM HAS A CRACK AT THE THROUGH HOLE FOR THE ELECTRICAL CONDUIT, RIGHT SIDE. REPAIRED PART IAW TIMCO REO 500041. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0056Seat Track · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 710, THE SEAT TRACK AT RBL 24 HAS A SPLICE ANGLE CORRODED. REMOVED AND REPLACED SPLICE ANGLE IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0057Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1110, THE FLOORBEAM HAS AREAS OF CORROSION AT SCREW HOLES AT LBL 11, LBL 17 AND LBL 20. REPAIRED FLOORBEAM IAW SRM 53-10-0, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0058Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY AS FOUND AT STATION 1050, THE FLOORBEAM LOWER CHORD WAS FOUND TO BE CORRODED AT RBL 20 TO RBL 45. REPAIRED LOWER CHORD IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0059Frame · gougedDURING C-CHECK AT TIMCO/OSC, THE FOLLWING DISCREPANCY WAS FOUND. AT STATION 720F, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0060Floorbeam · corrodedDURNG C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1050, THE FLOORBEAM LOWER CHORD AND STABILIZATION STRAP WAS FOUND CORRODED AT RBL 26. CLEANED CORROSION ON LOWER CHORD AND WAS FOUND TO BE WITHIN LIMITS. FABRICATED A NEW STABILIZATSDR GAIA0061Seat Track · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 760 TO 848, THE SEAT TRACK WAS FOUND TO HAVE CORROSION AROUND FASTENERS AT LBL 45. REMOVED AND REPLACED SEAT IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0062Stringer · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT THE AFT CARGO FORWARD DOOR SILL, CORROSION WAS FOUND BETWEEN DOOR LATCH FITTINGS. REPAIRED DAMAGED STRINGER IAW TIMCO DRAWING TIO-B727-006, DATED 1-22-00. THE AIRCRAFT WAS RETURNED TO SERVSDR GAIA0063Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1130, THE FLOORBEAM CAP AT LBL 30 HAS CORROSION AT SCREW HOLES. INSTALLED REPAIR IAW TIMCO DRAWING TIO-B727-00005, DATED 1-17-2000. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0086Skin · gougedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1090, A GOUGE WAS FOUND IN THE SKIN AT STRINGER S3L. REPAIRED IAW SRM 53-30-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0087Skin · damagedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT AFT CARGO AFT DOOR A HOLE WAS FOUND. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 0000302202Trim Brake · malfunctionedAFTER TAKEOFF, CREW COULD NOT TRIM STABILIZER. BOTH MANUAL AND CRUISE TRIM WERE INOPERATIVE. CREW FOLLOWED COM PROCEDURE AND LANDED IN ORD WITHOUT INCIDENT. ORD MAINTENANCE REPLACED STABILIZER TRIM BRAKE ASSEMBLY, OPERATIONAL CHECK.SDR 0000832293Web · corrodedDURING ''H'' CHECK, FOUND CORROSION ON VERTICAL STABILIZER TENSION TIE WEB, FORWARD HORIZONTAL LUG LOWER SURFACE AROUND FASTENER HOLES. REPAIRED PER EA22-170771.SDR GAIA0026Light · inoperativeDURING ROUTINE MAINTENANCE AT MHR IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHT OVER THE MAIN ENTRANCE DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 0000112201Switch · failedDURING APPROACH AND GEAR EXTENSION, CREW RECEIVED RED NOSE GEAR WARNING LIGHT. CREW RECYCLED GEAR THREE TIMES AND CONDITION REMAINED. PILOTS VERIFIED MANUALLY THAT NOSE LANDING GEAR WAS DOWN AND LOCKED FLIGHT MADE AN UNEVENTFUL LANDING. DTW MAINTENANCE REPLASDR 0000102201Pump · inoperativeDURING CLIMB-OUT AND PASSING THROUGH 2900 FEET ALTITUDE, THE NR 1 ENGINE EXPERIENCED A FLAMEOUT. THE FLIGHT CREW FOLLOWED COM PRODECURES AND DUMPED FUEL TO ACCOMPLISH PROPER LANDING WEIGHT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RESTART OF THE
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