Boeing 727-228
Service difficulty reports · 1,323
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 = '727228' 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 = '727228' 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 DHL97722003Temp Bulb · failedNR 1 ENG OIL TEMP IN YELLOW ON CLIMBOUT. REDUCED THRUST TO MAINTAIN IN LIMITS, ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED OIL TEMP BULB, CANNON PLUG TO TEMP BULB, OPS CHECK OK.SDR DHL97724004Contl Mech · out of adjustWITH FLAPS UP, NEED 20 TO 25 DEGREE CONTROL WHEEL DEFLECTION TO TURN AIRCRAFT LEFT. DEAD SPOT BETWEEN 0-25 DEGREES. CHECKED AND RERIGGED AILERONS AND SPOILERS PER M/M 27-61-0.SDR DHL97727004Skin · damagedNR 2 LOWER CARGO DOOR DAMAGE ON DOUBLER AND OUTER SKIN LOWER EDGE. INSTALLED DOUBLER REPAIR PER SRM 52-00-3 . FILLER 1 BY 20, DOUBLER 4 BY 24.SDR DHL9872115DBracket · crackedAT D-CHECK, LT WING 32 L/E FLAP ACTUATOR O/B MOUNT BRACKET HAS CRACK AT UPPER FWD END. REPLACED BRACKET PER SRM 57-20-2, 6.5 X 7.75. N/R 1308.SDR DHL97727003Egt Indicator · failedON CLIMBOUT, THE NR 1 EGT DROPPED TO 400DEG CENT. INDICATOR HAD TO BE TAPPED TO RETURN TO NORMAL. REPLACED NR 1 EGT INDICATOR IAW 77-20.SDR DHL97726003Skin · corrosionLEFT HAND INBD AFT FLAP TOP PANEL AT WBL 130.0 HAS PREVIOUS REPAIR 6 PATCH DEPARTING PANEL AND CORROSION ON SKIN SURROUNDING PATCH AREA. TOTAL AREA IS 12 BY 12. REMOVED PREVIOUS REPAIR, CLEANED CORROSION AND PERFORMED REPAIR PER SRM 51-40-6.SDR DHL97722002Skin · crackedFOUND I CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT. C/W EDDY CURRENT INSP, REMOVED RIVETS , ACCOMPLISHED REPAIR PER BOEING S/B 727-53-0198.\SDR DHL97727002Switch · failedTHE NR 1 KREUGER FLAP DID NOT INDICATE DOWN WITH FLAPS AT 5 DEGREES, NO ROLL TENDENCY. REMOVED AND REPLACED THE NR 1 KRUEGER FLAP POSITION INDICATING SWITCH IN ACCORDANCE WITH BOEING 727 MAINTENANCE MANUAL 27-82-1 AND PERFORMED OPERATIONAL CHECK PER BOEING MASDR DHL97722001Fuel Control · malfunctionedDURING CRUISE, NR 1 ENGINE VIBRATION, WITH ALL ENGINE PARAMETERS NORMAL. INSPECTED ENGINE AND REMOVED AND REPLACED FUEL CONTROL PER MM 73-21-1. PERFORMED ENGINE TRIM AND ENGINE POWER TEST.SDR DHL9872670DSupport · corrodedAT D CHECK, FUSELAGE UPPER LOBE INTERIOR FLOOR SUPPORT ANGLE STA 418 BL 24 TO 61 R CORRODED. REMOVED FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-2, 18 LONG. N/R 3787.SDR DHL9872624DSkin · disbondedAT D CHECK, LT OUTBD AFT FLAP AT LE UPPER SURFACES AREAS ARE GOUGED, AND WORN. INSTALLED 3 BONDING REPAIRS PER SRM 51-40-6, 4 BY 12', 8 BY 12 AND 6 BY 12. N/R 1433.SDR DHL9872614DRib · crackedAT D CHECK, RIB CRACKED AT STA 738.5. STOP DRILLED END OF CRACKS AT FLANGE OVER STR 6 AND 8. INSTALLED RIB REPAIRS PER SRM 57-10-5, 10 BY 3 AND 10.5 BY 3. N/R 2263.SDR DHL97724003Bolt · loosePRECAUTIONARY ENGINE SHUTDOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE SHUTDOWN 16 MIN OIL PRESSURE 15 PSI. ENGINE STABILIZED AT FLT IDLE FOR 20 MIN PRIOR. FOUND GEARBOX STUD AT FWD 6 O' CLOCK POSITION LAYING IN COWLSDR DHL97721003Transceiver · malfunctionedWEATHER RADAR WILL NOT RETURN GROUND OR ACTUAL WEATHER. REPLACED RADAR R/T PER MM 34-40, SYSTEM CHECKS OK.SDR DHL97721002Transceiver · malfunctionedDURING CLIMBOUT, RADAR RETURN WHEN TILT ADJUSTED TO PAINT ANY RETURN. PAINTED FROM 9-10 O' CLOCK AND 2-3 O'CLOCK, BUT NOTHING IN BETWEEN. LATER WHEN MANEUVERING, RETURN WAS FROM 1-3 O'CLOCK AND REMAINED THAT WAY FOR 5 MIN. THEREAFTER RETURNS WENT BACK TO FISDR DHL97724001Wire · brokenNR 2 ENGINE OIL TEMP EXCEEDED 157 DEGREES, TEMP EXCEEDED 120 FOR 15 MIN, PEAK TEMP 180. INSPECTED ENGINE OIL TEMP BULB AND OIL COOLER, NO DEFECTS NOTED. FOUND BROKEN GROUND WIRE ON ENGINE CASE, REPAIRED PER M/M 20-70-0. ENGINE RAN AND CHECKED OK ON GROUND.SDR DHL97721001Directional Gyro · malfunctionedNR 2 COMPASS SYSTEM UNUSEABLE WITH DG SELECTED NR 1. HSI'S WORKS NORMALLY. F/O'S RMI SPUN 360 DEGREES. REPLACED NR 2 DIRECTION GYRO. REPLACED F/O'S RMI INDICATOR. PERFORMED COMPASS SLAVING TEST. OPERATIONAL CHECK NORMAL.SDR DHL97726001Wire · chafedJFK - FLT 513 - AT FL 280, S/O NOTED ENGINE NR 3 OIL TEMP INCREASED INTO CAUTION RANGE. ALT PROCEDURE WAS ACCOMPLISHED, AFTER 15 MNUTES OF OPERATING ABOVE 120 DEGREES, ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURE. CLEANED WIRE TERMINALS AT GROUNDING STUD AT ENGINESDR DHL97727001Web · crackedAT A-CHECK, FOUND NOSE W/W RT SIDEWALL PRESSURE WEB CRACKED AT STA 268.5, 6 INCHES BELOW CEILING. STOP DRILLED CRACK, ACCOMPLISHED HFEC OF STOP DRILL HOLES, INSTALLED DOUBLER REPAIR PER S/B 53-0065 AND SRM 51-40-2. DOUBLER 15 BY 6.5, STRAP 1.4 BY 7.6.SDR DHL96720004Stall Warn Vane · brokenBIRD STRIKE ON DEPARTURE, STALL WARNING STICKSHAKER ACTIVATED CONTINUOUSLY UNTIL TOUCHDOWN. BIRD PARTS ON CAPT WINSHIELD, SAW AT LEAST 5 BIG BIRDS BEFORE IMPACT. CLEANED WINDOW AND NOSE AREA INSPECTED, NO DAMAGE. EVALUATED DENT PER SRM, COMPLIED WITH BIRD SSDR DHL96721008Accessory Unit · failedAFTER TAKEOFF FROM MSP COULD NOT SELECT GEAR LEVER PAST OFF. WENT THROUGH ALT PROC. NR 2 GEAR LEVER WILL NOT GO UP PAST OFF AND ALT. PROC #3. A/C SYSTEMS IN GROUND MODE - ALL INDICATIONS ARE THE A/C IS STUCK IN GROUND MODE. REPLACED LANDING ACCY UNIT - SDR DHL9672041CSkin · corrodedAT C-CHECK, FOUND CHORD ANGLE CORRODED IN AFT BAGGAGE COMP STA 950 RBL 15. REMOVED FASTENERS, CUT OUT SKIN 20.5 BY 12, REMOVED CORRODED CHORD ANGLE AND ATTACH STRAP TO L-ANGLE. INSTALLED REPAIR STRAP BETWEEN STR 28R AND 26R, INSTALLED NEW CHORD ANGLE PER SRSDR DHL9672021CFloorbeam · corrodedAT C-CHECK, CABIN FLOORBEAM AT BS 400 LBL 12 HAS HEAVY CORROSION. CUT OUT DAMAGED AREA OF FLOORBEAM, INSTALLED FLOORBEAM REPAIR PER SRM 53-1-8, REPAIR 13.5 LONG.SDR DHL96724007Switch · failedDURING ROTATION, FWD L/E FLAP AMBER LIGHT ILLUMINATED. CONFIRMED WITH S/O L/E FLAP PANEL. NR 1 L/E FLAP INTRANSIT LIGHT WAS ON AND LIGHT REMAINED ON DURING ALL FLAP SETTINGS. REPLACED NR 1 L/E FLAP SWITCH PER MM 27-80.SDR DHL9672040CSkin · corrodedAT C-CHECK, FOUND CORROSION ON INNER SKIN SURFACE AT DRAIN VALVE BETWEEN 28 TO 29R, FWD OF 950. INSTALLED DOUBLER PER SRM 53-30-3 36 BY 15, FILLER 20.5 BY 12.SDR DHL9672023CSeat Track · corrodedAT C-CHECK, CABIN SEAT TRACK STA 1070 LBL 48 FLANGE CORRODED. REMOVED AND REPLACED SEAT TRACK FROM STA 1030 TO 1070 PER SRM 51-10-1.SDR DHL9672039CMount · crackedAT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT O/B SIDE BOTH CORNERS CRACKED. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2, REPAIR 6 BY 8 .SDR DHL9672019CRib · crackedAT C-CHECK, NR 6 SLAT I/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1.SDR DHL9672010CRib · crackedAT C-CHECK, NR 3 SLAT I/B RIB CRACKED. REMOVED AND REPLACED RIB PER SRM 51-10-1.SDR DHL9672001CRib · crackedAT C-CHECK, NR 6 SLAT O/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1 AND 57-30-7.SDR DHL9672014CSkin · crackedAT C-CHECK, FUSELAGE EXTERNAL SKIN CRACKED AT BS 985 S-25L. CUT OUT DAMAGED SKIN, INSTALLED FLUSH REPAIR PER SRM 53-30-3 21 BY 7.SDR DHL9672009CRib · crackedAT C-CHECK, CRACK INDICATION FOUND AT LEFT WING RIB STA 656.5 AT S-2 LOWER ATTACH FASTENER HOLE OLD REPAIR. REMOVED OLD REPAIR, INSTALLED ANGLE REPAIR AT WING RIB PER SRM 57-10-5.SDR DHL96722006Engine · vibrationMIDDLE FREQUENCY VIBRATION FELT IN THE NR 1 THRUST LEVER AT ALL POWER SETTINGS ABOVE 1.4 EPR DURING FLIGHT. RETURNED TO DENVER. PERFORMED ENGINE VIBRATION SURVEY ON WING PER MM 72-00 TEST 1, ENGINE WITHIN MANUAL LIMITS. OK FOR CONT SERVICE.SDR DHL9672022CRib · crackedAT C-CHECK, INSPECTION FOUND CRACK AT WING RIB STA 738.5 STRINGER 2 LOWER AT ATTACH FASTENER HOLE. STOP DRILLED CRACK, HFEC STOP DRILL, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-127. ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-0127, REPAIR 7 BY 3 .SDR DHL9672008CRib · crackedAT C-CHECK, FOUND CRACK AT WING RIB STA 601.5 AT S-3 LOWER FASTENER ATTACH HOLE. STOP DRILLED CRACK, HFEC OF STOP DRILL OK. ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127, ACCOMPLIHED REPAIR PER SRM 57-10-5, REPAIR 9 BY 3.125.SDR DHL9672037CVerical Web · corrodedAT C-CHECK, FOUND CORROSION AT SEAT TRACK LOWER VERT WEB BEAM END AT ATTACHING FITTING INBD SIDE AT LBL 45 STA 870. REMOVED AND REPLACED VERTICAL WEB AND ATTACH FITTING PER SRM 51-10-1.SDR DHL9672024CSeat Track · corrodedAT C-CHECK, CORROSION AROUND FASTENER HOLES ON SEAT TRACK O/B FLANGE LBL 45 FROM STA 947 TO 939. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 950 PER SRM 51-10-1.SDR DHL9672017CSkin · corrodedAT C-CHECK, NR 2 CARGO DOOR INTERIOR SKIN CORRODED ON LOWER STRAP 24 INCHES FROM FWD EDGE AND 24 INCHES FROM LOWER EDGE. REMOVED AND RPLACED DOOR STRAP PER SRM 51-10-1, 1 BY 32.SDR DHL9672015CStiffener · crackedAT C-CHECK, WING CENTER SECTION INTERIOR STIFFENER, RBL 51 FS 740 CRACKED AT LOWER AREA. REPLACED STIFFENER PER SRM 51-30-2, 34 INCHES LONG.SDR DHL9672007CRib · crackedAT C-CHECK, INSPECTION OF LEFT WING REVEALED CRACK AT WING RIB STA 686.5 S-2 LOWER ATTACH FASTENER HOLE. STOP DRILLED CRACK, HFEC OF HOLE, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-0127 AND ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-0127, REPAIR 9 BY 3.125SDR DHL9672027CSeat Track · corrodedAT C-CHECK, CORROSION AND CRACK ON SEAT TRACK LBL 50.5 STA 360 TO 400. REMOVED AND REPLACED SEAT TRACK FROM STA 360 TO 460 PER SRM 51-30-2.SDR DHL9672026CSeat Track · corrodedAT C-CHECK, FOUND CORROSION ON SEAT TRACK STA 680 RBL 45. CUT OUT AND INSTALLED SEAT TRACK FROM BS 650 TO 690 PER SRM 53-10-5.SDR DHL9672025CSeat Track · corrosionAT C-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE STA 680 LBL 47. REMOVED AND REPLACED SEAT TRACK FROM STA 660 TO 690 PER SRM 51-10-1.SDR DHL9672006CRib · crackedAT C-CHECK, LEFT WING INSPECTION REVEALED CRACK AT WING RIB STA 629, ATTACH FLANGE AT S-2 LOWER SIDE. STOP DRILLED CRACK, ACCOMPLISHED HFEC OF STOP HOLE, ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127. INSTALLED ANGLE REPAIR PER SRM 57-10-5 AND S/B 57-0SDR DHL96722007Engine · vibrationENGINE NR 1 HAS ABNORMAL VIBRATIONS IN THRUST LEVER AND ENGINE START LEVERS. GROUND RAN NR 1 ENGINE PER JRH 04-02-01, NOT ABNORMAL VIBRATIONS NOTED THROUGHOUT OPERATING RANGE.SDR DHL96722005Csd · reqd serviceGEN NR 2 HAD 2 LIGHT TRIP EN ROUTE NO FAULT, INDICATIONS ON GEN FAULT PANEL. RESIDUAL VOLTS 14 TO 15 VOLTS AND UNSTABLE FREQS UNSTABLE AT 380 TO 382 CPS. FOUND NR 2 CSD OIL QTY LEVEL AT BOTTOM OF OPERATING BAND. SERVICED CSD PER MM 12-13-12, CHECKS NORMAL MSDR DHL9672038CPlenum Chamber · corrodedAT C-CHECK, CORROSION WAS FOUND ON UPPER WALL OF RAM AIR PLENUM CHAMBER OVER PRIMARY HEAT EXCHANGER. REMOVED HEAT EXCHANGER FOR ACCESS, REMOVED EXISTING DOUBLER, INSTALLED REPAIR PER ENGINEERING ORDER PMSI-135D-1. INSTALLED DOUBLER 15 BY 3.75, DOUBLER 19.5 SDR DHL9672033CRib · crackedAT C-CHECK, RIGHT WING RIB STA 629, LOWER FLANGE AT STR 6 CRACKED. STOP DRILLED CRACK, HFEC INSTALLED REPAIR PER SRM 57-10-5, 3 BY 10.SDR DHL9672020CSkin · crackedAT C-CHECK, LAP SEAM AT STA 328, STR 24R HAS BULGING AROUND RIVETS. REMOVED FASTENERS AT LAP SEAM. CHECKED INNER SIDE OF SKIN, FOUND NO EVIDENCE OF CORROSION. PERFORMED HFEC AT UPPER ROW, NO DEFECTS NOTED. FOUND CRACK AT ATTACH ANGLE RT SIDE BS 328. CUT OSDR DHL9672016CFloorbeam · corrodedAT C-CHECK, FLOORBEAM STA 420 LBL 62 CORRODED. REPLACED FLOORBEAM PER SRM 51-10-1, 24 INCHES LONG.
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