Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 DHL2006743008Skin · crackedL1 DOOR HINGE LOWER CUTOUT BS 306 HAS .25 INCH CRACK EXTENDING FWD FROM RADIUS. REMOVED ACCESS PANEL FOR REPAIR IAW B727 SRM 51-30-2. TRIM-OUT DAMAGED AREA DIM 1 X 1.250 INCH IAW SB 727-53A0198, VERIFIED CRACK REMOVAL WITH HFEC IAW B727 NDT M, PT6 51-00-00 FSDR C1HA200678005Window · delaminatedEYEBROW NR 4 WINDOW DELAMINATED AND BULGED IN FLIGHT. RAN COM PROCEDURE 2.56.3. REMOVED AND REPLACED L4 WINDOW AND THERMAL SWITCH IAW B727 MM 56-11-31. OPS CK GOOD IAW B727 MM 30-41-31.SDR C1HA200678004Stringer · crackedLEFT MLG BAY STR 18A CRACKED BS 945 (NDT CONFIRMED). ACCOMPLISHED REPAIR AS REQUIRED IAW CHAMPION AIR TASK CARD EO-727-5314-01 REV ORIGINAL, RII ACCOMPLISHED.SDR DHL2006743001Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHT LOW BATTERY, WILL NOT WORK FOR STANDBY POWER CHECK. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT SIGN BATTERIES IAW M/M 33-50-101, CK'S NORMAL P/N MISCO62.SDR C1HA200678001Shear Tie · corrodedPILLOWING AT FASTENERS BS 580 ABOVE STR 27L. CLEANED CORROSION ON SKIN WITH MATERIAL LOSS OF .008, ORIGINAL MATERIAL .063. FABRICATED SHEAR TIE FROM 1506-1388. REPAIRED AREA IAW B727 SRM 53-30-01 FIG 1, AND 53-10-2 FIG 3.SDR C1HA200678002Angle · crackedRIGHT WHEEL WELL VERTICAL ANGLE IS CRACKED AT STA 870 AND RBL 12. REMOVED AND REPLACED VERTICAL ANGLE IN RT WHEEL WELL AT STA 870 AND RBL 12 IAW B727 SRM 51-30-2, P/N 6518636-378, PO 627720.SDR C1HA200678003Pressure Panel · crackedRIGHT WHEEL WELL HAS CRACK AT STA 870 BELOW APU LOAD CONTROL VALUE AT RBL 24. NDT CONFIRMED CRACK THAT ENDS AT FASTENER HOLE. FABRICATED DOUBLERS IAW 727 SRM 53-10-9, FIG 5 AND INSTALLED REPAIRED WEB IAW B727 SRM 3-10-9 FIG 5.SDR XN0A1333Warning System · malfunctionedNOSE GEAR DOOR LIGHT STAYED ON AFTER BLOCK OUT, WENT OUT WHEN BLOCKED IN. INSPECTED NOSE GEAR DOOR LOCKING POSITION LIGHT SWITCHES IAW B727 MM CHAPTER 32-61-71. NO DEFECTS NOTED.SDR XN0A1331Pump · malfunctionedTEN MINUTES INTO FLIGHT SYSTEM -B- HYDRAULIC OVERHEAT LIGHT AND NR 2B HYDRAULIC PUMP LIGHT CAME ON SYSTEM -B- PRESSURE AND QUANTITY GOOD. REMOVED NR 2B ELECTRIC HYDRAULIC PUMP AND REPLACED WITH REPAIRED HYDRAULIC PUMP, OPS CHECK GOOD, LEAK CHECK GOOD IAW B727SDR 06FDEA1966Apu · fireDURING MTC WALKAROUND, FOUND FLAMES COMING FROM FLOW MULT FRESH AIR INLET. IMMEDIATELY SHUTDOWN APU, AND EXTINGUISHED FIRE, FIRED APU FIRED PERFORMED APU START USING ALT FIRE PROT, WITH NO DEFECTS. TURNED ON ENG NR 2 BLEED AIR AND WITHIN 30 SEC. BLEED AIR TSDR DHL2006748003Engine · failedNR 2 ENG FAILED AT APPROX 20000 LOUD BANG SHOOK AIRPLANE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.2.SDR 06FDEA1660Indicator · malfunctionedCAPT HAD NO AIRSPEED INDICATION ON TAKEOFF. REJECTED AT 80 KTS. REMOVED AND REPLACED CAPT'S AIRSPEED INDICATOR PER MM 34-12-021-4. OPS CHECKED GOOD IAW MM 34-12-00.SDR DHL2006743007Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.SDR DHL2006743005Acoustic Panel · delaminatedRIGHT WING PANEL AFT OF APU EXH LARGE DELAMINATION, 10 X 18 WBL 70 TO 90.SDR 06FDEA1530Repair · unknownFOUND REPAIR LOCATED AT STA 720E (WING ROOT) AND STR 19L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE MAJOR, AND WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1529Repair · unknownFOUND REPAIR LOCATED AT 720D AND STR 25L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1528Repair · unknownFOUND REPAIR LOCATED AT STN 1150 STR 21R REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CLASSIFIED AS MAJOR AND WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR DHL2006743004Torque Box · crackedAFT AIRSTAIRS RIGHT SIDE APPROX STA 1253 AND 1273 BELOW RT STAIR CASTING THE STRUCTURE IS CRACKED AND CASTING FOR ACTUATOR RAISES UP WHEN STAIRS STRUTS SEATS ITSELF.SDR PCSA04180601Warning Light · false activationFLIGHT 711 DURING CLIMBOUT FROM MIA THE CREW REPORTED THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, THE CREW PERFORMED THE ABNORMAL PROCEDURE CHECKLIST, THE LIGHT THEN WENT OUT. THE AIRCRAFT LANDED AT MID WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESDR DHL2006743006Fitting · crackedMAIN CARGO DOOR TORQUE TUBE HOOKS HAS CRACKED COUPING ON TORQUE TUBES CENTER HOOK.SDR 06FDEA1443Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1090 STR 26L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA1441Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1100 STR 23R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS CSDR 06FDEA1442Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. REPAIR IS CLASSIFED AS MAJOR PERSDR 06FDEA1440Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS SDR 06FDEA1439Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 415 STR 17R WAS ACCOMPLISHED IAW EO 7- 5313-7-2304 PT2 SECT A, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTING OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP,SDR 06FDEA1419Duct · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMB. COMPLETED QRH AND LIGHT RE-ILLUMINATED. NEW CLAMP DID NOT HELP 8TH STAGE DUCT APPEARS TO BE LEAKING IN PYLON. ALSO, REPLACED SENSE BRAIDED LINE, FOUND BLOWN COMING OFF T-FITING PER BOEING SPM. INSTSDR CA060403028Fuel Control · malfunctionedAT CRUISE ALTITUDE(FL350), THE NR 2 ENGINE WAS SURGING AND DROPPING POWER. ENGINE ANTI ICE AND FUEL HEAT CHECK C/W, NO CHANGE, ENGINE FAILURE- SHUTDOWN CHECK LIST C/W, NR 2 ENGINE SHUTDOWN INFLIGHT. MAINTENANCE INSPECTED AIRCRAFT IAW PW MM 72-00-00 PAGE 531. SDR C8GA20060006Quick Disconnect · looseFLT 1719 FROM MCO TO ATL, DURING TAKEOFF ROLL, FOR’S AIRSPEED INDICATOR BEGAN TO LAG. AFTER TAKEOFF WHILE CLIMBING, GEAR RETRACTED AND FLAPS RETRACTING FOR’S AIRSPEED INDICATOR WENT TO ZERO. AIRCRAFT RETURNED TO MCO WITHOUT INCIDENT. ON POST FLIGHT FOUND FOSDR DHL2006748002Fire Detector · malfunctionedDURING ROTATION SMOKE AND FIRE DET SYS LIGHTS 4&6 ILLUM WITH AFT FIRE MESSAGE AND LOWER CARGO FIRE LIGHT ILLUM ALONG WITH FIRE BELL. DURING INTL CLIMB LIGHT 4 WENT OUT. THEN 4 MIN AFTER FIRST IND LIGHT 6 WENT OUT AS DID AFT FIRE MESG AND LOWER CARGO FIRE LIGSDR DHL2006742001Engine · failedAT 70 KIAS EXPERIENCED LOUD BANG WITH ENGINE FAILURE LIGHT. NR3 ENGINE EGT INCREASED TO 700 C. COMPLETED ENGINE FAIL CHECK LIST ACFT WEIGHT 169.500 IAS 70 KTS OAT 28 G C PA 4860. BRAKE ENERGY NORMAL WIND CALM. REMOVED AND REPLACED NR3 ENG IAW MM 71-00 PERFOSDR PCSA03150601Frame · damagedAFTER FLIGHT 833 ARRIVED IN FDF AND DURING THE CARGO UNLOADING OPERATION THE MAIN CARGO DOOR SILL FRAME SUSTAINED DAMAGE. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR THE INTENDED MAINTENANCE FERRY FLIGHT BACK TO MIA UNPRESSURIZED FOR REPAIR. THE AIRCRAFT FSDR XN0A1308Compressor · stalledCOMPRESSOR STALL (OFF IDLE) NR 2 ENGINE. INSPECTED NR 2 ENGINE INTAKE AND EXHAUST, NO DEFECTS NOTED. PERFORMED ENGINE POWER RUN, NR 2 ENGINE IAW B727 MM 71-00-00, NO DEFECTS NOTED. SUSPECT HIGH CROSS WIND COMPONENT, NR 2 ENGINE NO DEFECT NOTED.SDR C8GA20060004Oil Cooler · failedFLT 1707 FROM PHX TO MEM. DURING CLIMBOUT NR 2 ENGINE OIL TEMP BEGAN RISING. INITATED ENGINE SHUT DOWN AS PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE OIL COOLER BAD. REMOVED AND REPLACED OSDR 06FDEA0798Engine · failedPRECAUTIONARY SHUTDOWN NR 2 ENGINE DUE TO VIBRATION. AIRCRAFT ON GROUND REPORTED SEEING SPARKS COMING FROM NR 1 ENGINE, HOWEVER HAD SEVERE VIBRATION ON NR 2 ENGINE. FAN HAS FOD AND BLADES BROKEN IN HALF, SECOND STAGE DAMAGED, THIRD STAGE IS ALSO DAMAGED, SDR 06FDEA0652Repair · misinstalledREPAIR DOUBLER AT STA BS 1140,STR 25-L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DOUBLER AT STA BS 1140 STR 25-L FOUND NOT IN COMPLIANCE WITH B-727 SRM 53-30-3 FIGURE 1. RESDR 06FDEA0651Floorbeam · crackedE/E COMPARTMENT RIGHT SIDE AT STA BS 420, FLOORBEAM CRACKED AROUND FASTENER AT RBL 25. REMOVED DAMAGED AREA AND FABRICATED 2 EACH ANGLES AND 1 EACH FILLER IAW B-727 SRM 53-10-8 FIGURE 1. ALODINED AND PRIMED BARE METAL IAW B-727 SRM 51-10-2. INSTALLED REPASDR 06FDEA0598Skin · corrodedFOUND CENTER WING TANK LOWER SKIN PANEL HAS INTERGRANULAR CORROSION IN THE LEFT UPPER A/C PLENUM BETWEEN STA BS 795 AND 810 BETWEEN LBL 25 AND LBL 35. REMOVED ALL THE CORROSION,FABRICATED AND INSTALLED EXTERNA L REPAIR DOUBLER,2 EA INTERNAL REPAIR DOUBLESDR DHL2006748001Fire Warning · false activationLOWER CARGO FIRE WARNING SYSTEM ACTUATED AFTER CHANGING TO SHIPS POWER FROM APU POWER. RESET CCHA & CCHB C/B'S; PERF TEST IAW B727 SMM 26-16-0. NO DEFECTS NOTED. VISUALLY INSP FWD & AFT CARGO BELLY PITS; NO DEFECTS NOTED.SDR CIHA200579003Attach Angle · crackedNR 1 ENGINE ATTACH ANGLE, P/N 69-16977-1, CRACKED AT HOLE-P. EDDY CURRENT INSP VERIFIED. REMOVED & REPLACED NR 1 ENG ATTACH ANGLE P/N:69-16977-1 PER ACD (BACDRW) 65-72772.SDR 05FDEA04422Indicator · inoperativeNR 2 EPR WOULD NOT REACH TAKEOFF EPR, NR 2 GAUGE WOULD ONLY REACH APPROXIMATELY 1.55 SETTING. ALL OTHER ENGINE GAUGES READ NORMAL. RELEASED FOR SERVICE PER MEL. NR 2 ENGINE EPR INDICATOR, INOP. RAN NR 2 ENGINE TO TEST EPR INDICATOR AND INDICATOR CHECKS GOOSDR 05FDEA04378Indicator · inoperativeNR 3 EPR GAUGE DID NOT MOVE WHEN THROTTLES ADVANCED FOR TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 CATEGORY: A EXPIRATION: 23DEC05 "MEL 77-01-01: NR 3 ENGINE EPR INDICATOR INOP."SDR PCSA12020501Unknown · noisyAFTER DEPARTURE FLT 8412 CLIMBED TO CRUISE FL320, REPORTED ACFT EXPERIENCED A LOUD BANG & SUBSEQUENT SIGNIFICANT VIBRATION, RETURNED, VIBRATION FELT BY CREW SEVERAL TIMES PRIOR TO LANDING. MX PREFORMED A VISUAL INSP OF THE NR 1, 2, & 3, ENG INTAKES & EXHAUST ISDR 05FDEA03930Repair · unknownEXISTING EXTERNAL REPAIR WITH BLIND FASTENERS AT BS 1217 S28R 4" BY 4" BY 0.032". REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THIS REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91417. REPAIR WSDR DHL2005748001Light · malfunctionedL1 DOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON DURING TEST. REMOVED AND REPLACED EXIT LIGHT ASSY, OPS CK GOOD PER B727 AMM 33-50-101.SDR 05FDEA03825Repair · unknownEXISTING EXTERNAL REPAIR ON FUSELAGE BS 376 STR 21R-22R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91422. DETERMINED TO BE A MAJOR REPAIR.SDR 05FDEA03770Repair · damagedEXISTING REPAIR ON LEFT HORIZONTAL STAB LEADING EDGE WITH SOLID FASTENERS AT L/E STA 61.0 10" WIDE BY 10" LONG. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR, SDR 05FDEA03769Repair · damagedEXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 710 - BS 720 18", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING STR REPAIR AND FABRICATED AND INSTALLED REPAIR PSDR 05FDEA03775Repair · improperFOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY BS 643 - BS 660 S27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR BS 646 TO 660SDR 05FDEA03774Repair · improperFOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 675 - BS 699, S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR AT STR 27R BS 675-699 AND FOUND REPAIR DSDR 05FDEA03773Repair · improperEXISTING FRAME REPAIR IN FWD CARGO BAY, BS500, S23L - S25L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING FRAME REPAIR BS 500 STR 23-25L/H FABRICATED ALODINED PRIMED AND
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