Boeing 727-25C
Service difficulty reports · 2,007
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 = '72725C' 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 = '72725C' 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 UPS02239907Flap Track · corrodedINSPECTION TYPE:C+SI #7 FLAP TRACK HAS SURFACE CORROSION ON THE I/B FWD ATTACH LUG. SURFA CE CORROSION ALSO FOUND ON THE FWD ATTACH PAD AND ON THE ON THE I/B FACE OF THE WING ATTACH FITTING. REPAIR CARRIED OUT IAW SMRO EO 20025507. REF. UPS ENGINEERING FILSDR UPS02239912Fitting · crackedINSPECTION TYPE: C & SI, CRACKS FOUND ON FWD OUTBOARD FLANGE OF LT BS 950 FITTING. REPAIRED CRACKS IAW SMRO EO'S 2002-055-002 AND 2002-055-012. REF. UP S EO B727-5310-17901 AND UPS FILE NO. 727-53-20088.SDR UPS02239906Fitting · crackedINSPECTION TYPE:C&SI WHILE CARRYING OUT NDT ON R/H 870 FITTING CRACKS WERE FOUND IN 3 FAS TENER HOLES IN ROW 3, 1ST HOLE FROM BOTTOM AND 3RD & 4TH HOLES FROM BOTTOM R/H 870 FITTING REPLACED IAW EO B727-5310-3057 & DRAWING 65C13724SDR UPS02239897Fitting · crackedINSPECTION TYPE: C & SI, RT MAIN GEAR DOOR ACTUATOR SUPPORT FITTING LUG CRACKED. LUG REPLACED IAW EO B727-3210-2583SDR UPS02239809Butt Joint · corrodedC CHECK FUSELAGE AT SKIN BUTT JOINT BS 260 AND BETWEEN STR 12 RT & 13 RT IS BULGING CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AS PER BOEING DRAW ING 69-62161 AND UPS E.O. B727-5310-1371-F APPENDIX ESDR UPS02239645Light · not seatedEMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOPERATIVE. RESEATED FWD ENTRY DOOR EMERGENCY EXIT LIGHT OPERATIONAL CKS GOOD.SDR UPS02239910Bracket · crackedINSPECTION TYPE: C & SI, NR 12 SPOILER SUPPORT CASTING I/B & O/B BRACKETS ARE CRACKED AT LWR ATTACH HOLES. BRACKETS REPLACED IAW DRAWING 65-17351 & SB 57-84SDR CA020912011Spar · cracked(CAN) RT WING REAR SPAR CRACKED AT STA 200.SDR CA020912010Skin · cracked(CAN) CRACK AT AFT CARGO DOOR CUTOUT SKIN, AFT LOWER CORNER AT FASTNER HOLES.SDR CA020909004Skin · cracked(CAN) ON HEAVY C-CHECK, FIVE CRACKS NOTED AROUND FASTENER HOLES AT BS 610-614, STR 3 LT, IN FUSELAGE SKIN.SDR CA020909003Skin · cracked(CAN) ON HEAVY C-CHECK, CRACKS NOTED AROUND FASTENER HOLE AT BS 488, STR 3 LT, IN FUSELAGE SKIN.SDR UPS02239091Fire Warning · false indicationINSPECTION TYPE:N/A CLIMBING THROUGH 20K GOT WHEEL WELL FIRE LIGHT. LOWERED GEAR AND LIGHT IMMEDIATELY WENT OUT. INSP NOSE AND MAIN GEAR LOOPS, NO DEFECTS FOUND. SYS CHECKS NORMAL. FIRE DET CONTROL PANEL REPLACED REF LP 653351 ITEM 2 M243137.SDR 02FDEA00561Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 1050, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.SDR CA020813015Stringer Clip · cracked(CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1030 AT STRINGER 8 LT. REMOVED AND REPLACED STRINGER CLIP WITH NEW CLIP IAW SRM 51-30-2SDR CA020813014Stringer Clip · cracked(CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1030 AT STRINGER 4 RT. REMOVED AND REPLACED STRINGER CLIP WITH A NEW CLIP IAW 51-30-2.SDR CA020813013Stringer Clip · cracked(CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1050 AT STRINGER 8 LT. REMOVED AND REPLACED STRINGER CLIP WITH A NEW CLIP IAW SRM 51-30-2SDR CA020813012Stringer Clip · cracked(CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1050 AT STRINGER 6 LT. REMOVED AND REPLACED WITH A NEW STRINGER CLIP IAW SRM 51-30-2.SDR CA020813011Stringer Clip · cracked(CAN) DURING C3-CHECK FOUND STRINGER CLIP CRACKED AT BS 1070 AT STRINGER 7 RT. REMOVED AND REPLACED WITH A NEW STRINGER CLIP AT 7R IAW SRM 51-30-2.SDR CA020813010Fitting · corroded(CAN) DURING C3 CHECK FOUND STRINGER END FITTING CORRODED AT BS 740 AT STRINGER 9 LT, REMOVED CORRODED FITTING AND INSTALLED NEW FITTING AT BS 740 AT STRINGER 9 LT IAW SRM 51-30-2SDR 02FDEA00563Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 1030, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.SDR UPS02238974Latch · out of adjustINSPECTION TYPE:N/A, ENTRY DOOR HANDLE UNLATCHED ON LANDING FOUND DOOR ENTRYWAY PARTIALLY OPENED. ALSO ACFT SUFFICIENT TO MAINTAIN PRESSURIZATION IN AUTO/MAN. PERFORMED FWD ENTRY DOOR ADJ FOR SOFT UNLATCHING PER MM 52-11-00.SDR UPS02238717Battery · dischargedINSPECTION TYPE:N/A EXIT LIGHT ABOVE COCKPIT ENTRANCE DOOR DOES NOT TEST. CABIN DOOR ENTRANCE LIGHT CHECKS OK BUT CHARGE STAT US IS IN-DOUBT. R/R EMERGENCY EXIT LIGHT BATTERIES IN COCKPIT ENTRANCE DOOR AND CABIN DOOR, REF UPS 727 M/M CHAP 33-50-67 OPS CHECKESDR UPS02238567Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS GOOD.SDR UPS02238494Light · inoperativeINSPECTION TYPE:PFLT COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY AND CLEANED CONNECTOR TO LIGHT ASSY MOUNTING PLATE, OPS CHECK GOOD PER MM 33-50-67.SDR UPS02238118Skin · corrodedINSPECTION TYPE:N/A CORROSION STA 1148 STRINGER 25L TO 26L. REMOVED CORRODED SKIN AND INTERNAL DOUBLER REPAIRED PER EO B727-5330 -16790-ASDR CA020426003Regulator Valve · failed(CAN) NR 1 ENGINE OIL PRESS RED LINED DURING T/O CLIMB. THROTTLE RETARDED TO IDLE, OIL PRESS BELOW RED LINE. A/C RETURNED TO BASE.OIL PRESS RELIEF/REGULATING VALVE REPLACED. ( O-RING FOUND DAMAGED, COMPLETE ASSY REPLACED)SDR UPS02238090Battery · dischargedINSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERIES, OPS CHECKS GOOD.SDR UPS02237609Control Panel · malfunctionedINSPECTION TYPE:N/A AIR TURNBACK DUE TO SMOKE IN COCKPIT SMELLED SMOKE CLIMBING THROUGH 4000 FT THEN WENT AWAY UNTIL CREW SAW SMOKE AND SMELLED HEAVY ELECTRICAL SMELL AFTER BLOCK IN WITH EXTERNAL POWER CONNECTED. INSPECTED BEHIND PANELS OF F/E PANEL. REMOVEDSDR UPS02237797Angle · bulgedINSPECTION TYPE:C LT AFT NOSE W/W DOOR CUTOUT HAS BULGE FASTENERS PULLING OFF BS 320 TO BS 350. REPLACED LEFT LOWER CHORD ANGLE AT NWW AREA IAW B727 SRM 51-30-2.SDR UPS02237796Skin · crackedINSPECTION TYPE:C LT FUSELAGE SKIN HAS CRACK STARTING AT FASTENER CUT OUT BS 254 STR 10L CRACK DOES NOT NEED STOP DRILL IT RUNS FROM FASTENER HOLE TO EDGE OF SKIN, INSTALLED DOUBLER REPAIR AT LT FUSELAGE. BS 254 STR 10L AS PER B727 SRM 53-30-3 MATERIAL USESDR UPS02237795Skin · bulgedINSPECTION TYPE:C UPPER FUSELAGE SKIN HAS BULGE AT BUTT JOINT BS 521 STR 3L - 4R.SDR UPS02237794Skin · canningINSPECTION TYPE:C RT FWD FUSELAGE SKIN HAS OIL CAN, PREVIOUSLY REWORKED BS 340 STR 19R.SDR 02FDEA00090O-Ring · damagedLOST HYDRAULIC SYS-A QT & PRESS INSTANTLY. REMOVED AND REPLACED O-RING, SERVICED HYD SYS.SDR UPS02237493Battery · dischargedINSPECTION TYPE:IN EMERGENCY EXIT LIGHTS OVER MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES, OPS CHECKS NORMAL.SDR UPS01237360Light · inoperativeINSPECTION TYPE:N/A BOTH EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT ASSY OVER EXIT DOOR P/N ON AND OFF 10-0067, S/N OFF 42-11, S/N O N 27025. OPS CHECKS GOODSDR UPS01237368Light · inoperativeINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT IN COCKPIT INOP HGT SPARE PREFLIGHT. EMERGENCY EXIT LIGHT IN COCKPIT CHARGED AND OPERATIONAL PER 33-50, OPS CHECK GOOD OK FOR SERVICE.SDR UPS01237348Uplock Cable · failedINSPECTION TYPE:N/A DEPARTURE, AFT AIRSTAIR FAILED TO RETRACT (UPLATCH CABLE FAILED) REPLACED UPLATCH CABLE.SDR MVI2001F00000Shaft · shearedAFTER NORMAL APPROACH WITH A GO AROUND FROM 501 AGL, FULL ENGINE POWER WAS ATTAINED ON ALL ENGINES. AT 700 FT, FE NOTED EPR ROLLBACK ON NR 3 ENGINE. ENGINE SUBSEQUENTLY WOULD NOT RESPOND TO POWER SETTINGS AND WAS SHUTDOWN. INSPECTION FOUND FUEL PUMP DRIVE SSDR CA011120012Lap Joint · corroded(CAN) WHILE CARRYING OUT AN EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION OF SPECIFIC LAP JOINTS. CORROSION WAS DETECTED AT STRINGER 24 RT AND LT FROM STA 259 TO 360 AND STRINGER 4 RIGHT STA 1130 TO 1183. AIRCRAFT HAS BEEN FERRIED ON A SPECIAL FLIGHT PERMITSDR CA011109005Skin · corroded(CAN) DURING ROUTINE INSPECTION CORROSION WAS FOUND IN THE FUSELAGE SKIN ABOVE THE MAIN CARGO DOOR BETWEEN BS 500 AND BS 540 AND FROM STRINGER S-3L TO S-4R (LEVEL 3 CORROSION).SDR UPS01237133Window · crackedINSPECTION TYPE:N/A, F/O SLIDING WINDOW CRACKED. REMOVED AND REPLACED NR 2 WINDOW ASSY PER MM 56-12-11. OPS CHECKS NORMAL P/N OFF/ON 5-71762-42 SN OFF 56WIN1244 ON UP01358.SDR UPS01237093Stringer · crackedINSPECTION TYPE:N/A STRINGER 20R CRACKED AT FRAME 294 FWD OF LAV WASTE CHUTE STRINGER REPAIRED AS PER SRM 53-10-03. STATION 319 TO 284.5 REPAIREDSDR UPS02239905Fitting · crackedINSPECTION TYPE:C&SI WHILE CARRYING OUT NDT INSP. OF L/H 870 FTG, RECENT CRACK FOUND FROM HOLE COMMON TO STR. END AT 1ST ROW, ALSO 2 OTHER HOLES HAVE CORROSI ON INDICATIONS L/H 870 REPLACED IAW EO B727-5310-3056-F & DRAWING 65C13724SDR UPS01237036Lap Joint · corrodedINSPECTION TYPE:IN CORROSION AT CREW OXYGEN SERVICE PORT LAP SEAM, STRINGER 19R, STATION 360 TO 344 HAS CORROSION AT LAP SEAM. REMOVED FASTENERS HS 86801 10501 / REMOVED CORROSION HS 86801. VERIFIED REMOVAL OF CORROSION. REINSTALLED FASTENERS AS PER EO B727-SDR 01FDEA00845Slat · failedUPON FLAP RETRACTION NR 6 SLAT FAILED TO RETRACT.SDR 01FDEA00830Duct · crackedPASSING 1500 FT ABOVE GROUND LEVEL NR 3 ENG FIRE LIGHT ILLUM WHEN THROTTLE RETARD. REMOVED AND REPLACED 8TH STAGE BLEED DUCT PER MM 36-00-001-2.SDR UPS01236938Skin · crackedINSPECTION TYPE:C FUSELAGE SKIN SHOW CRACK INDICATION BS 1080 STR 14R NDT FINDING MARKED RUNNING FORM FASTENER HOLE. VERIFICATION SKIN CRACK AT BS 1080 S14R IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4, CUT OUT DAMAGE AREA AT BS 1080 STR 14R IAW B727 SRM 53-3SDR UPS01236752Flap · delaminatedINSPECTION TYPE:W/E RIGHT WING I/B T/E MID-FLAP HAS 3 X 15 INCH DELAMINATION. REMOVED AND REPLACED FLAP IAW MM27-51-03 AND TASK CARD 1 259SDR UPS01236936Skin · crackedINSPECTION TYPE:C FUSELAGE INNER SKIN AT STA 1148-1166 STR 20R CRACKED AND CORRODED OUT OF LIMITS. REMOVE CORROSION FOUND OUT OF LIMITS AS PER SRM 51-10-2, CUT OUT DAMAGED AREA AT STA 1148-1166 STR 20R AND NDT INSPECTION AS PER PART 6 51-00-00 FIGURE 4, NO CRASDR UPS01236937Web · crackedINSPECTION TYPE:C NOSE WHEEL WELL R/T AT STA 277 RIGHT SIDE WALL SHOW CRACK BETWEEN RIVET, CRACK ALREADY VERIFIED IAW P6-51-00-00 FIG 2. REMOVED NOSE LANDING GEAR ACCESS PANEL #3125 RIGHT SIDE FOR REPAIR AS PER 727 SRM 51-30-02, CUT OUT DAMAGE AREA APPROX
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