Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 96FDEA00450Skin · dentedTWO DENTS IN FUSELAGE SKIN BS 400, STR 17L. ****S/D **** REPAIRED DENTS PER FEDEX SRM 53-30-03, FIG 1.SDR 96FDEA00447Seat Track · corrodedCORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208. *S/D* REMOVED CORRODED SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS PER FDE SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL AT BS 760 TO 848 RBL 25SDR 96FDEA00445Seat Track · corrodedCORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 45 WL 208. *S/D* REMOVED CORRODED SEAT TRACK WELL FROM BS 760 TO 848 LBL 45 WL 208, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL FROM BS 760 T0 848 RBL WL SDR 96FDEA00443Skin · corrodedBULGE IN SKIN LAP BS 1030, STR 26R. *** S/D **** REMOVED FASTENERS FROM SKIN STA 1020 - 1040, STR 26R. REMOVED SHIM, TRIMMED SHIM TO FIT, ALODINED AND PRIMED PER FEDEX SRM 51-10-1. FAY SEALED PER FEDEX SRM 51-20-04. INSTALLED FASTENER PER FEDEX SRM 51-3SDR 96FDEA00442Former · crackedCRACKED FAIRING FORMER BS 720 WL 148 RIGHT. REMOVED AND REPLACED FAIRING FORMER AT BS 720 PLUS 8 WL 148 RT SIDE IAW FEDEX SRM 51-30-2.SDR 96FDEA00441Keel Beam · crackedCRACKS IN LOWER I/B AND O/B FLANGE RADIUS IN RT KEEL BEAM BS 990. *S/D* REPAIRED RT KEEL BEAM PER FEDEX EO 7-5310-7-2356C, PT5 AND FEDEX EA 7-5310-2777B.SDR 96FDEA00440Fairing · gougeGOUGE ON FAIRING 3340, 22 INCHES FROM BOTTOM AND 12 AFT OF PANEL. *S/D* REMOVED DAMAGED AREA 3 FT BY 5 FT .040 AND REPAIRED PER SRM 51-40-2.SDR 96FDEA00439Frame · tornAT FRAME 500 ABOVE STR 24L THERE IS A 1 INCH BY .50 INCH HOLE TORN THROUGH TOP OF FRAME. *** S/D *** REPAIRED PER FEDEX SRM 51-40-03.SDR 96FDEA00438Threshold · crackedFWD CARGO THRESHOLD HAS A ON O/B EDGE AT STA 601. CRACK ON FWD CARGO THRESHOLD AT STA 601 WAS TIG WELDED IAW BOEING DRW NR 65-56169SDR.SDR 96FDEA00437Frame · dentedDENT ON TOP FLANGE OF FRAME AT BS 660, LBL 42, WL 165. ***S/D *** REPAIRED DENTED FRAME AT BS 660, LBL 42, WL 165 IAW FEDEX SRM 51-40-3.SDR 96FDEA00436Frame · dentedDENT ON TOP FLANGE OF FRAME AT BS 660, RBL 33, WL 160. ***S/D*** REPAIRED DENT ON TOP FLANGE PER FEDEX SRM 53-40-03.SDR 96FDEA00435Frame · dentedDENT ON TOP FLANGE OF FRAME AT BS 680, RBL 39, WL 163. *** S/D *** REPAIRED DENT ON FRAME AT BS 680, RBL 39, WL 163, IAW FEDEX SRM 51-40-3.SDR 96FDEA00434Floor Support · corrosionCORROSION (C53-113-01,1) ON FLOOR SUPPORT AROUND NUTPLATE HOLES AT BS 644 RBL 8.5 WL 157.5. REMOVED DAMAGED PORTION OF FLOOR SUPT FABRICATED REPAIR PART AND INSTALLED PER FEDEX SRM 51-40-3.SDR 96FDEA00433Skin · chafedSKIN IS CHAFED AT LAP BS 720D PLUS 12 STR 19L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AS PER FEDEX SRM 53-30-3.SDR 96FDEA00432Skin · chafedSKIN IS CHAFED AT LAP BS 720D PLUS 12 STR 19R. REPAIRED CHAFED SKIN AT LAP BS 720D PLUS 12 STR 19R PER FEDEX SRM 53-30-03 FIG 14.SDR 96FDEA00431Seat Track · corrosionCORROSION (C53-224-01-, 3) AND (C53-224-04) ON SEAT TRACK FLANGE AT BS 950E PLUS 5 RBL 25 WL 208. CANCELLED LLM 1677.SDR 96FDEA00430Fairing Formers · corrosionCORROSION (C53-132-01) ON FAIRING FORMERS BS 740 - 846, WL 138.5, LBL - RBL 10. **S/D *** REMOVED DAMAGED SECTION AND REPLACED WITH NEW PARTS USING OLD PARTS AS A TEMPLATE AT BS 740 - 846, WL 138.5, LBL - RBL 10 IAW FEDEX SRM 51-10-1.SDR 96FDEA00429Frame · damagedDOUBLE AND TRIPLE HOLES IN FRAME STA 1030 BETWEEN STR 8 AND 9R. ***S/D *** ACCESSED AREA, TRIMMED OUT DAMAGED AREA, FABRICATED DOUBLER, INSTALLED FASTENERS AT BS 130 BETWEEN STR 8 AND STR 9R PER EWO 96-2135.SDR 96FDEA00428Seat Track · corrodedCORROSION (C53-224-01) ON BS 740 RBL 45 WL 208 SEAT TRACK I/B FLANGE. REMOVED AND REPLACED SEAT TRACK FROM BS 720E TO 740 RBL 45 WL 208 IAW FEDEX SRM 53-10-5.SDR 96FDEA00427Floor Beam · corrosionCORROSION (C53-224-01, 3) (C53-22404) ON UPPER CHORD OF FLOOR BEAM BS 1110 RBL 35 AND 41 WL 208. REPAIRED UPPER CHORD OF FLOOR BEAM BS 1110 RBL 41 IAW FEDEX SRM 53-10-8. REMOVED CORROSION AT RBL 35 AND FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1.SDR 96FDEA00425Seat Track · corrosionCORROSION (C53-224-02, 3) (C53-224-04) ON SEAT TRACK FLANGES BS 1045 TO 1075 AND 1100 TO 1120 RBL 45 WL 208. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK AT BS 1060 TO 1080 RBL 45 WL 208 IAW FEDEX SR 53-10-5. REMOVED CORROSION FROM SEAT TRACK FLANGES BSDR 96FDEA00422L Angle · crackedCRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B + 10, RBL 14 WL 155. **S/D*** REMOVED CRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B + 10, RBL 14, WL 155. FABRICATED REPAIR PART, DRILLED, ALODINED, PRIMED, AND INSTALLED IAW FEDEX SRM 51-20-1.SDR 96FDEA00421Nose Cowl · dentedNR 1 ENG NOSE COWL LIP RING EXTERNAL SKIN HAS A DENT AT APPROX 9 O'CLOCK POSITION. REMOVED NR 1 ENG NOSE COWL AND SENT OUT FOR REPAIR. INSTALLED SERVICEABLE NR 1 ENG COWL IAW FEDEX MM 71-10-21.SDR 96FDEA00408Mopsill · crackedFOUND MOPSILL AT WL 208 BS 295 TO 304 LBL 50 IS CRACKED. REMOVED AND REPLACED MOPSILL WL 208 BS 295 TO 304 LBL 50.SDR 96FDEA00402Inner Skin · crackedNR 3 CARGO DOOR INNER SKIN HAS A 3 INCH CRACK AFT OF THE FWD EDGE 14 INCHES FROM THE BOTTOM. REMOVED DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-2.SDR 96FDEA00401Act Supt Ftg · gougedMCD AFT ACTUATOR SUPT FITTING IS GOUGED IN THREE PLACES. MCD AFT ACTUATOR SUPT FITTING BLENDED WITHIN LIMITS PER DRW NR 65-48200 AND FEDEX SRM 51-10-6 AND 51-10-2.SDR 96FDEA00384Skin · dentedTWO DENTS IN FUSELAGE SKIN BS 400 STR 17L. REPAIRED TWO DENT IN FUSELAGE SKIN BS 400 STR 17L PER FEDEX SRM 53-30-03 FIG 1.SDR 96FDEA00382Aft Flap · delaminatedRT WING I/B AFT FLAP HAS A 2 INCH DELAMINATED DENT 14 INCHES FROM I/B END UPPER SURFACE. ROUGH DAMAGE IS 5.5 BY 8.25. REPAIRED RT WING I/B AFT FLAP 14 INCHES FROM I/B END UPPER SURFACE IAW SRM 51-40-6.SDR 96FDEA00374Frame · dentedCREASED DENT IN FRAME AT BS 970 BETWEEN STR 26 TO 25L. REMOVED DAMAGED FRAME SECTION, INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-3.SDR 96FDEA00365Chord · corrosionCORROSION (C53-100-01-1) ON UPPER I/B FLANGE OF LOWER RT NOSE CHORD BS 360 TO 344 RBL 16 WL 145 BELLY AREA, ACCESS IS REQUIRED. REMOVED RT LOWER NOSE CHORD AT BS 360 TO 275 RBL 16 WL 145, REPLACED CHORD AND REINSTALLED ALL ITEMS REMOVED FOR ACCESS.SDR 96FDEA00364Frame · corrosionCORROSION (C53-113-01, -2) ON FRAME JUST O/B OF STR 29L AROUND FASTENERS COMMON TO SKIN AND KEEL BEAM, BS 970 WL 138.5 LBL 8. CORROSION WAS OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SHEAR TIE, BS 970 WL 138.5 LBL 8L AND REPAIRED PER SRM 53-10-4.SDR 96FDEA00363G-Beam · corrodedCORROSION BS 267 BL 0 LBL 5 WL 208 ON G-BEAM. REMOVED G-BEAM, DRILLED UP AND INSTALLED NEW G-BEAM. INSTALLED ALL ACCESS PANELS. REMOVED FOR ACCESS TO G-BEAM.SDR 96FDEA00352Skin · gougeGOUGE IN FUSELAGE SKIN AT BS 1223 WL 290 STR 19R, ACCESSING OF THE TORQUE BOX REQUIRED. REMOVED DAMAGE IN FUSELAGE SKIN AT BS 1223 WL 290 STR 19R AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3.SDR 96FDEA00327Press Switch · failedDURING CLIMB, THE NR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. THE THRUST LEVER WAS RETARDED AND THE LIGHT WENT OUT AT EPR BUT AFTER A FEW MINUTES THE LIGHT CAME ON AGAIN AND REMAINED ON. THE ENGINE WAS SHUTDOWN, ALL ENGINE READINGS WERE NORMAL, NRSDR 96FDEA00347Frame · dentedCREASED DENT IN FRAME AT BS 920 BETWEEN STR 26 TO 25L. *S/D* REMOVED DAMAGE FRAME SECTION, INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-3.SDR 96FDEA00346Keel Beam · corrodedCORROSION ON KEEL BEAM (STR 29L) AROUND FASTENERS COMMON TO THE SKIN AT BS 950. *S/D* REMOVED CORROSION FROM S-29L LEFTHAND KEEL BEAM AT BS 950 AND REPAIRED AREAS IAW SRM 27-53-13.SDR 96FDEA00345Chord · corrosionCORROSION (C53-100-01-1) ON UPPER I/B FLANGE OF LOWER RT NOSE CHORD BS 360 TO 344 RBL 16 WL 145, ACCESS IS REQUIRED. *S/D* REMOVED RT LOWER NOSE CHORD AT BS 360 TO 275 RBL 16, WL 145 AND REPLACED CHORD, REINSTALLED ALL ITEMS REMOVED FOR ACCESS.SDR 96FDEA00344Skin · dentedDENT IN SKIN BS 480 BETWEEN STR 22 TO 23R. *S/D* TRIMMED OUT DENT IN SKIN AT BS 480 BETWEEN STRINGER, 22 TO 23R, FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER PER FEDEX SRM 53-30-3.SDR 96FDEA00306Duct · looseTHREE MINUTES AFTER TAKEOFF WITH CLIMB POWER SELECTED 90 PERCENT, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMP RED TAB PROCEDURES AND LIGHT EXTINGUISHED, SYS TESTS GOOD AND NO FURTHER PROBLEMS. INSP STUB WING TEMP SENSORS VALVES AND DUCTS. FOUND LOOSE SDR 96FDEA00304Hydraulic Line · leakingDURING FLAP RETRACTION FOLLOWING TAKEOFF, A-SYS HYD QTY AND PRESS WENT TO 0. ALL CHECKLIST PROCEDURES WERE FOLLOWED, GEAR WAS MANUALLY CRANKED DOWN, 1 AND 2 FLUID SHUTOFFS WERE CLOSED AND ALTERNATE FLAP WAS TURNED ON. GROUND PROXIMITY SYSTEM INHIBITED, FLUIDSDR 96FDEA00195Fuel Control · failedAT IDLE POWER NR 3 ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT. CONTINUED OPERATION UNTIL NR 3 GEN FAILED. ACCOMP ENGINE SHUTDOWN PROCEDURES IAW CHECKLIST PROCEDURES AND LANDING UNEVENTFUL. REMOVED AND REPLACED MAIN FUEL PUMP AND FUEL CONTROL UNITS AS PERSDR 96FDEA00180Bypass Valve · failedON LANDING APPROACH, O/B FLAPS DIDN'T EXTEND WITH FLAP HANDLE, I/B FLAPS OKAY. SUBSEQUENT SYSTEM-A HYD HAD TOTAL LOSS. CHECKLIST, M/GAR EXTENSION AND LANDED OKAY. FOUND O/B TRAILING EDGE BYPASS VALVE BODY SEPARATED. REMOVED AND REPLACED VALVE, LEAK CHECKS SDR 96FDEA00179Uplock Sensor · malfunctionedRT GEAR UNSAFE RED LIGHT ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT REMAINED ON WITH DOOR LIGHT OUT. INSTALLED RT MAIN GEAR UPLOCK SENSOR PER MM 32-61-81, OPS CHECK NORMAL. REPLACED LANDING GEAR ACCESSORY UNIT, MODULE TESTED NORMAL PER 32-09-121.SDR 96FDEA00153Window · leakingCOPILOT WINDOW HAD LOUD WIND RUSH NOISE PASSING APPROX 4000 - 4500 FEET. LEVELED AT 5600 TO INSPECT. WINDOW APPEARED TO BE LEAKING EXCESSIVELY. RETURNED TO DFW. VERIFIED TORQUE. RESEALED AERODYNAMIC SEALANT IAW MM 56-11-0 AND MM SUPPLEMENT. APPLIED SPEEDSDR 96FDEA00133Floorbeam · corrosionCORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IAW FEDEX EA 7-5310-26943.SDR 96FDEA00132Floorbeam · corrosionCORROSION (C53-11-01 AND -3), ON LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1130 FROM RBL 50 TO LBL 38 WL 200. REMOVED CORROSION, FABRICATED REPAIR ANGLE PER EA 7-5310-26949.SDR 96FDEA00128Stringer · corrosionCORROSION (C53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3.SDR 96FDEA00134Skin · damagedBS 710 LBL 6 WL 149 FOUND DEEP GOUGE AT FASTENER HOLE ON EXTERIOR SKIN WHILE WORKING NR 0413. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3.SDR 96FDEA00130Stringer · crackedVERTICAL FIN STA 110, STR 8L IS CRACKED, BAY NR 6. REPAIRED CRACKED STRINGER PER SRM 55-30-4.SDR 96FDEA00084Skin · dentedFIVE DENTS IN SKIN 1050 TO 1056 STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3.
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