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 FDEA200910073499Stringer · corrodedFWD CARGO COMPARTMENT- CORROSION ON STRINGER 27R AT END SPLICE, BS 740. CUT OUT DAMAGE STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED NEW SECTION STRINGER AND 1EA SPLICE IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED STRINGESDR K11A2009100772401Stiffener · corrodedREAR SPARS STIFFENER CORROSION ON WEB.SDR FDEA200910063491Stringer · damagedFORWARD CARGO AREA, STA 580, STR 21L, DRILL START ON STRINGER. CUT OUT DAMAGED AREA DIM 17 5/8" LONG IAW SRM 51-10-3 FIG 1 REV 101, FABRICATED HAT SECTION, AND 2 EACH SPLICERS 2 EACH CHANNELS, 2 EACH ANGLES AND 2 EACH FILLERS IAW SRM 53-10-3 FIG 1 AND 53-1SDR FDEA200910063493Angle · crackedNR 7 SLAT AFT LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW T-DUCT. REMOVED ACCESS PANEL IAW B 727 SRM 51-30-2. REMOVED LOWER CHORD ANGLE IAW SRM 51-30-2. FABRICATED A NEW LOWER CHORD AND 1 EA SPLICE IAW SRM 57-50-2 FIG 2, AND 51-40-4 FIG 1. TREATED AND PRIMED IASDR FDEA200910063495Skin · damagedDRILL START STA 261 STR 21L. CUT-OUT DAMAGED AREA AND FABRICATED REPAIR FILLER AND DOUBLER IAW B727 SRM 53-30-3 FIGURE 3A. TREATED AND PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS AT BS 261 STRINGER 21LT IAW SRM 53-30-3 FIGURE 3A.SDR FDEA200910063490Web · crackedSTA. 1323, STR 20, LEFT AFT AIRSTAIR EQUIPMENT AREA, CRACK ON WEB. TRIMMED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 5 REV 101 AND SRM 53-10-2 FIG 6 TREATED AND PRIMED IAW 51-10-2 REV 101 INSTALLED DOUBLER AT STA 1323 STR 2SDR FDEA200910063492Skin · crackedNR 7 SLAT INBD HOOK AFT MOUNTING FASTENER IS LOOSE AND EDGE OF COUNTERSINK HAS CRACK INDICATION. HFEC INSPECTED AREA IAW NDTM 51-00-00 PART 6 FIG 23 VERIFIED CRACK ENDS AT EXISTING FASTENER HOLE. FABRICATED DOUBLER FOR NR 7 SLAT INBD AREA IAW SRM 57-50-3 FIGSDR FDEA200910063494Vertical Beam · misinstalledAFT CARGO COMPT, BS 1183 PRESSURE BULKHEAD LBL 17.8 VERTICAL BEAM INBD FLANGE FASTENERS HAVE IMPROPER SPACING IN 4 AREAS. REPAIRED AFT CARGO COMPARTMENT BS 1183 PRESSURE BULKHEAD IAW EA NR 7-53-10-126851.SDR K11A2009100372401Seat Track · corrodedSEAT TRACK HAS CORROSION ON TOP SIDE.SDR CA090827005Switch · unserviceableAFTER GEAR SELECTED UP ON DEPARTURE, NR 3 "REVERSER OPERATING" LIGHT ILLUMINATED. THRUST REVERSER WAS VIEWED TO BE IN NORMAL POSITION AFTER LANDING AND ACFT TAXIED BACK TO RAMP. LIGHT REMAINED ILLUMINATED UNTIL GROUND PWR WAS APPLIED TO THE ACFT. NR 3 "THRUSDR FDEA200908062926Frame · corrodedNO. 2 CARGO DOOR AFT FRAME, STA 990, BETWEEN STR 24R & 25R, EXFOLIATION ON FRAME ABOVE DOOR FITTING. FABRICATED ANGLE REPAIR FROM 15-5 PH .080 PO 290342002 DIM: 18 1/4" X 3 1/2", FABRICATED REPAIR FILLER FROM BAC 1505-10046 PO 2901682 DIM: 3 1/8" X 1 1/8 SDR FDEA200908042916Stiffener · crackedNR 7 SLAT ACT. ATTACH BRACKET I/B SIDE, INSIDE PLATE IS CRACKED. OPENED PANELS 7613, 7614, 7615 IAW MM 28-11-021-4 AND REMOVED STIFFNER AND PLATE ON NR 7 SLAT ACTUATOR IAW SRM 51-30-2. LOCATED AND DRILLED NEW STIFFNER PART 65-17240-24 IAW SRM 51-30-5 AND SDR FDEA200908042894Skin · damagedFUSELAGE OUTER SKIN HAS SCRATCHES AT STA 660 TO ST 700, STR 28L TO STR 28R. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 2 SRM 53-30-3 FIG 1 CUT OUT DAMAGE AREA IAW SRM 53-30--2 FIG 2 SRM 53-30-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 53-30-SDR FDEA200907292833Doubler · crackedLT MLG WING DOOR SKIN IS CRACKED FWD OF AFT HINGE AREA ABOVE SEAL RETAINER REMOVED DOUBLER AND FILLER IAW SRM 51-30-2 AND INNER PANEL IAW SRM 51-30-2 FABRICATED DOUBLER AND FILLER FROM 2024 T3 .050" PO NR 9008729 DIM 14.5" X 8" FOR DOUBLER AND 11" X 5.5" SDR FDEA200907282878Keelbeam · crackedRT W/W KEEL BEAM CHORD ON RT SIDE IS CRACKED AT BS 870 RBL 6. REMOVED AND DISCARDED GUSSET PLATE AND REMOVED FASTENERS ON CHORD IAW EA 7-5310-126839 HFEC SHOWS HOLES ARE FREE OF CRACKS IAW NDTM 51-00- 00 FIG 23 PART 6 TRIMMED OUT DAMAGED CHORD AREA DIM 2 SDR FDEA200907272806Angle · crackedNR 2 SLAT AFT LWR CHORD ANGLE PREVIOUS REPAIR IS CRACKED BELOW T-DUCT. REMOVED INNER ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. REMOVED CHORD ANGLE AT NR 2 SLAT IAW SRM 51-30-2. FABRICATED NR 2 SLAT AFT LWR CHORD ANGLE USING BAC 1514-1559 2024 T3511, PO NR 2SDR FDEA200907272792Actuator · failedFLIGHT TEST-THE NR 2 LED FAILED TO RETRACT AFTER TAKEOFF. NR 2 SLAT ASSY FOUND TO BE RETRACTED WITH ACFT INBOUND AND NR 2 SLAT INTRANSIT AMBER LIGHT ILLUM IN COCKPIT ON FWD PNL AND S/O IND PNL. T/S NR 2 SLAT INDICATION IAW MM 27-82-000-1 AND FOUND TO BE FASDR FDEA200907252756Angle · crackedRT WHEEL WELL VERTICAL ANGLE AT BS 870 IS CRACKED AT RBL 8. REMOVED VERTICAL ANGLE AT RT W/W BS 870 IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 53-10-2 FIG 4, 51-30-5, 51-20-01 REMOVED KEELBEAM PANELS IAW SRM 51-30-2 ALODINED AND PRIMED ANGLE IAW SRSDR FDEA200907252753Angle · crackedRT WING INBD MID-FLAP, LOWER CHORD ANGLE IS CRACKED BELOW INBD MECHANISM, WBL 90. OPENED INBD MIDFLAP INNER PANEL IAW SRM 51-30-2. CUT OUT DAMAGED SECTION DIM 47" IAW SRM 51-10-1 AND 51-40-4 FABRICATED CHORD SECTION FROM BAC1503-100046, PO NR 9008728 DISDR FDEA200907252752Structure · crackedLT IB MIDFLAP LWR AFT CHORD IS CRACKED 4 PL. ON IB CARRIAGE TRACK CUT OUT AND IB ACT ROD CUT OUT. REMOVED INNER SKIN AND TEARDROP FAIRING IAW SRM 51-30-2. REMOVED PREVIOUS REPAIR SECTION DIM 48" IAW SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC 1503 - 100046 SDR FDEA200907232724Frame · crackedFWD CARGO AREA, BS 540, STR 21L - 22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED GILLINER SUPPORT AND FRAME EXTENSION STUB IAW SRM 51-30-2. FORMED STUB FRAME WITH 7075 'O' .063" PO NR 9008655 IAW DWG 53FX 1350 REV A. HEAT TREATED PART FROM 'O' MATERSDR FDEA200907182664Skin · gougedPREVIOUS REPAIR AT BS 620 BETWEEN STR 5L AND STR 8L GOUGED. CUT-OUT DAMAGED AREA. FABRICATED FILLER REPAIR, AND DOUBLER IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1, TREATED AND PRIMED PARTS & AREA IAW SRM 51-10-2, INSTALLED DOUBLER, FILLER REPAIR IAW SRM 51-40SDR FDEA200907182663Skin · damagedPREVIOUS REPAIR AT BS 620 BETWEEN STR 11L AND STR 12L IS GOUGED TRIMMED AREA, FABRICATED FILLER AND DOUBLER REPAIR IAW SRM 53-10-2 FIG 3A AND 51-40-2 FIG 1. TREATED AND PRIMED DOUBLER, FILLER AND AREA IAW SRM 51-10-2, INSTALLED DOUBLER & FILLER REPAIR IAW SSDR FDEA200907162647Rib · crackedNR 6 SLAT RIB IS CRACKED, OTBD SIDE OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIB AT NR 6 SLAT OUTBD SIDE OF ACTUATOR IAW SRM 51-30-2 FABRICATED NEW SLAT RIB, HEAT TREATED RIB TO T6 IAW FAS ENGINEERING REPORT 2-37153-801 REV A VERIFIED HARDNESS IAW NDTMSDR FDEA200907132608Support Angle · crackedAFT AIRSTAIR AREA, RT LWR TORQUE BOX UPPER SUPPORT ANGLE IS CRACKED AT BS 1263. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-10-2, 51-30-5 AND 51-30-6 INSTALLED NEW SUPPORT ANGLE LOWER TORQUE BOX IAW SRM 51-30-2.SDR FDEA200907112587Doubler · crackedAFT AIRSTAIR AREA, LT LWR TORQUE BOX LIGHTNING HOLE HAS CRACK BS 1243 ROUTED OUT CRACKED AREA AT AFT AIRSTAIR AREA LT LWR TORQUE BOX LIGHTNING HOLE BS 1243 IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 AND 51-30-5. TREATESDR FDEA200907022678Frame · crackedFORWARD CARGO, STA 560, STR 21L - 22L, STUB FRAME EXTENSION CRACKED IN RADIUS. REMOVED CRACKED STUB FRAME EXTENSION AT FWD CARGO STA 560 S21-22L IAW SRM 51-30-2. HEAT TREATED STUB FRAME IAW FAS ENG REPORT 2-37153-801 REV A CW CONDUCTIVITY MEASUREMENT IAW NDTMSDR FDEA200906272335Spar · damagedRT WING T/E FALSE SPAR INBD REPAIR HAS LOOSE FASTENER IN THE UPPER SECTION WBL 118. FABRICATED REPAIR PARTS , NEW LOWER CHORD, ANGLE REPAIR , HEAT TREATED 7075 'O' TO T6 CONDITION IAW FAS ER 2-37153-801 REV A, NEW STRAP, TWO RADIUS FILLERS & NEW DOUBLER SDR CA090622011Dome · damaged(CAN) UPON LEVELING AT FL380 AND REDUCING THRUST TO CRUISE POWER SETTINGS, FLIGHT CREW NOTICED THAT NR 2 ENG EXPERIENCED AN ENG STALL. THERE WERE NO FURTHER PROBLEMS DURING REMAINDER OF FLIGHT. UPON ARRIVAL AT DESTINATION, MX CARRIED OUT TROUBLESHOOTING OF NSDR CA090619008Diffuser · cracked(CAN) DURING INSP, FOUND DIFUSSER CASE CRACKED 7-8 IN. ENGINE REPLACED.SDR CA090619007Shroud · delaminated(CAN) FUEL NOZZLE PHENOLIC HEAT SHROUD DELAMINATED AS VIEWED THROUGH THE ENGINE COLD STREAM IN GROUND INSP. UPON FURTHER INSP DETERMINED DIFFUSER CASE CRACKED 7-8 IN. ENG REPLACED.SDR C8GA20090181Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT WING INBD MID-FLAP UPPER T/E IS DELAMINATED. DAMAGED AREA WAS REMOVED DIM 12.5 INCH X 4 INCH. FABRICATED REPAIR FILLER FROM 2024 T3 .016 INCH DIM 12.5 INCH X 4 INCH AND DOUBLER FROM 2024 T3 .020 INCHSDR C8GA20090180Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING REPAIR MAPPING IT WAS NOTED THAT THE EXISTING REPAIR LOCATED ON THE EXTERNAL FUSELAGE SKIN B.S. 300 BETWEEN STRINGER 24R - 26R IS NON-COMPLAINT WITH SRM. REMOVED EXISTING REPAIR, CUT OUT DAMAGE DIM 18" X 15", PERFORMED HFESDR C8GA20090175Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LWR RUDDER RT SIDE UPPER REPAIR ON THE L/E IS CRACKED FIN STA 170. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301 1/4 HD .012" DIM 25" X 12". INSTALLED REPAIR, NO OTHER DEFECTS WSDR C8GA20090174Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LWR RUDDER RT SIDE CTR LWR REPAIR ON THE L/E IS CRACKED FIN STA 110. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301 1/4 HD .012" DIM 25" X 12". INSTALLED REPAIR, NO OTHER DEFECTSDR C8GA20090173Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LOWER RUDDER RT SIDE CTR UPPER REPAIR ON THE L/E IS CRACKED FIN STA 134. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301 1/4 HD .012" DIM 15.5" X 12". INSTALLED REPAIR, NO OTHER DSDR C8GA20090172Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LOWER RUDDER LT SIDE UPPER REPAIR ON THE L/E IS CRACKED FIN STA 87. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301 1/2 HD .012 INCH DIM 25 INCH X 12 INCH. INSTALLED REPAIR, NO OSDR C8GA20090171Skin · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE LWR RUDDER LT SIDE UPPER REPAIR ON THE L/E IS CRACKED. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301.5 HD .012 INCH DIM 25 INCH X 12 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WSDR C8GA20090170Skin · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE UPPER RUDDER RT SIDE LWR REPAIR ON THE L/E IS CRACKED. THE EXISTING REPAIR WAS REMOVED AND NEW DOUBLER WAS FABRICATED FROM 301.5 HD .012 INCH DIM 21.125 INCH X 9.625 INCH. INSTALLED REPAIR, NO OTHER DESDR C8GA20090169Frame · damagedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE FRAME LOCATED AT BS 380 BETWEEN STRINGER 5L AND 6L HAS A HOLE DRILLED IN THE RADIUS. DAMAGED AREA WAS REMOVED DIM .375 INCH X .375 INCH. FABRICATED ANGLE REPAIR FROM 7075 T6 .063 INCH DIM 7.5 INCH X 3.SDR C8GA20090168Skin · crackedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT WING L/E SKIN IS BENT AT THE NR 5 SLAT OTBD TRACK CUTOUT. STOP DRILLED CRACK, PERFORMED HFEC INSP FOR VERIFICATION OF CRACK CONTAINMENT, NO CRACKS NOTED. FABRICATED DOUBLER FROM 2024 T3 .063 INCH DIMSDR C8GA20090167Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT OTBD AILERON T/E IS DELAMINATED ON INBD END. DAMAGED AREA WAS REMOVED DIM 3 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 3 INCH X 3 INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 5 INCH X 5 ISDR C8GA20090166Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE LT OTBD AILERON T/E IS DELAMINATED ON OTBD END. DAMAGED AREA WAS REMOVED DIM. 8 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 8 INCH X 3INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 8INCH X 5 ISDR C8GA20090165Stiffener · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FRAME AT BS 800 AT STR 14R IS CRACKED. DAMAGED STIFFENER WAS REMOVED AND NEW STIFFENER PN BAC1490-2510 WAS INSTALLED. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090164Frame · bentWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FRAME AT BS 970 ABOVE 26L IS BENT. DAMAGED AREA WAS REMOVED DIM 1 INCH X .625 INCH. FABRICATED REPAIR DOUBLER FROM 7075-0 .071 INCH DIM 5.25 INCH X 12 INCH AND HEAT TREATED TO T6. INSTALLED REPAIR, NO OSDR C8GA20090163Frame · bentWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE FRAME AT BS 990 ABOVE 26 L IS BENT. DAMAGED AREA WAS REMOVED DIM 1 INCH X .5 INCH. FABRICATED REPAIR DOUBLER FROM 7075-0 .063 INCH DIM 12 INCH X 4.5 INCH AND HEAT TREATED TO T6. INSTALLED REPAISDR C8GA20090162Frame · bentWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1050 ABOVE 26 R IS BENT. DAMAGED AREA WAS REMOVED DIM 1 INCH X .75 INCH. FABRICATED REPAIR DOUBLER FROM 7075-0 .063 INCH DIM 12 INCH X 12 INCH AND HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER SDR C8GA20090161Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP, CORROSION WAS NOTED BETWEEN STR 29L AND 30 AT THE AFT SHEAR TIE BS. 1166. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED SHEAR TIE AND FABRICATED NEW FROM 7075 T6 .063 INCH DIM 6 INCH X 2.25 INCH, FABRICATED DOUBLER FROM 70SDR C8GA20090160Skin · misrepairedWHILE IN HEAVY MX PERFORMING EXTERNAL REPAIR MAPPING, IT WAS NOTED THAT EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 435 BETWEEN STR 16R-18R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, REMOVED DAMAGED AREA PERFORMED HFEC INSP WITH NO DEFICIENCY. FABRISDR C8GA20090159Skin · misrepairedWHILE IN HEAVY MX PERFORMING EXTERNAL REPAIR MAPPING, IT WAS NOTED THAT THE EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 255 JUST AFT OF THE LT CONTROL CABIN NR 3 WINDOW IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, REMOVED DAMAGED AREA PERFORMED HFEC I
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