Boeing 727-30C
Service difficulty reports · 931
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 = '72730C' 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 = '72730C' 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 DHL9770143CWeb · crackedDURING C-CHECK, NOSE W/W LEFT SIDEWALL PRESSURE WEB CRACKED 4 ABOVE LOWER CHORD, BS 282 W/L161. CUT OUT DAMAGED SECTION AT W/L 161 BS 282 (3 BY .75) PER BOEING S/B 727-53-0145. INSTALLED DOUBLER AT NOSE W/W LEFT SIDEWALL PRESSURE WEB AT BS 282 W/L 161 ABOUT SDR DHL9770130CWeb · corrodedDURING C-CHECK, CORROSION BULGES UNDER SHEAR WEB AROUND FITTINGS AT BS 500, 520, 540 LBL 57. REMOVED FASTENERS AND CUT OUT DAMAGED AREA ON SHEAR WEB, BS 540 LBL 57 PER SRM 51-40-2, SIZE 4.5 BY 3.5. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, AT BS 540, LBL 57.SDR DHL9770126CSeat Track · corrodedDURING C-CHECK, OUTBOARD FLANGE OF SEAT TRACK HAS HEAVY CORROSION AT BS 360 TO 380, LBL 65 STRAP ON TOP OF SEAT TRACK FLANGE. REMOVED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF TRACK FROM BS 360 TO 380, LBL 65, N/R 3617.SDR DHL9770112CFrame · crackedDURING C-CHECK, THE INNER FLANGE OF FRAME AT BS 560 STR 6 RT WAS FOUND CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4, N/R 3489.SDR DHL9770110CFrame · crackedDURING C-CHECK, FOUND THE INBOARD FLANGE OF FRAME CRACKED 4 ABOVE FLOOR LEVEL RIGHT SIDE BS 500. CUT OUT DAMAGED AREA AT BS 500 FRAME RT SIDE ABOVE FLOOR LEVEL IAW SRM 51-40-3. INSTALLED DOUBLER REPAIR 8 BY 4 PER SRM 51-30-2, N/R 3486.SDR DHL9770107CSkin · corrodedDURING C-CHECK, FOUND CORROSION AT BS 1183 STR 10L. REMOVED DAMAGED AREA ON FUSELAGE AT STA 1183, STR 10 LEFT(3.3125 BY 5.75) PER SRM 53-30-3 FIG 3. REMOVED CORROSION BETWEEN DOUBLER SKIN ON FUSELAGE. MATERIAL LOSS .002, INSTALLED DOUBLER REPAIR PER SRM 53-SDR DHL9770102CRib · crackedDURING C-CHECK, C/W RIGHT WING O/B WS 656.5 RIB INSPECTION PER S/B 727-57-127. INSPECTED RIB PER S/B 27-57-127R3 WS 656.5, FOUND RIB CRACKED AT LOWER FLANGE, NR 2 STRINGER AFT OF FORWARD SPAR. STOP DRILLED CRACK AND REPAIRED PER S/B 57-127. REPAIR SIZE 10.5SDR DHL9770128CStrap · corrodedDURING C-CHECK, CABIN STRAP ON TOP OF INBOARD FLANGE OF SEAT TRACK HAS HEAVY CORROSION, RBL 65 BS 360 TO 380. REMOVED AND REPLACED DAMAGE SECTION OF SEAT TRACK FROM BS 360 TO 380 RBL 65 PER SRM 51-30-2, N/R 3621.SDR DHL9770113CFrame · crackedDURING C-CHECK, FOUND INNER FLANGE OF FRAME CRACKED AT BS 600 RT, 4 ABOVE FLOOR LEVEL. REMOVED DAMAGE FROM FRAME AT BS 600 RT. INSTALLED REPAIR TO FRAME (8 BY 4) IN ACCORDANCE WITH SRM 51-30-2, N/R 3490.SDR DHL9770173CFitting · crackedAT C-CHECK, CRACK AT BS 940 FITTING AT FLOORBEAM ATTACH LBL 59 UPPER FLANGE AFT SIDE MOST INBD. ACCOMPLISHED HFEC FOR CRACKS, CUT OUT DAMAGED AREA. ACCOMPLISHED HFEC OF AREA, INSTALLED REPAIR ANGLES PER BOEING TELEX32-9430 AND DRAWING 65C19121DN.SDR DHL9770172CFitting · crackedAT C-CHECK, CENTER ENGINE INLET DUCT HOUSING ATTACH FITTING AT BS 1182 LT IS CRACKED AT OUTBD LUG. REPLACED ATTACH FITTING PER SRM 51-10-1.SDR DHL9770169CFitting · corrodedAT C-CHECK, CORROSION ON STA 1183, STR 20L UPPER T-FITTING. REMOVED AND REPLACED PER SRM 51-10-1.SDR DHL9770156CFloorbeam · corrrodedAT C-CHECK, UPPER SURFACE OF FLOORBEAM HAS CORROSION AT FS 328, LBL 30. CUT OUT DAMAGED SECTION OF T-ANGLE. INSTALLED ANGLE PER SRM 51-40-4 PER SRM 51-40-4. ANGLE 5 LONG, STRAPS 16 LONG.SDR DHL9770155CFloorbeam · corrodedAT C-CHECK, UPPER FLANGE OF FLOORBEAM HAS 2 CRACKS ON FWD SIDE, UNDER SIDE AT FS 480 LBL 15 AND LBL 31. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-8 FROM LBL 14 TO LBL 35. T-ANGLE 21 LONG, SUPPORT ANGLE 31 BY 2.5 BY 1, RADIUS FILLER 31 BY 2.5 BY 1SDR DHL9770154CSeat Track · corrodedAT C-CHECK, CORROSION ON UNDERSIDE OF SEAT TRACK LBL 24 FS 495 TO 560 INBD AND OUTBD SIDE. REMOVED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-37-2 FROM STA 480 TO 590.SDR DHL9770152CFrame · crackedAT C-CHECK, AFT CARGO CIRCUMFERENTIAL FRAME CRACKED AT STA 1090 ABOVE STRINGER 27L. ROUTED OUT CRACK, HFEC INSTALLED DOUBLER AT STA 1090 STR 27L PER SRM 53-10-4. REPAIR .75 BY 8.SDR DHL9770114CSkin · crackedDURING C-CHECK, THE RIGHT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED AT FASTENERS AT W/L 218, BS 251.6 AND 227.8. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA AT W/L 218 STA 227.8 DIMENSIONS 2 BY 1 AND W/L 218 STA 251.6 STA 227.8 DIMENSIONS 1 AS PER S/B 727-53-SDR DHL97702004Switch · dirtyON TAKEOFF, THE EQUIPMENT ACCESS LIGHT CAME ON. DEFERRED PER MEL 52-4, VERIFY ACCESS DOORS SECURED PRIOR TO DEPARTURE. CLEANED AND LUBRICATED DOOR SWITCH PER MM 52-70, CLEARED DEFERRED ITEM.SDR DHL9770170CWindow Post · crackedAT C-CHECK, CRACK INDICATION ON COCKPIT WINDOW POST RIGHT HAND E-POINT. REMOVED PAINT AND FASTENERS PER S/B 53-0086. REMOVED FILLER AND ACCOMPLISHED NDT. FOUND NO EVIDENCE OF CRACK. INSTALLED DOUBLER REPAIR PER S/B 53-0086.SDR DHL9770164CBrackets · crackedAT C-CHECK, L/E FLAP NR 6 ACTUATOR BRACKETS CRACKED AT I/B AND O/B SIDES UPPER AND LOWER ATTACH LUGS. REMOVED BRACKETS, INSTALLED BRACKETS PER SRM 51-40-3 .SDR DHL9770163CRib · crackedAT C-CHECK, L/E LOWER CHORDS CRACKED AROUND BOLTS AT WS 120 I/B AND O/B SIDES. REMOVED LOWER CHORD. REPLACED CHORD PER SRM 51-40-3 AND 51-20-2. REPAIR 1 BY 1.SDR DHL9770160CFitting · corrodedAT C-CHECK, NR 3 SLAT RIB BULGED AT O/B TRACK ATTACH FITTING. CORROSION FOUND ON FITTING. REPLACED FITTING PER SRM 51-10-1.SDR DHL9770158CSupport · corrodedAT C-CHECK, CORROSION ON COCKPIT FLOOR NEXT TO F/E SEAT TRACK, STA 268 RBL 0 TO 4. REMOVED SEAT TRACK SUPPORT AND INSTALLED NEW SUPPORT PER SRM 51-30-2.SDR DHL9770157CAngle · corrodedAT C-CHECK, CORROSION ON FRAME ATTACH ANGLES AT CENTER SECTION UPPER SKIN AT FS 760 RBL 63 TO 66. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-4, 1 BY 1 BY 6.SDR DHL9770153CFrame · crackedAT C-CHECK, AFT CARGO CIRCUMFERENTIAL FRAME AT BS 1050 HAS CRACK BETWEEN STR 26R AND 25R. CUT OUT DAMAGED AREA, PERFORMED HFEC AND INSTALLED REPAIR PER SRM 51-40-3. FILLER 2 BY 1, DOUBLER 12 BY 2.5 BY 1.SDR DHL9770142CWeb · crackedDURING C-CHECK, NOSE W/W LEFT SIDEWALL PRESSURE WEB CRACKED AFT OF LOWER EDGE OF AFT ACCESS PANEL W/L 172, BS 282 TO 283. CUT OUT DAMAGED SECTION AT W/L 172, BS 282 TO 283 (2 BY .75) PER BOEING S/B 727-53-0145. INSTALLED DOUBLER AND STRAP AT LEFT SIDEWALL W/SDR DHL9770108CSkin · crackedDURING C-CHECK, FOUND THE FORWARD CARGO DOOR CUTOUT SKIN CRACKED IN THE LOWER FORWARD CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR PER THE SRM 53-30-3. REPAIR SIZE 6 BY 8, N/R3465.SDR DHL9770103CSkin · dentedDURING C-CHECK, NUMEROUS DENTS WERE FOUND ON O/B AILERON UPPER SURFACE OUTBOARD END NEAR T/E. REMOVED DAMAGED SKIN AND INSTALLED HOT BOND REPAIR PER SRM 51-40-6 AND 51-20-3 ON OUTBOARD AILERON UPPER SURFACE O/B END TRAILING EDGE. REPAIR SIZE 12 BY 48, N/R 20SDR DHL9770171CBracket · crackedAT C-CHECK, TAIL SKID COMPT UPPER LEFT SUPPORT ROD AFT ATTACH BRACKET CRACKED. REMOVED AND REPLACED ATTACH BRACKET.SDR DHL9770161CFitting · corrodedAT C-CHECK, NR 3 SLAT RIB BULGED AT I/B TRACK ATTACH FITTING. REPLACED FITTING PER SRM 51-30-2.SDR DHL9770167CAngle · crackedAT C-CHECK, FOUND CORROSION/CRACK ON SPANWISE CHORD AT CEILING STA 351 BL 0. REMOVED AND REPLACED SPANWISE CHORD ANGLE PER SRM 51-30-2.SDR DHL9770159CFloorbeam · corrodedAT C-CHECK, CORROSION ON CABIN FLOORBEAM 804 LEFT O/B END ATTACH TO WING CENTER SECTION. REMOVED DAMAGED LOWER CHORD FROM FLOORBEAM, INSTALLED ANGLE AND STRAP REPAIR PER AVITAS EO DRAWING 97PMSI152D-5. REPAIR 6 BY 3 AND .75 BY 6 (STRAP).SDR DHL9770162CRib · crackedAT C-CHECK, C/W WITH LEFT WING RIB CHORD INSP BL 70.5. REMOVED FASTENERS, NDT FASTENERS HOLES CRACK INDICATION NOTED, STOP DRILLED, HFEC STOP DRILL. ACCOMPLISHED S/B 57-112, INSTALLED FASTENERS.SDR UPS97222408Light · inoperativeINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT TURN ON WITH SWITCH IN ON POSITION. REPLACED BATT ON EMERGENCY EXIT LIGHT, OPS CKS NORMAL.SDR DHL9770214DFrame · crackedAT D-CHECK, FRAME INNER FLANGE CRACKED 4 ABOVE FLOOR AT BS 580 RIGHT SIDE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR AT STA 580 PER SRM 53-10-4, SIZE 21 X 6 AND 21 X 3.5.SDR UPS97222084Trunnion · wornINSPECTION TYPE: SP. RIGHT MLG TRUNNION FITTING HAS 4 EACH OUT OF ROUND HOLES AT LOWER REAR SPAR STA. 224.5. HOLES GO THROUGH FITTING, LOWER REAR SPAR AND REAR SPAR WEB. ITEM FOUND WHEN FITTING WAS REMOVED FOR FUEL LEAK. OVERSIZED HOLES IAW DHC SK-906-84SDR 97ZZZX1023Fitting · crackedFOUR EACH FITTINGS, P/N 69-20773-7, LOCATED BETWEEN THE CENTER TWO AFT FLAP TRACKS ARE CRACKED AT THE LOWER FLANGE OF THE FITTINGS. CRACKS RANGE FROM 1 INCH TO 6 INCHES DOWN THE LOWER FLANGE. SUSPECT CAUSE WOULD BE EXCESSIVE BOWING OF THE MID-FLAP.SDR UPS97221862Light · inoperativeEMERGENCY EXIT LIGHT IN COCKPIT IS NOT SECURE AND CAME ON DURING LANDING ROLL OUT. RESECURED, OPS CHECKED GOOD.SDR UPS97221835Shear Web · corrodedINSPECTION TYPE-C, SHEAR WEB STA 1131 RBL 62 WL 208 HAS CORROSION AT NUTPLATE HOLE. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK DONE IAW EO NR 727-53-1851 AND TRAMCO EWO 97-2020.SDR DHL97701001Seal · looseAFTER TAKEOFF, MAIN CARGO DOOR LIGHT ILLUMINATED. REMAINED ON THROUGHOUT FLIGHT, EXTINGUISHED AFTER CVG, PERFORMED EMERGENCY CHECKLIST. FOUND FWD VENT DOOR SEAL LOOSE ON MAIN CARGO DOOR. REINSTALLED SEAL PER MM 52-34-0, LIGHT OPS CHECKS OK.SDR UPS97221834Support Fitting · crackedINSPECTION TYPE-C, NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE IS CRACKED AT LOWER I/B ATTACH BOLT HOLE. REMOVED CRACKED NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE. REPLACED PER SRM 51-30-2, MM 27-61-81, 27-61-0.SDR UPS97221841Skin · crackedINSPECTION TYPE-C, LT WING I/B FOREFLAP L/E SKIN CRACKED FWD OF DEFLECTOR DOOR I/B END. REMOVED AND INSTALLED SERVICEABLE FOREFLAP, WORK DONE IAW MM 27-51-01.SDR UPS97221833Angle · corrodedINSPECTION TYPE-C, CORROSION FOUND ON RT LOWER L-ANGLE RBL 24 BS 178 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED L-ANGLE PER SRM 51-40-4, 53-10-2, 51-10-1, 51-10-6, 51-30-2.SDR UPS97221840Hinge · corrodedINSPECTION TYPE-C, NR 5 K-FLAP CENTER HINGE FITTING HAS SEVERAL SPOTS OF CORROSION. REMOVED AND INSTALLED NEW HINGE ASSY, WORK DONE IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2, 51-20-04, MM 27-87-01.SDR UPS97221839Rib · crackedINSPECTION TYPE-C, NR 3 SLAT 1ST RIB I/B OF ACTUATOR ROD END CRACKED. REPLACED WITH NEW SLAT ASSY, WORK DONE IAW MM 27-81-11.SDR UPS97221838Fitting · corrosionINSPECTION TYPE-C, CORROSION ON FAIRING ATTACH FITTING AT BS 1073 STR 19L. FABRICATED NEW FITTING AND INSTALLED, WORK DONE IAW 53-10-1, 51-10-2, 51-10-1 AND MM 51-20-151.SDR UPS97221818Seat Track · corrodedINSPECTION TYPE-C, BS 480 TO 500 RBL 65 WL 208 THERE IS CORROSION IN THE SEAT TRACK WELL. REPLACED SEAT TRACK PER SRM 53-10-5, 51-30-2.SDR UPS97221817Fitting · corrodedINSPECTION TYPE-C, CARGO NET ATTACHMENT FITTING CORRODED AT BS 364 LBL 39 WL 206. REPLACED WITH NEW PART IAW SRM 51-30-2, 51-10-2, 51-20-151.SDR UPS97221816Fitting · corrodedINSPECTION TYPE-C, CARGO NET ATTACHMENT FITTING CORRODED AT BS 364 RBL 56 WL 206. REPLACED WITH NEW PART IAW SRM 51-30-2, 51-20-1, 51-30-5.SDR UPS97221815Threshold · crackedINSPECTION TYPE-C, AFT CORNER THRESHOLD, AFT FRAME IS CRACKED AT BS 676 WL 215 RBL 67. REPLACED WITH NEW PART IAW SRM 51-30-3, 51-30-2, 51-20-4.
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