Boeing 727-30C

Service difficulty reports · 931

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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.

SDR 96ZZZM456Angle · crackedDURING C-CHECK, FOUND FORWARD ENTRY DOOR CUTOUT AT BOTTOM LATCH ANGLE IS CRACKED AT SEVERAL PLACES. STOP DRILLED CRACK PER SRM 51-10-1. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .050 3 INCAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM455Door Frame · crackedDURING C-CHECK, FOUND MCD FRAME CRACKED AT STATION 540 ABOVE WINDOW FRAME MKD PER SSID D6-48040-1 F-3A. INSTALLED TYPICAL ANGLE REPAIR PER SRM 51-40-3. MATERIAL USED 7075-T6. SIZE OF REPAIR 10 INCH BY 4 INCH .050 THICKNESS.Aug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM454Spar Web · corrosionDURING C-CHECK, FOUND WING CENTER SECTION, AFT LOWER SPAR WEB EXTERIOR HAS CORROSION, STATION 870 LBL 0 TO 14 INCHES (SEVERAL AREAS) BULDGING FROM AROUND FASTENERS. CUT OUT DAMAGE AREA AS PER SRM 51-40-2 25 INCH BY 3 INCH. INSTALLED WEB REPAIR AS PER SRM 51-Aug 8, 1995 · N703DH · Boeing 72730C · Wing SparSDR 96ZZZM453Skin · corrodedDURING C-CHECK, FOUND ON FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 MATERIAL LOSS NOTED BETWEEN 10 PERCENT TO 20 PERCENT BETWEEN STRINGER 14R AND 15R. REMOVED FASTENERS. CUT OUT DAMAGED AREA BETWEEN STRINGER 14 AND 15R 4 INCH BY 11 INCH APPROX PEAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM452Skin · corrosionDURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGERS 20R AND 23R SKIN PANEL HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA 22.5 INCH BY 4.5 INCH APPROXIMATELY PER SB 727-53-0084. FABRICATED FILLER AAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM451Skin · corrodedDURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE BUTT SEAM AT FS 441 BETWEEN STRINGER 24R AND 26R HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 16 INCH PER SB 727-53-0084. REMOVED CORROSAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM450Skin · corrosionDURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGER 17L AND 19L HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4.5 INCH BY 22 INCH PER SB 727-53-0084. REMOVED CAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM449Skin · corrodedDURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGER 22L AND 26L HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 37 INCH PER S/B 727-53-0084. REMOVED COAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM448Skin · corrodedDURING C-CHECK, FOUND FUSELAGE EXTERIOR GREATER THAN 10 PERCENT LOSS MATERIAL NOTED AT FWD SIDE OF FS 259 IN AREA OF LAP SEAM COMMON TO BUTT SEAM AT STRINGER 19R. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 4 INCH PER SB 727-53-0084. FABRICATED FILLAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR 96ZZZM447Spar Web · crackDURING C-CHECK, FOUND VERTICAL STABILIZER FORWARD SPAR WEB HAS CRACK AT EXISTING REP OUTBOARD SIDE OF FWD TERMINAL FITTING LEFT AT TOP OUTBOARD LEFT SIDE CABLE PULLEY CASTING UNDER PNL 9707. TWO CRACKS FOUND UPPER CRACK ROUTED OUT PER SRM 51-10-1, LOWER CRACKAug 8, 1995 · N703DH · Boeing 72730C · Vertical Stabilizer, Spar/RibSDR 96ZZZM446Fitting · crackedDURING C-CHECK, FOUND HORIZONTAL STABILIZER FRONT SPAR RIGHT UPPER OUTBOARD FITTING INDICATES CRACK AT LUG HOLE. REMOVED BUSHING AT RIGHT UPPER OUTBOARD LUG. ACCOMPLISHED HFEC INSPECTION OF LUG HOLE, CRACK NOTED AT 7 O'CLOCK POSITION. REAMED LUG TO .8125 INAug 8, 1995 · N703DH · Boeing 72730C · Horizontal Stabilizer StructureSDR 96ZZZM445Seat Track · corrodedDURING C-CHECK, FOUND CENTER SEAT TRACK CORRODED, GOUGED AND BROKEN OUT FS 380-390. REMOVED SEAT TRACK AS PER SRM 51-30-2. INSTALLED NEW SECTION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2. REINSTALLED FLOOR PANELS PER SRM 51-30-2.Aug 8, 1995 · N703DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZM444Support · corrosionDURING C-CHECK, FOUND FORWARD LAV LIGHT CORROSION ON AFT WALL SUPPORT FS 344 RBL 25 TO 55. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED DOUBLER 5 INCH BY 1 INCH 7075-T6 .080 SHIM 4 INCH BY 1 INCH Aug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM443Floor Support · corrodedDURING C-CHECK, FOUND FORWARD LAV FLOOR SUPPORT CORRODED ON TOP AND BOTTOM FS 314 RBL 13 TO 42. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED FWD LAV FLOOR SUPPORT FS 314 RBL 13 TO 42 WITAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM442Floor Support · corrosionDURING C-CHECK, FOUND FORWARD LAV FLOOR SUPPORT CORRODED FS 330 TO 344 RBL 51. REMOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED ANGLE 2024-T3 .080 FILLER .080 PER SRM 51-40-3. ALODINED AND PRIMED PEAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM441Floor Support · corrodedDURING C-CHECK, FOUND FLOOR PANEL SUPPORT CORRODED STATION 850-870 RBL 64. REPLACEMENT OF SUPPORT ANGLE AT STATION 850 TO 870 RBL 64 AS PER SRM 51-10-1 PAR 4. INSTALLATION AS PER SRM 51-30-2.Aug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM440Skin · dentedDURING C-CHECK, FOUND THE OVERWING LEADING EDGE CUTOUT FOR THE NR 2 SLAT OUTBOARD TRACK DENTED. ROUTED OUT DAMAGED SKIN PER SRM 51-10-1. FABRICATED DOUBLER .063, 2024-T3, 7 INCH BY 4 INCH PER SRM 57-30-4. INSTALLED REPAIR DOUBLER PER SRM 57-30-4. INSTALLEDAug 8, 1995 · N703DH · Boeing 72730C · Wing, Plate/SkinSDR 96ZZZM439Stringer · corrodedDURING C-CHECK, FOUND STRINGER CORRODED SECOND STRINGER BELOW VERTICAL FIN FRONT SPAR FORGING IN STAIRWELL STATION 1210. VERT FIN STRINGER 2 LEFT. REMOVED CORROSION FROM SECOND STRINGER BELOW VERTICAL FIN STATION 1210 PER SRM 51-10-2. MATERIAL LOSS .010, COAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Main, Longeron/StringerSDR 96ZZZM438Airstair Wall · crackedDURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1305 AIR STAIR RIGHT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALL REPAIR PER SRM 51-40-2 2024-T3 .040 8 INCH BY 4 INCH. TREATED AND PRIMAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM437Airstair Wall · crackedDURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1300 AIR STAIR LEFT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .040 5 INCH BY 3 INCH. TREATED AND PRIAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR 96ZZZM436Airstair Wall · crackedDURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1300 AIR STAIR LEFT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .040 5 INCH BY 3 INCH. TREATED AND PRIAug 8, 1995 · N703DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203890Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 13 SPOILER DELAMINATED ON THE UPPER SURFACE LEADING EDGE AT CENTER HINGE FITTING. REPAIRED WITH FIBERGLASS AND RESIN IAW SRM 57-50-6.Jul 17, 1995 · N906UP · Boeing 72730C · SpoilersSDR UPS203889Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF RT MLG FWD TRUNNION BEARING SUPPORT FITTING. INSTALLED NEW TRUNNION SUPPORT FITTING IAW OHM 32-10-13, MM 32-11-51, MM 32-11-01.Jul 17, 1995 · N906UP · Boeing 72730C · Main Landing Gear Attach SectionSDR UPS203888Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF LT MLG FWD TRUNNION BEARING SUPPORT. INSTALLED NEW TRUNNION SUPPORT FITTING IAW MM 32-11-01, MM 32-11-01, MM 32-32-11.Jul 17, 1995 · N906UP · Boeing 72730C · Main Landing Gear Attach SectionSDR UPS203887Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND LINE OF CORROSION BETWEEN FASTENERS STATION 941, RBL 58 TO 59, WL 207 TOP FLANGE OF FRAME FITTING, POSSIBLE CRACK. REPAIRED PER EWO 95-2805 AND UPS EO B727-5310-7200-A.Jul 17, 1995 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203882End Cap · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RIGHT WING O/B FOREFLAP I/B END CAP CRACKED ON UPPER SURFACE. REPLACED IAW SRM 51-30-2, 51-10-2.Jul 17, 1995 · N906UP · Boeing 72730C · Trailing Edge FlapsSDR UPS203881Angle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT BS 296 LBL 14 WL 180. REPLACED IAW SRM 51-10-6, 53-10-1, 51-30-5, 51-10-2, 51-30-2, 51-20-4.Jul 17, 1995 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203880Intercostal · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT BS 1110 TO 1130 RBL 6 WL 152. REPLACED IAW SRM 53-10-2, 51-20-21, 51-10-2, M/M 51-20-00.Jul 17, 1995 · N906UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203874Spar · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LOWER FRONT SPAR CHORD AT STA 740 WL 167 LBL 37. REPLACED IAW SRM 51-30-2.Jul 17, 1995 · N918UP · Boeing 72730C · Wing SparSDR UPS203873Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON SLAT TRACK ON O/B SIDE. REPLACED IAW SRM 57-51-31 AND 51-30-2.Jul 17, 1995 · N918UP · Boeing 72730C · Wing, Rib/BulkheadSDR UPS203872Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 594 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2.Jul 17, 1995 · N918UP · Boeing 72730C · Wing Miscellaneous StructureSDR UPS203871Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 598 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2.Jul 17, 1995 · N918UP · Boeing 72730C · Wing Miscellaneous StructureSDR UPS203870Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 553 ON L/W L/E. REPLACED IAW SRM 51-30-2, M/M 36-00-01.Jul 17, 1995 · N918UP · Boeing 72730C · Wing Miscellaneous StructureSDR UPS203869Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER FLANGE AT BS 484, STR 24 LT WL 157. REPAIRED IAW SRM 53-10-6, 53-10-3, 51-30-2.Jul 17, 1995 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS203868Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 21R AT BS 620. REPLACED IAW SRM 53-10-3.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Main, Longeron/StringerSDR UPS203867Floorbeam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER CHORD AT BS 1050 WL 199 LBL 31 TO RBL 45. REPLACED IAW SRM 51-30-2 AND EO B727-5310-7183-A.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS203866Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 1 SLAT ON LT SIDE NR 5 RIB FROM END. REPLACED IAW OHM 57-51-31, SRM 51-30-2.Jul 14, 1995 · N918UP · Boeing 72730C · Leading Edge DevicesSDR UPS203865Side Load Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM AT STA 740 WL 170 LBL 34 TO RBL 34. REPAIRED IAW 727-53-1628.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203864Angle · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAM ANGLE AT BS 600 RBL 49 TO 59 WL 201. REPAIRED IAW SRM 53-10-1, 51-10-2, M/M 51-20-121, 51-30-2.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203863Floorbeams · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAMS AT BS 580, RBL 49 TO 59, WL 201. REPAIRED IAW B727-5310-7176-A, SRM 53-10-1.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Main, Floor BeamSDR UPS203862Rib · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT O/B TRACK I/B RIB AND FITTING CORRODED. REPLACED IAW SRM 51-10-1, 51-30-2.Jul 14, 1995 · N918UP · Boeing 72730C · Leading Edge DevicesSDR UPS203861Attach Lug · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 K-FLAP CORROSION ON O/B ATTACH LUG. REPLACED IAW M/M 27-81-01.Jul 14, 1995 · N918UP · Boeing 72730C · Leading Edge DevicesSDR UPS203860Attach Lug · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 K-FLAP CORROSION ON I/B ATTACH LUG. REPLACED IAW M/M 27-81-01.Jul 14, 1995 · N918UP · Boeing 72730C · Leading Edge DevicesSDR UPS203859K-Flap · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 K-FLAP CORRODED. REPLACED IAW M/M 27-81-01.Jul 14, 1995 · N918UP · Boeing 72730C · Leading Edge DevicesSDR UPS203858Strap · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BL 0 STABILIZER STRAP BS 1025 TO 1148 AROUND NUTPLATES. REPLACED IAW SRM 51-30-8, 51-30-2, 51-20-4, 51-10-6, 51-10-2, 51-10-1.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203857Crease Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM AT BS 1130 WL 208 RBL 64. REPLACED IAW SRM 53-10-1, 51-30-2, 51-20-4.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203856Frame · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE OF FRAME AT BS 344 STR 22 RT, WL 177. REPAIRED IAW SRM 51-40-3.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Main, FrameSDR UPS203855Strap · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRAP AT BS 519 TO 660, BL 0, WL 201 AROUND NUTPLATE HOLES ON LOWER SIDE. ALSO, AT LBL 2, RBL 2 AT BS 612 TO 628. REPLACED IAW EO B727-5310-7178-A.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203853Angle · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED ON I/B ATTACH ANGLE AT BOTTOM OF TWO HOLES IN RIGHT WING AT WL 208 FS 100.0. REPAIRED IAW SRM 51-30-2.Jul 14, 1995 · N918UP · Boeing 72730C · Fuselage Miscellaneous StructureSDR UPS203852Core · damagedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01.Jul 14, 1995 · N918UP · Boeing 72730C · Spoilers
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