Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  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 DL72S992077Indicator · malfunctionedWHEN FLAPS WERE POSITIONED TO FLAPS 2, THE LEFT AND RIGHT OUTBOARD SHOWED SLIGHT ASYMMETRY (ABOUT 1 NEEDLE WIDTH) RAN CHECKLIST AND LOWERED FLAPS WITH ALTERNATE FLAP SWITCHES. FLAPS LOWERED TO 30 ON BOTH OUTBOARD, BUT INBOARD NOW SHOWED A SLIGHT SPLIT(ABOUT 5Sep 16, 1999 · N516DA · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72L992084Skin · damagedUPPER RUDDER DAMAGED TORN 2 INCHES BY 7 INCHES AT L/E RUDDER STA 180 TO 187. DRILLED UP REPAIR PER SRM 55-20-3 FIG 1. INSTALLED REPAIR PER SRM 55-20-3.Sep 16, 1999 · N511DA · Boeing 727232 · Rudder, Plate/SkinSDR DL72L992085Skin · corrodedTHE LOWER SKIN OF THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH A 5 INCH LONG AREA OF CORROSION OVER THE UPPER TWO FASTENER ROWS. THE CORRODED AREA WAS CUT AWAY AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 368232-14, REV A.Sep 15, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L992083Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 660 & 680. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAISep 15, 1999 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L992055Rib · crackedFOUND ON MV2 CK, .375 INCH CRACK ON NR 2 L/E SLAT RIB O/B OF ACTUATOR ATTACH BOLT. REPAIRED PER MM 57-54-0.Sep 15, 1999 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L992054Stiffner · crackedFOUND ON MV2 CK, L/E WING SPAR STIFFENER CRACKED AT THE NUMBER 7 SLAT O/B TRACK O/B SIDE. REPAIRED PER MM 57-20-21.Sep 15, 1999 · N511DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L992053Stiffner · crackedFOUND ON MV2 CK INBD AND OUTBD SPAR STIFFENERS CRACKED AT THE NUMBER 7 SLAT I/B TRACK ON THE FWD WING SPAR. REPAIRED PER MM 57-20-21.Sep 15, 1999 · N511DA · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9901232Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 580, STRINGER 26R-27R. THE CORRODED AREA WAS REMOVED IAW SRM 53-10-4 AND A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND 53-10-4.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901231Frame · corrodedINSPECTION FOUND FRAME AND WEB CORRODED AT STA 1148 FROM STRINGER 27L-27R. THE WEB WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-10-6, 53-10-4, FIGURE 45, AND 51-30-2. THE FRAME WAS REPAIRED IAW SRM 53-10-4, FIGURE 15.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901230Stringer · corrodedINSPECTION FOUND STRINGER 29R CORRODED AT STA 344. THE SKIN WAS CUT AND CORRODED STRINGER WAS REMOVED. A FILLER, DOUBLER, AND STRINGER REPAIR WERE INSTALLED IAW SRM 53-30-3.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9901229Web · corrodedINSPECTION FOUND WEB SKIN CORRODED AT STA 1142-1148, STRINGER 26R TO 20R. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-40-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901228Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 15. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8 AND 51-30-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9901227Shear Tie · corrodedINSPECTION FOUND FRAME SHEAR TIES CORRODED AT STA 720B, STRINGER 28L-28R, STA 720C, S28L-28R, AND STA 720F, S25R-27R. THE SHEAR TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-10-6, 53-10-4, 51-30-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901226Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 1148, STRINGER 24R TO 27R. REPAIRED SHEAR TIE IAW SRM 53-10-4.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901225Angle · corrodedINSPECTION FOUND THREE ANGLES CORRODED IN KEEL BEAM AREA FROM STA 759-824. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-4, 51-30-2, AND 51-10-1.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901224Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL BETWEEN STA 990 AND 1010 AT S24L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-1, 51-40-3, AND 51-30-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901223Angle · corrodedINSPECTION FOUND KEEL BEAM ANGLES AT STA 750, RT SIDE AND STA 850, RBL 5 TO LBL 5 CORRODED. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901222Stringer · corrodedINSPECTION FOUND STRINGER S28R AND S27L CORRODED AT STA 660-680. THE CORRODED SECTION OF STRINGERS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW 51-30-2, 53-10-3, 51-30-1, 51-10-2, AND 51-10-6.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9901221Frame · crackedINSPECTION FOUND A 4 INCH CRACK IN FRAME AT STA 500, STRINGER 21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS INSTALLED IAW SRM 51-40-3.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901220Shear Tie · corrodedINSPECTION FOUND SHEAR TIES CORRODED AT STA 990, S29R AND STA 1090, S29R. NEW SHEAR TIES WERE INSTALLED IAW SRM 53-10-4, 51-30-2, AND 51-10-2.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Internal Mounting StructureSDR CALA9901219Keel Beam · corrodedINSPECTION FOUND KEEL BEAM WEB CORRODED AT STA 801, LT SIDE. THE CORRODED WEB AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-1.Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, KeelSDR DL72L992031Flap Track · corrodedNR 4 FLAP TRACK, REF AD 90-07-05, 90-06-09, 91-09-03, 94-05-04, TYPICAL CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATTACH PAD AND ATTACH HOLES. WEAR FOUND AT TRACK FWD ATTACH LUG FACES AND FWD MLG HINGE FITTING ATTACH HOLES. AUTHORIZED MACHINING TO OVERSIZSep 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992030Flap Track · corrodedNR 5 FLAP TRACK, REF AD 90-07-05 AND AD 90-06-09, TYP CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATTACH PAD SURFACE AND ATTACH BOLT HOLES. TYPICAL WEAR FOUND AT FWD TRACK ATTACH LUG FACES. ALL CORROSION AND WEAR WAS MACHINED. AUTHORIZED REWORKED DIMENSIONSep 13, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L992026Battery · discharged32 OVERHEAD EXIT LIGHT INOP. REPLACED BATTERY OPS NOW OK.Sep 12, 1999 · N513DA · Boeing 727232 · Emergency LightingSDR DL72L992025Battery Pack · dischargedRT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK OPS CK OK.Sep 12, 1999 · N513DA · Boeing 727232 · Emergency LightingSDR DL72S992012Stiffener · cracked2 INCH VISIBLE CRACK IN VERT SPAR STIFFENER I/B SIDE OF O/B TRACK NR 3 L/E SLAT. REPAIRED PER MM 57-20-21 P 813.Sep 10, 1999 · N416DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S992011Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK O/B SIDE OF TRACK. REPAIR PER MM 57-20-21.Sep 10, 1999 · N416DA · Boeing 727232 · Leading Edge DevicesSDR DL72S992010Skin · cracked.5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0.Sep 10, 1999 · N416DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S992009Web · cracked.25 INCH CRACK ON LEFT VERT TORQUE BOX WEB LWR LIGHTING HOLE STA 1290. ROUTE OUT CRACK PER MM 53-11-0.Sep 10, 1999 · N416DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S992008Stringer · crackedFOUND ON F1 LETTER CK, 1 INCH CRACK IN STRINGER 18A AT STA 940 IN THE UPPER AND LOWER RADIUS RT. REPAIRED PER MM 53-12-0.Sep 10, 1999 · N416DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S992007Bleed Valve · malfunctionedAFTER TAKEOFF, (NORMAL POWER) THE ENG 2 APU BLEED HIGH TEMP LIGHT ILLUMINATED. THE NR 2 THROTTLE WAS RETARDED AND THE LIGHT WENT OUT. DISCUSSED WITH ATL/MCC AND FLIGHT RETURNED TO SLC. LIGHT TESTED GOOD. REPLACED NR 2 ENG BLEED VALVE CB, CKS GOOD.Sep 9, 1999 · N517DA · Boeing 727232 · Compressor Bleed ValveSDR CALA9901169Stringer · corrodedINSPECTION FOUND FORWARD CARGO STRINGER 27L CORRODED AT FS 660-640, FS 720C-720B, AND 720B-720A. THE CORRODED AREAS WERE CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-20-0.Sep 9, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S991988Light · damagedR1 DOOR EMERGENCY EXIT LIGHT DAMAGED. REPLACED EMERGENCY LIGHT ASSY.Sep 7, 1999 · N405DA · Boeing 727232 · Emergency LightingSDR DL72S991985Rod · brokeAFTER T/O, DURING GEAR RETRACTION, GOT A LOUD SNAP WITH A VIBRATION AND A RED GEAR DOOR ON FWD PANEL AND NLG DOOR LIGHT ON S/O PNL. REPLACED NOSE GEAR ACT ROD. SWUNG NOSE GEAR GEAR AND DOORS OPERATE NORMAL.Sep 7, 1999 · N531DA · Boeing 727232 · Landing Gear Door Retract SectionSDR DL72K991987Battery · dischargedEMERGENCY CEILING AREA WHITE LIGHT INOP. REPLACED BATTERY.Sep 7, 1999 · N417DA · Boeing 727232 · Emergency LightingSDR DL72S991979Pack Battery · dischargedFOUND MID LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CKS GOOD.Sep 6, 1999 · N485DA · Boeing 727232 · Emergency LightingSDR DL72S991976Battery · dischargedL-2 DOOR OVERHEAD EMERGENCY LT WOULD NOT TEST REPLACED BATTERY PACK.Sep 6, 1999 · N532DA · Boeing 727232 · Emergency LightingSDR DL72L991998Stringer · wornSTRINGER 7L OF THE VERTICAL STABILIZER WAS FOUND TO BE WORN AT FIN STATION 228. THE DAMAGE WAS REPAIRED PER ER/A 333496.Sep 5, 1999 · N501DA · Boeing 727232 · Vertical StabilizerSDR DL72L991997Frame · corrodedTHE CARGO DOOR OPENING FRAME AT FS 1142 WAS FOUND TO HAVE CORROSION ON THE FORWARD SIDE OF THE WEB. THE DAMAGE WAS REPAIRED PER ER/A 333525-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991996Skin · gougedTHE FUSELAGE SKIN WAS GOUGED AT FS 306 AND WL 249 ON THE LHS OF THE AIRCRAFT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333507-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991995Skin · misdrilledTHE FUSELAGE SKIN WAS MISDRILLED AT FS 1096 AND STRINGER 1 DURING THE ACCOMPLISHMENT OF EO 4-60553-3AD. THIS DAMAGE WAS ADDRESSED BY ER/A 333491-14AD AT HMV.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L991993Stringer · gougedTOOLING DAMAGE WAS FOUND ON THE LOWER SURFACE OF STRINGER 17R AT FS 1176. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333504-14K.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L991992Stringer · crackedA CRACK WAS FOUND IN THE STRINGER TO RIB ATTACH FLANGE OF WING STRINGER 17R AT WING STATION 304. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333519-14.Sep 5, 1999 · N501DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72L991991Stringer · corrodedSTRINGER 27R WAS FOUND CORRODED AT FS 1137. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333521-14.Sep 5, 1999 · N501DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L991967Web · crackedFOUND ON MV-2 CK, 1 INCH CRACK STA 1303 WEB WL 270 RBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.Sep 4, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L991966Web · crackedFOUND ON MV-2 CK, 1 INCH CRACK IN STA 1303 WEB WL 270 LBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.Sep 4, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S991960Battery Pack · dischargedRT AFT 2 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M957 AND M956, OPS CHKS GOOD.Sep 3, 1999 · N406DA · Boeing 727232 · Emergency LightingSDR DL72S991955Skin · crackedFUSELAGE SKIN FS 360-481, STRG 4L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONSep 2, 1999 · N520DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S991946Web · crackedFOUND ON C2 LETTER CK, .0625 INCH CRACK IN LT TORQUE BOX WEB LT SIDE STA 1266. REPAIRED PER MM 53-11-0.Sep 1, 1999 · N518DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L992087Frame · corrodedFOUND DURING MV2 CORROSION VISIT NRC 226, CORROSION AT SUPPORT FRAME FOR ACCESS PANEL 3455R AT LWR SURFACE I/B OF FWD HINGE. REPAIRED PER M/M 53-30-1 FIG 804.Sep 1, 1999 · N511DA · Boeing 727232 · Fuselage Miscellaneous Structure
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