N467DA, cancelled Sep 5, 2003

Service difficulty reports · 37

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N467DA' AND deregistration_id = 'N467DA-2003-09-05'
  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 DL72S981702Oven · smokingFWD GALLEY OVENS EMITTED BURNING PLASTIC SMELL AND VISABLE SMOKE AFTER TURNING ON. FOUND PLASTIC SHIPPING LABEL ON SIDE OF FOOD CARRIER. REMOVED AND REPLACED CARRIER.Aug 18, 1998 · N467DA · Boeing 727232 · Buffet/GalleysSDR DL72S981268Skin · crackedRIVETS LOOSE .25 INCH CRACK IN DORSAL FIN OUTER SKIN RT SIDE BELOW PANEL 9516. REPAIR PER M/M 54-30-0 FIG 801.Jun 16, 1998 · N467DA · Boeing 727232 · Nacelle/Pylon StructureSDR DL72S981145Switch · dirtyTAILSKID LIGHT ON TAKEOFF ROLL AT 70 KNOTS, CLEANED PROX SWITCH.May 29, 1998 · N467DA · Boeing 727232 · Landing Gear Position and WarningSDR DL72S972341Stiffener · crackedFOUND DURING F-1 LETTER CHECK, 1.25 INCH CRACK NR 4 L/E SLAT I/B TRACK ROLLER BOX I/B STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.Nov 12, 1997 · N467DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972339Web · crackedA .25 INCH CRACK AT UPPER LIGHTENING HOLE ON VERTICAL WEB STA 1235 R IN 48 SECTION. REPAIRED PER M/M 53-11-0.Nov 12, 1997 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972204Battery Pack · dischargedMSU - CK OP OF ALL EMER LIGHTS. FOUND LT OVERWING EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS NML.Oct 29, 1997 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S971349Frame · double drilledDURING THE PERFORMANCE OF SI 4-61904-12, THE SECOND FASTENER HOLE ABOVE THE FLOORBEAM ON THE INBOARD FLANGE WAS DISCOVERED TO HAVE BEEN LOCATED CLOSE ENOUGH TO A PILOT HOLE TO CREATE A DOUBLE DRILLED HOLE. THE DOUBLER DRILLED HOLE WAS OVERSIZED TO 0.403 THROUJun 25, 1997 · N467DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S970904Sockets · missing2 TRACK LIGHT SOCKETS RIPPED LOOSE FROM FLOOR TRACK, AT ROWS 16 AND 20. REPLACED SOCKETS AND CAPSULES, CKS NORMAL.May 12, 1997 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S970571Track Lights · looseEMERGENCY TRACK LIGHTING AFT CABIN LOOSE FROM FLOOR. REPLACED LIGHT SEGMENT, CKS OK.Mar 27, 1997 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S962149Web · crackedFOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK LWR TORQUE BOX VERTICAL WEB BS 1273 LEFT SIDE AT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.Sep 20, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961783Power Supply · inoperativeON LAYOVER, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPS NORMAL.Jul 25, 1996 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S961782Battery Pack · dischargedON LAYOVER, FOUND CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED BATTERY PACK. OPS NORMAL.Jul 25, 1996 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S960721Circuit Breaker · crackedON FINAL, ALL 3 BUS TIE BREAKERS TRIPPED, PHASE UNBALANCE, OVER EXCITED NR 2 AND NR 3, NR 1 TR UNIT C/B POPPED. FOUND APU GEN BREAKER CRACKED WITH LOOSE CONNECTIONS. REPLACED SAME. ALSO, REPLACED NR 1 ENG GEN BREAKER. RAN ENGS PARALLELED, ALL CHECKS NORMALMar 31, 1996 · N467DA · Boeing 727232 · AC Power Distribution SystemSDR DL72S960467Skin · crackedDURING INSPECTION, THREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. ALL CRACKS GO THROUGH THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. CRACK LENGTH VARIED FROM 1 TO 2 INCH LENGTH. IN ACCORDANCE WFeb 28, 1996 · N467DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960466Bear Strap · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL SKIN DOUBLER OF THE R-2 DOOR CUTOUT AT STATION 1070. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 2-8-96, THE DAMAGE WAS CUT OUT AND A DOUBLER AND TRIPLER INSTALLED.Feb 28, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960453Skin · wornLOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232 · AileronsSDR DL72S960452Spar · crackedSPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.Feb 28, 1996 · N467DA · Boeing 727232 · AileronsSDR DL72S961606Transverse Beam · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. REPAIRED PER ERA 303225-14AD.Feb 27, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960274Door Actuator · iced upON DEPARTURE, RT MAIN GEAR WOULD NOT RETRACT, TRANSIT LIGHT ON AND SECOND OFFICER'S PANEL NEVER ILLUMINATED. REMOVED ICE BUILD-UP ON RT GEAR DOOR ACTUATOR, LUBED GEAR AND DOORS, PERFORMED GEAR SWING AND OPS NORMAL.Feb 4, 1996 · N467DA · Boeing 727232 · Landing Gear Door ActuatorSDR DL72S953846Eel · inoperativeAFT AIRSTAIR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED LIGHT ASSEMBLY AND BATTERY PACK OPERATION NORMAL.Sep 23, 1995 · N467DA · Boeing 727232 · Emergency LightingSDR DL72S953140Web · crackedLT VERTICAL WEB OF NWW HAS 2.0 CRACK BETWEEN STA 294.5 AND STA 285.5, APPROX WL 170. REPAIRED PER DL ERA 302166-14AD.Jul 21, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951112Plate Web · crackedDURING INSPECTION AT CV-2, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 270. IN ACCORDANCE WITH BAC S/B 727-53-145, THE DAMAGED PORTION OF THE WEB WAS TRIMMED OUT, AND A DOUBLER AND 4 REPAIR STRAPS WERE INSTALLED.Mar 3, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950822Skin · corrodedDURING CV-2 CK, FOUND FUSELAGE SKIN DAMAGED BETWEEN STA 720E AND 720F AT STR 27L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3.Feb 15, 1995 · N467DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950815Beam · crackedDURING INSPECTION, THE FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED IN THE ANGLE. THE BEAM WILL BE REPLACED IN ACCORDANCE WITH B727 S 53-0129 REV 4.Feb 9, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950816Stringer · corrodedDURING CV-2 CK, FOUND CORROSION AT STR 23R JUST FWD OF STA 520. REPAIRED PER SRM 53-10-3 ID PER PS 900-5-1 NR 4.Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950761Web · crackedDURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950773Floor Support · crackedFOUND ON LTR CK - 1 INCH CRACK THROUGH MOUNT BOLT HOLE FLOOR PANEL SUPPORT CHANNEL FWD SIDE STA 950C BL 18R - REPAIR - REPAIRED PER SRM 53-10-5 AND I.D. PER P.S. 900-5-1 NR 4.Feb 7, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950821Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER.Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950819Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813.Feb 6, 1995 · N467DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950818Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813.Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S950793Stringer · corrodedFOUND ON CV2 CK - CORROSION INSIDE STRINGER 27L FWD STA 720F - REPAIR - REPLACED SECTION OF STRINGER PER SRM 53-10-3 FIG 1.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S950789Clip · corrodedFOUND ON CV2 CK - CORROSION AT LOWER FWD FUSELAGE SKIN CLIP STA 303 AT NOSE W/W CHORD - REPAIR - REPAIRED PER SRM 51-40-3 FIG 1.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950788Floor Beam · corrodedFOUND ON CV2 CK - CORROSION AT FLOOR BEAM AT BL 0 TO LBL 16 STA 1110 - REPAIR - INSTALLED REPAIR ANGLE PER MM 53-20-11 FIG 804A.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950787Floor Beam · corrodedFOUND ON CV2 CK - CORROSION AT FLOOR BEAM TOP SIDE AND BOTTOM WHERE CLIP NUTS ATTACH STATION 380 RBL 12 TO 63 - REPAIR - REPLACED TEE CAP PER SRM 53-10-8.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950786Seat Track · corrodedFOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 344 TO 360 AT LBL 22 - REPAIR - REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950785Seat Track · corrodedFOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 480 LBL 22 - REPAIR - REPLACED DAMAGED SEAT TRACK FROM 440-480 PER SRM 53-10-5 FIG 7.Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950817Rib · crackedDURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9.Feb 2, 1995 · N467DA · Boeing 727232 · Leading Edge Devices
Back to N467DA, cancelled Sep 5, 2003