N77215, cancelled Mar 11, 1998

Service difficulty reports · 22

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 = 'N77215' AND deregistration_id = 'N77215-1998-03-11'
  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 CALA9701432Slide · low pressureL-1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH MM 25-61-311.Oct 11, 1997 · N77215 · Boeing 737130 · Escape SlideSDR CALA9700860Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 360, STRINGER 17L. THE DENTED SECTION OF SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 28 AND ECRA 5330-02523.May 20, 1997 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9601542Hyd Line · leakingTHE A-HYDRAULIC SYSTEM QUANTITY GRADUALLY DECREASED TO 1 GALLON WHILE EN ROUTE. THE A-SYSTEM HYDRAULIC PUMPS WERE TURNED OFF. WHEN THE PUMPS WERE TURNED ON TO LOWER FLAPS THE SYSTEM FAILED AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED AT EWR WITHOUT INCIOct 31, 1996 · N77215 · Boeing 737130 · Hydraulic System, MainSDR CALA9601447Line · leakingLOSS OF A-SYSTEM HYDRAULICS. FOUND PRESSURE LINE FROM NR 2 ENGINE LEAKING. REPLACED LINE AND BOTH ENGINE DRIVEN AND ELECTRIC HYDRAULIC PUMPS AND REPLACED ALL FILTERS PER MM 29-11-32 AND 29-12-21.Oct 12, 1996 · N77215 · Boeing 737130 · Hydraulic System, MainSDR CALA9601325Air Dist Fan · inoperativeA STRONG ELECTRICAL ODOR WAS SMELLED IN THE COCKPIT AFTER TAKEOFF. THE FLIGHT ATTENDANT'S REPORTED SMOKE IN THE AFT/MID CABIN. THE AIR DISTRIBUTION FAN WAS TURNED OFF AND THE SMOKE APPEARED TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO IAD WHERE IT LANDED WITHSep 23, 1996 · N77215 · Boeing 737130 · Air Distribution FanSDR CALA960491Battery · dischargedGSO - THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE RIGHT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (XApr 15, 1996 · N77215 · Boeing 737130 · Emergency LightingSDR CAL960492Battery · dischargedGSO - THE LEFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE LEFT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X)Apr 15, 1996 · N77215 · Boeing 737130 · Emergency LightingSDR CAL960485Chord · crackedGSO - INSPECTION FOUND LT OUTBOARD CHORD CRACKED PAST SECOND FASTENER HOLE AT STA 727. THE CHORD SEGMENT WAS REMOVED AND RPELACED IAW BOEING DRAWING 65C33722. (X)Mar 27, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960484Floor Beam · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FLOOR BEAM LOWER T-CHORD AT BBL ZERO, STA 675. THE FLOOR BEAM CHORD WAS REPAIRED IAW ECRA 5710-01462 AND BOEING DRAWINGS 65C19643, 65C17173, ND 65C17103. (X)Mar 25, 1996 · N77215 · Boeing 737130 · Fuselage Main, Floor BeamSDR CAL960483Skin · delaminatedGSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-6, SRM 51-10-2, AND SRM 51-20-21. (X)Mar 25, 1996 · N77215 · Boeing 737130 · AileronsSDR CAL960487Skin · corrodedGSO - INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 259 TO STA 306, STR 24L TO STR 27L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A NEW SECTION OF SKIN AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (X)Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960486Stringer · corrodedGSO - INSPECTION FOUND STR 21R AND SKIN PANEL CORRODED AT STA 294.5. THE STRINGER AND SKIN PANEL WERE REMOVED. A NEW STRINGER, SKIN SECTION, AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-4. (X)Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Longeron/StringerSDR CAL960489Skin · delaminatedGSO - INSPECTION FOUND UPPER AFT TRAILING EDGE SECTION OF RUDDER DELAMINATING. THE LENGTH OF DELAMINATION WAS APPROXIMATELY 12 INCHES. THE DELAMINATED SECTION OF RUDDER WAS REMOVED. A NEW CORE SECTION AND SKIN PLIES WERE FABRICATED AND BONDED IAW SRM 51-40-Mar 21, 1996 · N77215 · Boeing 737130 · Rudder, Plate/SkinSDR CAL960488Chord · corrodedGSO - INSPECTION FOUND LOWER CHORD CORRODED AT LEFT AND RIGHT ENDS ON UPPER AND LOWER SURFACES OF HORIZONTAL FLANGE, STA 294.5. THE CORRODED CHORD SEGMENT WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW SRM 51-30-2, SRM 51-30-5, AND SRM 51-10-2. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960482Skin · crackedGSO - INSPECTION FOUND A 0.3 INCH CRACK IN RT WING LEADING EDGE SKIN ON OUTBOARD EDGE OF OUTBOARD SLAT TRACK CUT-OUT, WBL 304. THE CRACK WAS ROUTED OUT IAW ECRA 5720-01512. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Wing, Plate/SkinSDR CAL960481Angle · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESSURE PANEL AT BS 663.75. BOTH ANGLES WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-10-2. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960480Skin · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT NR 2 SLAT AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, SR 51-10-2, AND SRM 51-30-2. (X)Mar 4, 1996 · N77215 · Boeing 737130 · Wing, Plate/SkinSDR CAL960490Frame · crackedGSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME. THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED WEB WAS CUT OUT. REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND SRM 51-30-2. (X)Mar 3, 1996 · N77215 · Boeing 737130 · Cargo/Baggage DoorsSDR CAL960152Hyd Line · leakingFLT NR 1446 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE LEAKING AT CLAMP. THE PRESSURE LINE WAS RFeb 14, 1996 · N77215 · Boeing 737130 · Hydraulic System, MainSDR CAL950519T-Angle · corroded31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X)Jun 5, 1995 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL950518Pressure Panel · corroded31J - THE NOSE WHEEL WELL PRESSURE BULKHEAD WAS FOUND WITH A CORROSION BULGE 1 INCH IN DIAMETER, AT THE AFT FORWARD OUTBOARD CORNER OF THE LEFT ACCESS PANEL BETWEEN THE SKIN AND INVERTED 'T'. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03128, REV IR. (M)Jun 1, 1995 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL950241Hydraulic Line · chafedEWR - FLT 1204 - THE B-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE TO EWR. THE A-SYSTEM QUANTITY GAUGE DECREASED TO ONE GALLON. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A B-SYSTEM HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE HYDRMar 30, 1995 · N77215 · Boeing 737130 · Hydraulic System, Main
Back to N77215, cancelled Mar 11, 1998