# Service difficulty reports: N24213, cancelled Mar 12, 1998 A list on [N24213, cancelled Mar 12, 1998](https://openairdocs.org/deregistered/N24213-1998-03-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9700734](https://openairdocs.org/sdr/CALA9700734.md): Batt Charger · burned · May 15, 1997 · N24213 · Boeing 737130 · Battery/Charger System > AN ELECTRICAL ODOR WITH A SLIGHT TRACE OF HAZE WAS NOTICED IN THE CABIN WHILE ON DESCENT INTO CLE. THE GASPER FAN AND GALLEY POWER WAS TURNED OFF AND THE ODOR DECREASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BATTERY CHARGER IN E AND E COMP - [SDR CALA9700643](https://openairdocs.org/sdr/CALA9700643.md): Strut · cracked · May 4, 1997 · N24213 · Boeing 737130 · Main Landing Gear Strut/Axle/Truck > A GRINDING SOUND WAS HEARD COMING FROM LANDING GEAR AREA DURING TAXI. MAINTENANCE FOUND THE NR 2 BRAKE ASSEMBLY DAMAGED DUE TO A SHEARED BOLT AND THE LT MLG INNER CYLINDER WAS CRACKED. THE LT MLG INNER CYLINDER WAS REMOVED AND REPLACED. IN ADDITION, THE NR - [SDR CALA9700056](https://openairdocs.org/sdr/CALA9700056.md): Fan · inoperative · Jan 13, 1997 · N24213 · Boeing 737130 · Air Distribution Fan > THE FLIGHT ATTENDANTS REPORTED, A BURNING ODOR IN CABIN WHILE EN ROUTE. THE SMOKE CHECKLIST PROCEDURE WAS ACCOMPLISHED AND THE ODOR DISSIPATED AFTER THE RT PACK WAS SHUTDOWN. THE AIRCRAFT LANDED AT PVD WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE - [SDR CALA9601644](https://openairdocs.org/sdr/CALA9601644.md): Relay Module · burnt · Nov 15, 1996 · N24213 · Boeing 737130 · DC Generating System > SMOKE WITH FUMES WAS OBSERVED COMING FROM ELECTRICAL PANEL BY THE JUMP SEAT ON AIRCRAFT RIGHT ON APPROACH. THE M181 MODULE WAS HOT TO TOUCH, THE MODULE WAS REMOVED AND SMELLED BURNT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLA - [SDR CALA9601261](https://openairdocs.org/sdr/CALA9601261.md): Drive Mechanism · worn bearing · Sep 3, 1996 · N24213 · Boeing 737130 · Trailing Edge Flap Control System > WHEN FLAPS WERE SELECTED TO 30 DEGREES ON APPROACH, THE AIRCRAFT ROLLED LEFT. THE FLAPS WERE SET TO 25 DEGREES AND THE ROLL STOPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT INBOARD AFT FLAP STICKING IN THE UP POSITION WITH FLAPS LOW - [SDR CALA9600856](https://openairdocs.org/sdr/CALA9600856.md): Skin · dented · May 29, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 1016, S29R. THE DENTED AREAS WERE CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 SRM 51-30-2 AND 51-10-2. - [SDR CALA9600855](https://openairdocs.org/sdr/CALA9600855.md): Stringer · corroded · May 29, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER CHANNEL CORRODED AT STA 351.2 TO 360, S20L. THE STRINGER CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND BOEING DRAWING 69-48934. - [SDR CALA9600854](https://openairdocs.org/sdr/CALA9600854.md): Angle · corroded · May 29, 1996 · N24213 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND NOSE WHEEL WELL CEILING SUPPORT I BEAM AND ATTACHING ANGLES CORRODED. THE BEAM AND ANGLES WERE REMOVED. A NEW BEAM AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2 AND 51-10-2. - [SDR CALA9600853](https://openairdocs.org/sdr/CALA9600853.md): Frame · cracked · May 29, 1996 · N24213 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 3 INCH CRACK IN UPPER FLANGE OF C-1 DOORWAY AFT FRAME. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BOEING DRAWING 65C35242. - [SDR CALA9600850](https://openairdocs.org/sdr/CALA9600850.md): Skin · dented · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6. - [SDR CALA9600849](https://openairdocs.org/sdr/CALA9600849.md): Skin · dented · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6. - [SDR CALA9600848](https://openairdocs.org/sdr/CALA9600848.md): Stringer · corroded · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1. - [SDR CALA9600847](https://openairdocs.org/sdr/CALA9600847.md): Stringer · corroded · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1. - [SDR CALA9600846](https://openairdocs.org/sdr/CALA9600846.md): Skin · creased · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND SKIN CREASED FROM BS 228 TO 360, JUST ABOVE STRINGER 19R. THE DAMAGED SKIN WAS CUT OUT, REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 16. - [SDR CALA9600845](https://openairdocs.org/sdr/CALA9600845.md): Floorbeam · corroded · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Floor Beam > INSPECTION FOUND CORROSION ON AFT UPPER FLANGE OF FLOORBEAM AT BS 294.5, RBL 20 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION OF FLOORBEAM AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 FIGURE 1. - [SDR CALA9600844](https://openairdocs.org/sdr/CALA9600844.md): Skin · corroded · May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND SKIN CORRODED AT BS 410, STRINGER 18L. THE CORRODED SKIN WAS CUTOUT. A REPAIR DOUBLER AND FILLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6. - [SDR CALA9600852](https://openairdocs.org/sdr/CALA9600852.md): Skin · dented · May 24, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND NEW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2. - [SDR CAL950924](https://openairdocs.org/sdr/CAL950924.md): Angle · cracked · Oct 11, 1995 · N24213 · Boeing 737130 · Fuselage Miscellaneous Structure > GSO - INSPECTION FOUND A 2.5 INCH CRACK IN RADIUS OF RT LOWER FORWARD SHEAR BEAM ATTACH ANGLE AT STA 664. THE CRACKED ANGLE WAS REMOVED AND SHEAR BEAM MODIFICATION KIT PART NR 5310-02450-10 WAS INSTALLED IAW EA 5310-02450. (X) - [SDR CAL950925](https://openairdocs.org/sdr/CAL950925.md): Floor Beam · cracked · Oct 4, 1995 · N24213 · Boeing 737130 · Fuselage Main, Floor Beam > GSO - INSPECTION FOUND FLOOR BEAM WEB CRACKED AT FIVE EACH LOWER FASTENER HOLES BETWEEN BS 700-BS 717, BBL 0.07. THE COMBINED CRACK LENGTH WAS APPROXIMATELY 5 INCHES. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW WEB AND DOUBLER WERE FABRICATED AND INSTAL - [SDR CAL950857](https://openairdocs.org/sdr/CAL950857.md): Skin · corroded · Sep 11, 1995 · N24213 · Boeing 737130 · Fuselage Main, Plate/Skin > IAH - INSPECTION FOUND A POPPED FASTENER WITH CORROSION IN SKIN AT LAP JOINT FORWARD OF C-1 DOOR THRESHOLD STATION 400. THE CORRODED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 16. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N24213' AND deregistration_id = 'N24213-1998-03-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N24213-1998-03-12/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.