# Service difficulty reports: N16201, cancelled Nov 16, 1998 A list on [N16201, cancelled Nov 16, 1998](https://openairdocs.org/deregistered/N16201-1998-11-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9801218](https://openairdocs.org/sdr/CALA9801218.md): Accessory Unit · inoperative · Jul 8, 1998 · N16201 · Boeing 737130 · Landing Gear Position and Warning > THE GEAR HANDLE STOPPED IN THE OFF POSITION WHEN RAISING THE GEAR AFTER TAKEOFF. THE GEAR TRIGGER WAS PULLED AND THE GEAR CAME UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. TESTS WERE CONDUCTED IAW MM 32-09-200 AND ALL CHECKED GOOD. - [SDR CALA9601797](https://openairdocs.org/sdr/CALA9601797.md): Window Frame · corroded · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD LOWER CORNER OF NR 4 RT CABIN WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REMOVED AND A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA9601796](https://openairdocs.org/sdr/CALA9601796.md): Skin · cracked · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND.5 INCH CRACKS IN LT FUSELAGE SKIN AT BS 188 TO 251, WL 207 TO 234. THE AREA WAS REPAIRED IAW SRM 51-30-2, BAC DRAWING NR 65-18420, AND EA 5310-01188. - [SDR CALA9601791](https://openairdocs.org/sdr/CALA9601791.md): Floorbeam · corroded · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Floor Beam > INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD AT STA 294.5 FROM RBL 20 TO LBL 20. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2. - [SDR CALA9601790](https://openairdocs.org/sdr/CALA9601790.md): Skin · cracked · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. - [SDR CALA9601789](https://openairdocs.org/sdr/CALA9601789.md): Skin · corroded · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND EXTERNAL FUSELAGE SKIN LAP BULGED AND ONE FASTENER SHEARED AT FS 380, STRINGER 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2, 53-30-2 AND 51-30-2. - [SDR CALA9601788](https://openairdocs.org/sdr/CALA9601788.md): Stringer · corroded · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2. - [SDR CALA9601787](https://openairdocs.org/sdr/CALA9601787.md): Skin · corroded · Dec 11, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND NLG WHEEL WELL UPPER SKIN CORRODED AFT OF ACCESS, STA 240. THE SKIN WAS REPAIRED IAW ECRA 5310-03378. - [SDR CALA9601846](https://openairdocs.org/sdr/CALA9601846.md): Bear Strap · corroded · Dec 9, 1996 · N16201 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND E AND E DOOR CUTOUT BEAR STRAP CORRODED AT FORWARD SIDE OF CUTOUT. STRINGER 29 WAS REMOVED AND CORROSION WAS REMOVED FROM SKIN AND BEAR STRAP IAW SRM 51-10-6. A REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. - [SDR CALA9601845](https://openairdocs.org/sdr/CALA9601845.md): Skin · corroded · Dec 9, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND NOSE WHEEL WELL CUTOUT AFT RT CORNER HAD CORRODED SKIN AND STRESSED FASTENERS. LOWER LOBE SKINS WERE CUT AND REMOVED FROM STA 253 TO 312. THE LOWER CHORD AT STA 294.5 WAS REMOVED AND REPLACED IAW BAC DRAWING 65-45808. A SPLICE WAS FABRICATE - [SDR CALA9601786](https://openairdocs.org/sdr/CALA9601786.md): Stringer · cracked · Dec 9, 1996 · N16201 · Boeing 737130 · Wing, Longeron/Stringer > INSPECTION FOUND A 1 INCH CRACK AT STRINGER 7R FASTENER ON RT WING UPPER SURFACE, WBL 200. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 5710-01765. - [SDR CALA9601844](https://openairdocs.org/sdr/CALA9601844.md): Skin · corroded · Dec 7, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE EXTERIOR SKIN LAP CORRODED AT STA 540, STRINGER 26L. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. - [SDR CALA9601772](https://openairdocs.org/sdr/CALA9601772.md): Floorbeam · corroded · Dec 7, 1996 · N16201 · Boeing 737130 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 10 TO RBL 46. THE UPPER T-CAP WAS REMOVED, A NEW UPPER T-CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. - [SDR CALA9601771](https://openairdocs.org/sdr/CALA9601771.md): Intercostal · cracked · Dec 7, 1996 · N16201 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 INCH CRACK IN INTERCOSTAL AT STA 357, STRINGER 16L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. - [SDR CALA9601769](https://openairdocs.org/sdr/CALA9601769.md): Web · corroded · Dec 6, 1996 · N16201 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT LAV LT PAN CORRODED AROUND DUMP CHUTE AND CENTER SUBSTRUCTURE CHANNEL CORRODED AT UPPER SURFACE. THE FLOOR WEB AND CENTER CHANNEL WERE REMOVED, A REPLACEMENT WEB AND CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND 51-10 - [SDR CALA9601770](https://openairdocs.org/sdr/CALA9601770.md): Stiffener · corroded · Dec 4, 1996 · N16201 · Boeing 737130 · Fuselage Miscellaneous Structure > INSPECTION FOUND STA 285.62 NOSE WHEEL WELL RT VERTICAL STIFFENER CORRODED 3 INCHES FROM LOWER END AND 2 INCHES FROM UPPER END. THE VERTICAL STIFFENER WAS REMOVED, A REPLACEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BAC DRAWING 6 - [SDR CALA9601842](https://openairdocs.org/sdr/CALA9601842.md): Skin · corroded · Nov 25, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN RIVETS AT BS 964, STRINGER 20L. THE CORRODED AREA OF SKIN WAS CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. - [SDR CALA9601843](https://openairdocs.org/sdr/CALA9601843.md): Skin · cracked · Nov 16, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. - [SDR CAL960529](https://openairdocs.org/sdr/CAL960529.md): Skin · cracked · Apr 25, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > GSO - REMOVED DAMAGE AREA AND FABRICATED DOUBLER, INSTALLED DOUBLER AT STRINGER 20R - STATION 192 PER SRM 53-30-3. (M) - [SDR CAL960511](https://openairdocs.org/sdr/CAL960511.md): Switch · inoperative · Apr 21, 1996 · N16201 · Boeing 737130 · Landing Gear Position and Warning > FLT NR 234 - EWR - RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED, AFTER GEAR LOWERED DURING APPROACH FOR LANDING. CYCLED GEAR, RED AND GREEN LIGHT FLICKERED ALTERNATELY DURING SECOND APPROACH. FOUND RIGHT DOWNLOCK SENSOR AT FAULT, REPLACED SAME PER MX - [SDR CAL951147](https://openairdocs.org/sdr/CAL951147.md): Skin · corroded · Dec 13, 1995 · N16201 · Boeing 737130 · Fuselage Main, Plate/Skin > GSO - INSPECTION FOUND THE FUSELAGE SKIN AND DOUBLERS CORRODED AT AFT LOWER CORNER OF C-1 DOORWAY. THE CORROSION WAS REMOVED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 5330-02343. (X) - [SDR CAL951145](https://openairdocs.org/sdr/CAL951145.md): Light · inoperative · Dec 13, 1995 · N16201 · Boeing 737130 · Emergency Lighting > GSO - INSPECTION FOUND THE LEFT OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED, RECHARGED, AND INSTALLED. (M) - [SDR CAL951144](https://openairdocs.org/sdr/CAL951144.md): Battery Pack · discharged · Dec 13, 1995 · N16201 · Boeing 737130 · Emergency Lighting > GSO - INSPECTION FOUND THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 23 INOPERATIVE. THE EMERGENCY EXIT LIGHT BATTERY PACK WAS REMOVED AND REPLACED. (M) - [SDR CAL951143](https://openairdocs.org/sdr/CAL951143.md): Light · inoperative · Dec 13, 1995 · N16201 · Boeing 737130 · Emergency Lighting > GSO - INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. (M) - [SDR CAL951142](https://openairdocs.org/sdr/CAL951142.md): Battery Pack · discharged · Dec 13, 1995 · N16201 · Boeing 737130 · Emergency Lighting > GSO - INSPECTION FOUND BOTH RT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (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 = 'N16201' AND deregistration_id = 'N16201-1998-11-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16201-1998-11-16/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.