# Service difficulty reports: N17252, cancelled Oct 14, 1998 A list on [N17252, cancelled Oct 14, 1998](https://openairdocs.org/deregistered/N17252-1998-10-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9801327](https://openairdocs.org/sdr/CALA9801327.md): Torsion Link · sheared · Jul 23, 1998 · N17252 · Boeing 737291 · Main Landing Gear Strut/Axle/Truck > THE LT MLG LOWER TORSION LINK SHEARED AFTER LANDING IN EWR. THE LT MLG LOWER TORSION LINK WAS REMOVED AND REPLACED. IN ADDITION, THE SHIMMY DAMPER AND BOTH INBOARD AND OUTBOARD GUIDE BRACKETS WERE REPLACED. A GEAR SWING WAS PERFORMED AND OPERATION CHECKED G - [SDR CALA9800918](https://openairdocs.org/sdr/CALA9800918.md): Axle · failed · May 29, 1998 · N17252 · Boeing 737291 · Main Landing Gear Strut/Axle/Truck > THE NR 4 MAIN WHEEL SEPARATED FROM AIRCRAFT DURING TAXI IN. MAINTENANCE FOUND THE AXLE SHEARED OFF, NO OTHER AIRCRAFT DAMAGE WAS FOUND. THE RT MLG INNER CYLINDER WAS REMOVED AND REPLACED IAW MM 32-11-21 AND 12-15-31. *S/D* INVESTIGATION BY ENGINEERING CONC - [SDR CALA9700917](https://openairdocs.org/sdr/CALA9700917.md): Skin · cracked · Jun 14, 1997 · N17252 · Boeing 737291 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 8.25 INCH CRACK ON THE LT NOSE WHEEL WELL SIDEWALL AND A 3 INCH CRACK ON THE RT NOSE WHEEL WELL SIDEWALL AT STA 259.5, WL 180. REPAIRS WERE INSTALLED IAW ECRA 5310-03512. - [SDR CALA9700609](https://openairdocs.org/sdr/CALA9700609.md): Fuel Pump · shaft sheared · Apr 24, 1997 · N17252 · Boeing 737291 · Engine Fuel Pump > AFTER ROTATION NR 2 ENGINE FAILURE RETURNED TO CLE. NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED PER MM 73-11-01/72-60, PERFORMED POWER ASSURANCE RUN MM 71-09-266 PARTS CHG COMPLETE. - [SDR CALA9700232](https://openairdocs.org/sdr/CALA9700232.md): Hyd Line · leaking · Feb 21, 1997 · N17252 · Boeing 737291 · Hydraulic System, Main > THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE. THE GEAR AND FLAPS WERE EXTENDED MANUALLY AND THE AIRCRAFT LANDED AT CLE. MAINTENANCE FOUND A HOLE IN PRESSURE HYDRAULIC LINE FROM NR 1 ENGINE PUMP. THE HYDRAULIC LINE AND THE NR 1 ENGINE PUMP WERE RE - [SDR CALA9600974](https://openairdocs.org/sdr/CALA9600974.md): Logic Cards · inoperative · Jul 8, 1996 · N17252 · Boeing 737291 · Landing Gear Position and Warning > THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A NOSE GEAR SWING WAS PERFORMED IAW MM 32-61-00, PAGE 501 TO 504 AND ALL GEAR OPERATION AND INDICATI - [SDR CALA9600986](https://openairdocs.org/sdr/CALA9600986.md): Floor Beam Web · cracked · Jul 2, 1996 · N17252 · Boeing 737291 · Fuselage Main, Floor Beam > INSPECTION FOUND A CRACK IN FLOOR BEAM WEB AT STA 294.5, RBL 47. THE CRACKED SECTION WAS REMOVED AND A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. - [SDR CALA9600985](https://openairdocs.org/sdr/CALA9600985.md): Battery · discharged · Jul 2, 1996 · N17252 · Boeing 737291 · Emergency Lighting > INSPECTION FOUND LOW VOLTAGE AT THE FORWARD ENTRY DOOR SLIDE LIGHT. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION OF THE LIGHT CHECKED GOOD. - [SDR CALA9600984](https://openairdocs.org/sdr/CALA9600984.md): Battery · discharged · Jul 2, 1996 · N17252 · Boeing 737291 · Emergency Lighting > THE SLIDE LIGHT VOLTAGE AT AFT ENTRY DOOR WAS FOUND LOW AND THE BULB WAS BURNED OUT. THE BATTERY PACK AND BULB WERE REMOVED AND REPLACED. - [SDR CALA9600983](https://openairdocs.org/sdr/CALA9600983.md): Battery · inoperative · Jul 2, 1996 · N17252 · Boeing 737291 · Emergency Lighting > INSPECTION FOUND EMERGENCY LIGHT OVER R-2 DOOR INOPERATIVE. THE BATTERY WAS REMOVED, RECHARGED AND REINSTALLED IAW MM 33-50-42. OPERATION OF THE LIGHT CHECKED GOOD. - [SDR CALA9600982](https://openairdocs.org/sdr/CALA9600982.md): Battery · inoperative · Jul 2, 1996 · N17252 · Boeing 737291 · Emergency Lighting > INSPECTION FOUND EMERGENCY LIGHT OVER L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION OF THE LIGHT WAS RESTORED. - [SDR CALA9600981](https://openairdocs.org/sdr/CALA9600981.md): Stringer · cracked · Jun 21, 1996 · N17252 · Boeing 737291 · Wing, Longeron/Stringer > INSPECTION FOUND A CRACK IN LT WING STRINGER 13 AT RIB MOUNTING POINT, FIRST RIB OUTBOARD OF WING ROOT, WBL 92.5. THE CRACK WAS STOP DRILLED IAW BOEING DRAWING NR 65C34533. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C34533. THE S - [SDR CALA9600980](https://openairdocs.org/sdr/CALA9600980.md): Frame · cracked · Jun 19, 1996 · N17252 · Boeing 737291 · Fuselage Main, Frame > INSPECTION FOUND FORWARD CARGO PIT FRAME CRACKED AT STA 460 BETWEEN STRINGER 20L AND 21L. THE CRACKED SECTION OF FRAME WAS REMOVED IAW SRM 51-30-2 AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113. - [SDR CALA9600978](https://openairdocs.org/sdr/CALA9600978.md): Skin · creased · Jun 19, 1996 · N17252 · Boeing 737291 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 992 BETWEEN STRINGER 27L AND 27R. THE DAMAGED SECTION OF SKIN WAS REMOVED, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6, 51-10-2 AND 51-30-2. - [SDR CALA9600977](https://openairdocs.org/sdr/CALA9600977.md): Stringer · damaged · Jun 17, 1996 · N17252 · Boeing 737291 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND FUSELAGE SKIN DENTED AND STRINGER DAMAGED AT STA 400, STRINGER 18L. THE DAMAGED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. THE SKIN WAS RETURNED TO ORIGINAL CONTOUR IAW SRM 51-70, FIGURE 4. REPAIR PARTS FOR STRINGER WERE FABRICATED AND I - [SDR CALA9600975](https://openairdocs.org/sdr/CALA9600975.md): Skin · dented · Jun 14, 1996 · N17252 · Boeing 737291 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500 TO 510 BETWEEN STRINGER 3L AND 4L. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. - [SDR CALA9600979](https://openairdocs.org/sdr/CALA9600979.md): Skin · cracked · Jun 12, 1996 · N17252 · Boeing 737291 · Fuselage Main, Plate/Skin > INSPECTION FOUND A CRACK IN SKIN AT FORWARD GALLEY DOOR FORWARD LOWER CUTOUT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, FILLER, DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. - [SDR CALA9600976](https://openairdocs.org/sdr/CALA9600976.md): Skin · corroded · Jun 12, 1996 · N17252 · Boeing 737291 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND FASTENERS BELOW AFT CARGO DOOR. THE CORRODED AREA WAS CUT OUT, A SKIN SECTION, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-6 AND 51-10-2. - [SDR CAL960069](https://openairdocs.org/sdr/CAL960069.md): Light · wire broken · Jan 30, 1996 · N17252 · Boeing 737291 · Emergency Lighting > FLT NR 1630 - EWR - THE AFT CABIN RIGHT EMERGENCY EXIT LIGHT NEAR BACK WALL ON FLOOR WOULD NOT ILLUMINATE. MAINTENANCE FOUND A WIRE TO THE EXIT LIGHT BROKEN. THE WIRE WAS REPAIRED AND THE LIGHT WAS RELAMPED. (M) - [SDR CAL960006](https://openairdocs.org/sdr/CAL960006.md): Hyd Pump · leaking · Jan 7, 1996 · N17252 · Boeing 737291 · Hydraulic Pump (Electric/Engine), Main > IAH - FLT 1607 - THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 ENGINE DRIVE - [SDR CAL951051](https://openairdocs.org/sdr/CAL951051.md): Battery · discharged · Nov 18, 1995 · N17252 · Boeing 737291 · Emergency Lighting > FLT NR 1205 - EWR - INSPECTION FOUND THE AFT GALLEY R-2 DOOR SLIDE PACK DOOR LIGHT INOPERATIVE. THE BATTERY FOR THE LIGHT WAS REPLACED AND OPERATION CHECKED GOOD. (M) - [SDR CAL950807](https://openairdocs.org/sdr/CAL950807.md): Hyd Line · leaking · Sep 11, 1995 · N17252 · Boeing 737291 · Hydraulic System, Main > GSO - FLT 1867 - THE AIRCRAFT WAS RETURNED TO GSO AFTER LOSING THE A-HYDRAULIC SYSTEM IN-FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO OUTBOARD SPOILER PANEL IN LT WING OUTBOARD OF GEAR LEAKING. THE FLEX LINE WAS REPLACED. IN - [SDR CAL950782](https://openairdocs.org/sdr/CAL950782.md): Hyd Pump · leaking · Sep 2, 1995 · N17252 · Boeing 737291 · Hydraulic Pump (Electric/Engine), Main > GSO - FLT 1495 - THE A-HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLAC - [SDR CAL950115](https://openairdocs.org/sdr/CAL950115.md): Hyd Module · leaking · Feb 10, 1995 · N17252 · Boeing 737291 · Hydraulic System, Main > CLE - FLT 1255 - THE 'A' HYDRAULIC SYSTEM WAS LOST AFTER DEPARTING LGA. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND PLUG BROKEN ON 'A' SYSTEM HYDRAULIC MODULE. THE 'A' SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED AND LEAK CHECKS WERE ## 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 = 'N17252' AND deregistration_id = 'N17252-1998-10-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N17252-1998-10-14/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.