# Service difficulty reports: N10242, cancelled Jun 23, 1998

A list on [N10242, cancelled Jun 23, 1998](https://openairdocs.org/deregistered/N10242-1998-06-23.md).

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

- [SDR CALA9800727](https://openairdocs.org/sdr/CALA9800727.md): Wheel · missing · May 2, 1998 · N10242 · Boeing 7372C0 · Wheel/Ski/Float
  > THE NUMBER THREE TIRE ASSY DEPARTED THE AIRCRAFT ON LANDING. INSPECTED AXLE, NO DAMAGE. INSTALLED NR 3 TIRE AND WHEEL ASSY WITH NEW SPRING RETAINER AND AXLE NUT PER MM 32-45-11.
- [SDR CALA9701710](https://openairdocs.org/sdr/CALA9701710.md): Fitting · leaking · Dec 6, 1997 · N10242 · Boeing 7372C0 · Turbine Engine Oil System
  > THE NR 2 ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DROP WHILE EN ROUTE. THE NR 2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM BANJO FITTING AT ENGINE OIL FILTER HOUSING. A NEW FITTING AND PACKING WERE INST
- [SDR CALA9701219](https://openairdocs.org/sdr/CALA9701219.md): Bulkhead · cracked · Jun 7, 1997 · N10242 · Boeing 7372C0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND AN 8 INCH CRACK IN FORWARD PRESSURE BULKHEAD OF NOSE WHEEL WELL ON LT SIDE APPROXIMATELY THREE INCHES OUTBOARD OF DOOR STOP. DOUBLERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C17111.
- [SDR CALA9700583](https://openairdocs.org/sdr/CALA9700583.md): Hydraulic Line · chafed · Apr 20, 1997 · N10242 · Boeing 7372C0 · Hydraulic System, Main
  > I/B CREW REPORTED LOSS OF A-SYSTEM HYD. FLUID CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.
- [SDR CALA9700070](https://openairdocs.org/sdr/CALA9700070.md): Battery · inoperative · Jan 20, 1997 · N10242 · Boeing 7372C0 · Emergency Lighting
  > INSPECTION FOUND THE LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT LANYARD PULLED OUT FROM ITS SEAT AND THE LIGHT WAS NOT ON. THE BATTERY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9601712](https://openairdocs.org/sdr/CALA9601712.md): Fuel Control · inoperative · Nov 25, 1996 · N10242 · Boeing 7372C0 · APU Engine Fuel and Control
  > THE NR 1 GENERATOR FAILED WHILE EN ROUTE. THE APU WAS STARTED AND THE FIRE WARNING BELL SOUNDED WITH THE RED APU FIRE HANDLE ILLUMINATED. THE APU START SWITCH WAS PLACED TO OFF AND THE FIRE WARNING SYSTEM TESTED GOOD. THE AIRCRAFT WAS DIVERTED TO CMH WHERE
- [SDR CALA9601218](https://openairdocs.org/sdr/CALA9601218.md): Fire Det · shorted · Aug 24, 1996 · N10242 · Boeing 7372C0 · Fire Detection
  > THE APU FIRE WARNING LIGHT AND BELL ACTIVATED ON SHORT FINAL INTO IND WITH APU START. THE APU SWITCH WAS MOVED TO OFF, BUT THE WARNING CONTINUED. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE FIRE LIGHT STAYED ON AND THE BELL WAS INTERMITTENT. THE AIRCRAFT LA
- [SDR CAL960504](https://openairdocs.org/sdr/CAL960504.md): Battery Pack · discharged · Apr 19, 1996 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - R1 DOOR SLIDE LIGHT BATTERY CHECK BAD - LOW VOLTAGE. REPLACED R1 DOOR SLIDE LIGHT BATTERY PACK, OPS CHECK GOOD IAW B737 MX MAN 33-51-63. (X)
- [SDR CAL960503](https://openairdocs.org/sdr/CAL960503.md): Light · inoperative · Apr 19, 1996 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - L1 DOOR SLIDE LIGHT BATTERY CHECKS BAD - ZERO VOLTS. REMOVED AND REPLACED L1 DOOR EVAC SLIDE LIGHT BATTERY PACK ASSY, OPS CHECK GOOD IAW B737 MM 33-51-63. (X)
- [SDR CAL960502](https://openairdocs.org/sdr/CAL960502.md): Light · inoperative · Apr 19, 1996 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - 42 DOOR SLIDE LIGHT BATTERY CHECKS BAD - ZERO VOLTS. REPLACED R2 DOOR SLIDE BATTERY PACK. OPS CHECK GOOD IAW B737MM 33-52-63. (X)
- [SDR CAL960507](https://openairdocs.org/sdr/CAL960507.md): Floor Beam · corroded · Apr 10, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > GSO - FLOOR BEAM AT STA 986 AT RBL 65 AND LAV SUPPORT CHANNEL CORRODED. REMOVED FLOOR BEAM CAP. FABRICATED NEW CAP AND INSTALLED PER B737 SRM 51-10-2, SRM 51-30-2, AND BOEING DWG 65-61381. REMOVED PARTITION SUPPORT AND REPLACED WITH NEW PART PER B737 SRM 51
- [SDR CAL960526](https://openairdocs.org/sdr/CAL960526.md): Skin · cracked · Apr 9, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - R1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. CRACK APPROXIMATELY 1.5 INCH LONG. CUT OUT 1.5 INCH CRACK, FABRICATED REPAIR PARTS IAW B737 SRM 53-30-3 FIG 26. ALODINED AND PRIMED PER SRM 51-10-2. SEALED AND INSTALLED REPAIR IAW SRM 53-30-3 FIG 26. SCUFF
- [SDR CAL960523](https://openairdocs.org/sdr/CAL960523.md): Skin · corroded · Apr 6, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - RIGHT OUTBOARD AFT CORNER OF NOSE WHEEL WELL UPPER PRESS. PANEL HAS SEVERE BULGING AROUND FASTENERS. REMOVED CORROSION, INSTALLED DOUBLER PER CAL EA 5310-02452 OP 1. ALODINED AND PRIMED BARE METAL. (M)
- [SDR CAL960509](https://openairdocs.org/sdr/CAL960509.md): Floor Web · cracked · Apr 6, 1996 · N10242 · Boeing 7372C0 · Fuselage Floor Panel
  > GSO - COCKPIT FLOOR HAS BULGING IN 2 PLACES AND CRACKED FLOOR WEB AT STA 259.5. CRACK LENGTH =.1250 INCH. CUT OUT AND REPLACED FLOOR SECTION AT BS 259.5. CORD SECTION CUT AND SPLICED, FLOOR SUPPORT REPAIRED, FLOOR BEAM WEB CUT AND SPLICED IAW B737, SRM 53-
- [SDR CAL960505](https://openairdocs.org/sdr/CAL960505.md): Bulkhead Skin · corroded · Apr 3, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Bulkhead
  > GSO - CORROSION FOUND AT BS 540 BETWEEN 27L AND 26L. REMOVED DAMAGE FROM WEB. FABRICATED FILLER, DOUBLER AND SHIMS. ALODINED AND PRIMED FILLER DOUBLER AND SHIMS. INSTALLED FILLER, DOUBLER AND SHIMS IAW SRM 51-10-02 AND EC/RA 5710-01723. (X)
- [SDR CAL960527](https://openairdocs.org/sdr/CAL960527.md): Stiffener · cracked · Apr 2, 1996 · N10242 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - FOUND BS 540 STIFFENER RBL 26 CRACKED. APPROXIMATELY 1 INCH IN LENGTH. REMOVED CRACKED SUPPORT BEAM. FABRICATED NEW SUPPORT BEAM AND TAPERED SHIMS. INSTALLED SUPPORT BEAM AND SHIMS IAW B737 SRM 51-30-2. ALODINED AND PRIMED SUPPORT AND SHIMS IAW SRM
- [SDR CAL960524](https://openairdocs.org/sdr/CAL960524.md): Skin · disbonded · Apr 2, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - DISBOND FOUND BETWEEN WINDOWS AT STATION 727 LEFT, 6 INCHES DISBOND AREA. DRILLED LOCATION FOR FIELD RIVETS AND OVERSIZED FASTENERS AND INSTALLED PER SA 004-5310-01827, SA 007-5310-01827, AND CAL CARD JA5310-0182702001. (M)
- [SDR CAL960521](https://openairdocs.org/sdr/CAL960521.md): Skin · disbonded · Apr 2, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - DISBOND FOUND AT 6TH WINDOW FORWARD OF STATION 980 LEFT 8 INCH AREA. ADDED FIELD FASTENERS AT DISBOND AND OVERSIZE EXISTING FASTENERS AND INSTALLED PER SA004-5310-01827, SA007-5310-01827 AND JA5310-0182702001. (M)
- [SDR CAL960510](https://openairdocs.org/sdr/CAL960510.md): Frame · corroded · Apr 2, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - FRAME STA 520 CORRODED BETWEEN STR 28L AND STR 28R ON UPPER LEG. CUT OUT DAMAGED AREA 12 INCHES LONG BY 3 INCHES DEEP. FABRICATED L-ANGLE REPAIR AND FILLER PER B737, SRM 51-40-3 AND SRM 51-40-4. INSTALLED REPAIR IAW B737, SRM 51-40-3 AND SRM 51-40-4.
- [SDR CAL960506](https://openairdocs.org/sdr/CAL960506.md): Bulkhead Skin · corroded · Apr 2, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Bulkhead
  > GSO - CORROSION FOUND AT BS 540 BETWEEN 27R AND 26R. REMOVED CORRODED AREA AROUND PNEUMATIC DUCT. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED AS REQUIRED. INSTALLED FILLER AND DOUBLER IAW B737 SRM 51-10-2, SRM 51-30-2, AND EC/RA 5710-01723. (X)
- [SDR CAL960508](https://openairdocs.org/sdr/CAL960508.md): Floor Beam · cracked · Apr 1, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > GSO - AFT PIT FLOOR BEAM CRACKED, STA 727B, STR 27R AND STR 27L. CRACK APPROXIMATELY.5 INCH IN EXTRUSION. FABRICATED REPAIR PARTS IAW B737 SRM 53-10-5. TREATED AND PRIMED IAW B737 SRM 51-10-2. INSTALLED PARTS. (X)
- [SDR CAL960525](https://openairdocs.org/sdr/CAL960525.md): Skin · corroded · Mar 22, 1996 · N10242 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - RIGHT FORWARD FUSELAGE OUTER SKIN BULGED AND RIVETS PULLING THROUGH JUST FORWARD OF BS 253.5 AT STRINGER 526R. REMOVED DAMAGED SECTION OF SKIN, REMOVED RIGHT CHORD ANGLE. FABRICATED REPAIR DOUBLERS AND FILLERS. INSTALLED NEW RIGHT CHORD ANGLE AND SKIN
- [SDR CAL960047](https://openairdocs.org/sdr/CAL960047.md): Control Panel · inoperative · Jan 20, 1996 · N10242 · Boeing 7372C0 · Cabin Pressure Control System
  > BDL - FLT 1064 - THE CABIN PRESSURE BEGAN TO FLUCTUATE AT FL 270 WHILE EN ROUTE FROM CLE TO BDL, AND SHORTLY AFTER, BEGAN TO CLIMB RAPIDLY. PRESSURE CONTROL WAS SWITCHED TO STANDBY, BUT CABIN PRESSURE COULD NOT BE MAINTAINED. A DESCENT WAS STARTED, THE OXYGE
- [SDR CAL951120](https://openairdocs.org/sdr/CAL951120.md): Mount Bolt · backed out · Dec 9, 1995 · N10242 · Boeing 7372C0 · Landing Gear Door Retract Section
  > FLT NR 1727 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND GEAR DOOR FORWARD TOP MOUNT BOLT ON LEFT GEAR BACKED OUT OF HOLE. THE BOLT, NUT, AND WASHER
- [SDR CAL950916](https://openairdocs.org/sdr/CAL950916.md): Actuator · leaking · Oct 14, 1995 · N10242 · Boeing 7372C0 · Drag Control Actuator
  > EWR - FLT 0244 - THE A-HYDRAULIC SYSTEM WAS LOST AFTER LANDING AT EWR. THE PUMPS WERE FEATHERED WITHIN ONE MINUTE OF LOW PRESSURE LIGHT ILLUMINATION. MAINTENANCE FOUND THE NR 1 GROUND SPOILER ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27
- [SDR CAL950892](https://openairdocs.org/sdr/CAL950892.md): Eel · inoperative · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - THE FORWARD BULLNOSE PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-31. (X)
- [SDR CAL950891](https://openairdocs.org/sdr/CAL950891.md): Eel · inoperative · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - THE R-2 DOOR PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EXIT LIGHT BATTERIES WERE RECHARGED IAW MM 33-51-101. (X)
- [SDR CAL950890](https://openairdocs.org/sdr/CAL950890.md): Eel · inoperative · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - THE AFT BULLNOSE PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-31. (X)
- [SDR CAL950889](https://openairdocs.org/sdr/CAL950889.md): Eel · inoperative · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - THE LT E AND E HATCH PORTABLE EXIT LIGHT WAS FOUND DIM. THE E AND E HATCH PORTABLE EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-01. (X)
- [SDR CAL950888](https://openairdocs.org/sdr/CAL950888.md): Eel Exit Sign · inoperative · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - INSPECTION FOUND THE R-1 DOOR EMERGENCY EXIT LIGHT DIM. THE EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-101. (M)
- [SDR CAL950887](https://openairdocs.org/sdr/CAL950887.md): Eel Battery · discharged · Oct 3, 1995 · N10242 · Boeing 7372C0 · Emergency Lighting
  > GSO - INSPECTION FOUND THE R-2 DOOR SLIDE LIGHT VOLTAGE READING ZERO. THE R-2 DOOR ESCAPE SLIDE LIGHT ASSY AND BATTERY WERE REMOVED AND REPLACED IAW MM 33-51-63. (X)
- [SDR CAL950893](https://openairdocs.org/sdr/CAL950893.md): Frame · corroded · Sep 30, 1995 · N10242 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND CORROSION ON CHORD AT STA 227.8, BL ZERO. THE CORRODED SECTION OF CHORD WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 51-40-4. (X)
- [SDR CAL950635](https://openairdocs.org/sdr/CAL950635.md): Transducer · inoperative · Jul 31, 1995 · N10242 · Boeing 7372C0 · Autopilot System
  > FLT NR 1405 - ATL - THE AIRCRAFT HAD A SLIGHT YAW AFTER TAKEOFF FROM EWR. THE RANGE OF THE YAW GREW AS SPEED INCREASED. THE YAWING STOPPED AFTER THE YAW DAMP SWITCH WAS POSITIONED TO OFF. MAINTENANCE FOUND THE RUDDER PCU 'B' POSITION TRANSDUCER OPEN. THE T
- [SDR CAL950409](https://openairdocs.org/sdr/CAL950409.md): Hyd Line · chafed · May 20, 1995 · N10242 · Boeing 7372C0 · Hydraulic System, Main
  > FLT NR 1758 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC FLUID WHILE AT CRUISE. THE 'ABNORMAL' CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE HYDRAULIC LIN

## 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 = 'N10242' AND deregistration_id = 'N10242-1998-06-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10242-1998-06-23/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.