# Service difficulty reports: N10236, cancelled Jun 15, 1999

A list on [N10236, cancelled Jun 15, 1999](https://openairdocs.org/deregistered/N10236-1999-06-15.md).

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

- [SDR CALA9801537](https://openairdocs.org/sdr/CALA9801537.md): Solenoid · inoperative · Aug 26, 1998 · N10236 · Boeing 737222 · Landing Gear Selector
  > THE LANDING GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION TO UP UNLESS OVERRIDE TRIGGER WAS PULLED AFTER TAKEOFF. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER LOCK SOLENOID AT FAULT. THE LEVER LOCK SOLENOID WAS REMOVED AND REPLACED IAW MM 32-31-31. IN AD
- [SDR CALA9800690](https://openairdocs.org/sdr/CALA9800690.md): Line · leaking · Apr 23, 1998 · N10236 · Boeing 737222 · Hydraulic System, Main
  > THE B SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.8 GALLONS IN FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF THE B SYSTEM LOW QUANTITY LIGHT. THE ABNORMAL CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING ED
- [SDR CALA9800390](https://openairdocs.org/sdr/CALA9800390.md): Sign · shorted · Mar 5, 1998 · N10236 · Boeing 737222 · Passenger Compartment Lighting
  > THE CREW REPORTED SMOKE APPEARED MOMENTARILY IN CABIN AT PUSH TIME. MAINTENANCE FOUND THE NO SMOKING FASTEN SEAT BELT SYSTEM INOPERATIVE WITH THE ROW 6 ABC OVERHEAD PSU BASE ASSEMBLY SHORTED OUT. THE WIRES FOR PSU AT ROW 6 ABC WERE CUT AND STOWED AND THE SYS
- [SDR CALA9701651](https://openairdocs.org/sdr/CALA9701651.md): Floorbeam · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 1.5 AND LBL 9. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03623.
- [SDR CALA9701650](https://openairdocs.org/sdr/CALA9701650.md): Floorbeam · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 312, RT OUTBOARD END. THE CORRODED SECTION WAS REMOVED IAW SRM 51-30-2, REPAIR FILLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2, AND 51-30-2.
- [SDR CALA9701649](https://openairdocs.org/sdr/CALA9701649.md): Web · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED AT BS 330 TO 340, RT CUSP. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.
- [SDR CALA9701648](https://openairdocs.org/sdr/CALA9701648.md): Angle · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION IN ANGLE AT BS 797, S26L. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-3, FIGURE NR 1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-2, AND 51-30-0.
- [SDR CALA9701647](https://openairdocs.org/sdr/CALA9701647.md): Floorbeam · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 344 FROM LBL 24 TO RBL 24. THE CORRODED FLOORBEAM CAP WAS REMOVED, A REPLACEMENT CAP AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 53-30-2.
- [SDR CALA9701646](https://openairdocs.org/sdr/CALA9701646.md): Support · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344, LBL 10. THE FLOOR SUPPORT WAS REMOVED IAW SRM 53-10-2. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.
- [SDR CALA9701645](https://openairdocs.org/sdr/CALA9701645.md): Support · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294.5 TO 312, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.
- [SDR CALA9701644](https://openairdocs.org/sdr/CALA9701644.md): Frame · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > INSPECTION FOUND CABIN FLOOR FRAME CORRODED AT STA 987 FROM BL 55L TO BL 55R. THE CORRODED UPPER CAP WAS REMOVED IAW SRM 51-30-2. A NEW UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.
- [SDR CALA9701643](https://openairdocs.org/sdr/CALA9701643.md): Floorbeam · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CAP AND WEB CORRODED INSIDE E AND E COMPARTMENT AT BS 328. THE CORRODED SECTION OF BEAM CAP WAS REMOVED AND A NEW SECTION AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. THE CORRODED SECTION OF FLOORBEAM WEB
- [SDR CALA9701642](https://openairdocs.org/sdr/CALA9701642.md): Support · corroded · Nov 19, 1997 · N10236 · Boeing 737222 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT UPPER PLATE CORRODED AT STA 328 TO 344, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.
- [SDR CALA9701376](https://openairdocs.org/sdr/CALA9701376.md): Hyd Line · cracked · Sep 17, 1997 · N10236 · Boeing 737222 · Hydraulic System, Main
  > THE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE CRACKED. THE HYDRAULIC PRESSURE LINE WAS REMOVED
- [SDR CALA9601488](https://openairdocs.org/sdr/CALA9601488.md): Stringer · cracked · Oct 12, 1996 · N10236 · Boeing 737222 · Fuselage Main, Longeron/Stringer
  > RIGHT A/C BAY OUTBOARD SIDE APPROX 1.5 LONG CRACK EXTENDING UNDER STIFFENER AT FUSELAGE STATION. REMOVED STIFFENER, STOP DRILLED CRACK, AND INSTALLED PER SRM 51-10-1 AND 51-30-2.
- [SDR CALA9601487](https://openairdocs.org/sdr/CALA9601487.md): Skin · corroded · Oct 12, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE STATION 877 TO 857 AT STATION 24R LAP JOINT SWOLLEN BETWEEN FASTENER HEADS. REMOVED FASTENERS AT LAP JOINT AND CORROSION PER SRM 51-10-2 AND 51-10-6 AND INSTALLED FASTENERS PER SRM 51-30-2.
- [SDR CALA9601486](https://openairdocs.org/sdr/CALA9601486.md): Battery Pack · discharged · Oct 12, 1996 · N10236 · Boeing 737222 · Emergency Lighting
  > L2 DOOR MOUNTED ESCAPE SLIDE LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-63.
- [SDR CALA9601485](https://openairdocs.org/sdr/CALA9601485.md): Skin · bulged · Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN ON LEFT SIDE NOSE WHEEL WELL EDGE HAS BULGES AND RIVETS PULLING THROUGH FROM STATION 235.8 TO 251.8. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED PER SRM 53-30-3, 51-30-2, AND 51-10-2.
- [SDR CALA9601484](https://openairdocs.org/sdr/CALA9601484.md): Skin · oil can · Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN OIL CAN AT BS 390L AND STR 17L. TRIMMED OUT DAMAGED AREA PER SRM 53-30-3, FABRICATED DOUBLER PER SRM 53-30-3 AND 51-10-2, INSTALLED DOUBLER PER SRM 53-30-3 AND 51-30-2.
- [SDR CALA9601483](https://openairdocs.org/sdr/CALA9601483.md): Blkhd Web · cracked · Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Bulkhead
  > FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON LEFT SIDE ABOVE WL 208 APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED PER SRM 53-10-11, 51-30-2, AND 51-10-2.
- [SDR CALA9601482](https://openairdocs.org/sdr/CALA9601482.md): Bulkhead · cracked · Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Bulkhead
  > FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON RIGHT SIDE ABOVE WL STA 208, APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS, INSTALLED PER SRM 53-10-11, 53-30-2, AND 51-10-2.
- [SDR CALA9601481](https://openairdocs.org/sdr/CALA9601481.md): Skin · cracked · Oct 3, 1996 · N10236 · Boeing 737222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED IN 2 PLACES ON LEFT SIDE BETWEEN STA 727A AND 727B AT STRINGER 18 APPROX 3 EACH. CUT OUT DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUBLER AND INSTALLED PER SRM 53-30-3, 53-30-2, AND 51-10-2.
- [SDR CAL950970](https://openairdocs.org/sdr/CAL950970.md): Battery Pack · discharged · Oct 24, 1995 · N10236 · Boeing 737222 · Emergency Lighting
  > GSO - EXIT LIGHT INOP. REPLACED RIGHT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)
- [SDR CAL950969](https://openairdocs.org/sdr/CAL950969.md): Battery Pack · discharged · Oct 24, 1995 · N10236 · Boeing 737222 · Emergency Lighting
  > GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND LEFT EXTERNAL EMERGENCY LIGHT INOP. REPLACED LEFT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)
- [SDR CAL950968](https://openairdocs.org/sdr/CAL950968.md): Battery Pack · discharged · Oct 24, 1995 · N10236 · Boeing 737222 · Emergency Lighting
  > GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND BATTERY PACK INOP. REPLACED BATTERY PACK FOR L-1 SLIDE. (M)
- [SDR CAL950967](https://openairdocs.org/sdr/CAL950967.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATLY.75 INCH AT BS 500A BETWEEN S20L, S21L, AND ABOVE S23L, REMOVED AND REPLACED. (M0
- [SDR CAL950966](https://openairdocs.org/sdr/CAL950966.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK APPROXIMATELY.75 INCH IN FRAME SEGMENT AT BS 400 BETWEEN S21L AND S22L, REMOVED AND REPLACED. (M)
- [SDR CAL950965](https://openairdocs.org/sdr/CAL950965.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATELY.75 INCH AT BS 500A BETWEEN S20R AND S21R, REMOVED AND REPLACED. (M)
- [SDR CAL950964](https://openairdocs.org/sdr/CAL950964.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN ONE-HALF D-CHECK. DURING INSPECTION, FOUND CRACK APPROXIMATELY.75 INCH AT BS 420 BETWEEN S21L, S22L, S23L. STOP DRILLED CRACK AND INSTALLED DOUBLER. (X)
- [SDR CAL950963](https://openairdocs.org/sdr/CAL950963.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN ONE-HALF D-CHECK DURING INSPECTION, FOUND CRACK FRAME SEGMENT APPROXIMATELY.05 INCH AT BS 480 BETWEEN S20L AND S21L. REMOVED AND REPLACED. (X)
- [SDR CAL950962](https://openairdocs.org/sdr/CAL950962.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - AIRCRAFT IN 1/2 D-CHECK DURING INSPECTION, FOUND CRACK IN FRAME SEGMENT AT BS 460 APPROXIMATELY.75 INCH, BETWEEN S20L AND S21L. REMOVED AND REPAIRED. (X)
- [SDR CAL950960](https://openairdocs.org/sdr/CAL950960.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500B BETWEEN STR 19L AND STR 20L, AND BETWEEN STR 25L AND STR 27L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY.33 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X
- [SDR CAL950959](https://openairdocs.org/sdr/CAL950959.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500 BETWEEN STR 21L AND STR 22L AND STR 22L AND STR 23L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY.75 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)
- [SDR CAL950958](https://openairdocs.org/sdr/CAL950958.md): Frame · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A CRACK IN FRAME AT BS 420 BETWEEN S22R AND S21R AND BETWEEN S21R AND S20R. THE CRACK AT EACH LOCATION WAS APPROXIMATELY.75 INCH LONG. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)
- [SDR CAL950956](https://openairdocs.org/sdr/CAL950956.md): Skin · cracked · Oct 24, 1995 · N10236 · Boeing 737222 · Cargo/Baggage Doors
  > GSO - INSPECTION FOUND A.50 INCH CRACK AT FORWARD LOWER CORNER OF AFT CARGO DOOR CUT-OUT, EXTERNAL SKIN. THE CRACKED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW TIMCO ENGINEERING ORDER RFO-01655. (X)
- [SDR CAL950527](https://openairdocs.org/sdr/CAL950527.md): Hyd Line · worn · Jun 28, 1995 · N10236 · Boeing 737222 · Hydraulic System, Main
  > FLT NR 1728 - CLE - THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IND. BOTH THE RED AND GREEN LIGHTS REMAINED ON. WHEN THE GEAR HANDLE WAS PLACED DOWN, THE RED LIGHT EXTINGUISHED. THE HYDRAULIC QUANTITY GAUGE DROPPED TO.8 GALS. THE AIRCRAFT W

## 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 = 'N10236' AND deregistration_id = 'N10236-1999-06-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10236-1999-06-15/reports

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