# Service difficulty reports: N16232, cancelled Jun 15, 1999

A list on [N16232, cancelled Jun 15, 1999](https://openairdocs.org/deregistered/N16232-1999-06-15.md).

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

- [SDR CALA9701782](https://openairdocs.org/sdr/CALA9701782.md): Cylinder · leaking · Dec 19, 1997 · N16232 · Boeing 737217 · Landing Gear Retraction/Extension System
  > THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO ZERO ON APPROACH TO EWR. ALL ABNORMAL AND EMERGENCY CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG HYDRAULIC TRANS
- [SDR CALA9700978](https://openairdocs.org/sdr/CALA9700978.md): Light · inoperative · Jun 28, 1997 · N16232 · Boeing 737217 · Emergency Lighting
  > INSPECTION FOUND FIRST CLASS EMERGENCY TRACK LIGHT AT L-1 DOOR INOPERATIVE. MAINTENANCE REPLACED SOCKET AND DAMAGED WIRE, OPERATIONAL CHECK WAS GOOD.
- [SDR CALA9700584](https://openairdocs.org/sdr/CALA9700584.md): Tr Unlock Light · illuminated · Apr 19, 1997 · N16232 · Boeing 737217 · Engine Thrust Reverser
  > ONTAKEOFF ROLL, CREW RECEIVED NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATE. REJECTED TAKEOFF AT 100 KNOTS. RETURNED TO GATE WHERE MAINTENANCE PERFORMED INSPECTION PER MM 5-5-111 P201-208. ALSO, TESTED TR SYSTEM IAW B7373 MM 78-32-01, ALL CHECKED NORMAL.
- [SDR CALA9601628](https://openairdocs.org/sdr/CALA9601628.md): Solenoid · inoperative · Nov 14, 1996 · N16232 · Boeing 737217 · Landing Gear Selector
  > THE GEAR LATCH WOULD NOT RELEASE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CIRCUIT BREAKERS WERE PULLED AND RESET IAW QRH PROCEDURES, BUT WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE
- [SDR CALA9601188](https://openairdocs.org/sdr/CALA9601188.md): Hyd Pump · leaking · Aug 19, 1996 · N16232 · Boeing 737217 · Hydraulic Pump (Electric/Engine), Main
  > THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED
- [SDR CALA9600906](https://openairdocs.org/sdr/CALA9600906.md): Pcu · inoperative · Jun 27, 1996 · N16232 · Boeing 737217 · Rudder Control System
  > THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE RIGHT ON TAKEOFF. FIFTEEN TO TWENTY DEGREES OF LEFT AILERON WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. THE YAW
- [SDR CALA9600798](https://openairdocs.org/sdr/CALA9600798.md): Strap · corroded · May 8, 1996 · N16232 · Boeing 737217 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRAP AT C-1 DOOR THRESHOLD CORRODED, STA 420 TO 500. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.
- [SDR CALA9600801](https://openairdocs.org/sdr/CALA9600801.md): Skin · cracked · May 6, 1996 · N16232 · Boeing 737217 · Trailing Edge Flaps
  > INSPECTION FOUND A 1 INCH CRACK IN UPPER SKIN OF RT WING INBOARD AFT FLAP. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND MM 51-20-0.
- [SDR CALA9600811](https://openairdocs.org/sdr/CALA9600811.md): Floorbeam · corroded · May 4, 1996 · N16232 · Boeing 737217 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, RBL 40 TO 55. THE CORRODED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND L-ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 52-20-1 AND 52-10-2.
- [SDR CALA9600810](https://openairdocs.org/sdr/CALA9600810.md): Floorbeam · corroded · May 3, 1996 · N16232 · Boeing 737217 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 328. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND MM 51-20.
- [SDR CALA9600812](https://openairdocs.org/sdr/CALA9600812.md): Frame · cracked · May 1, 1996 · N16232 · Boeing 737217 · Fuselage Main, Frame
  > INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO FRAME AT STA 480, S21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND 51-10-2.
- [SDR CALA9600803](https://openairdocs.org/sdr/CALA9600803.md): Bracket · cracked · May 1, 1996 · N16232 · Boeing 737217 · Vertical Stabilizer
  > INSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-0, 51-40-3, 51-10-2 AND 51-30-2.
- [SDR CALA9600802](https://openairdocs.org/sdr/CALA9600802.md): Bracket · cracked · May 1, 1996 · N16232 · Boeing 737217 · Vertical Stabilizer
  > INSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2.
- [SDR CALA9600797](https://openairdocs.org/sdr/CALA9600797.md): Channel · cracked · May 1, 1996 · N16232 · Boeing 737217 · Fuselage Miscellaneous Structure
  > THE STRINGER TO FLOOR BEAM ATTACHMENT U-CHANNEL HAD TWO 1 INCH CRACKS AT STA 500A, STRINGER 28R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7 AND 51-30-2.
- [SDR CALA9600796](https://openairdocs.org/sdr/CALA9600796.md): Intercostal · cracked · May 1, 1996 · N16232 · Boeing 737217 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 500, STRINGER 27L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2.
- [SDR CALA9600795](https://openairdocs.org/sdr/CALA9600795.md): Frame · cracked · May 1, 1996 · N16232 · Boeing 737217 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT STA 480, BL 0. THE CRACK WAS REMOVED AND A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.
- [SDR CALA9600799](https://openairdocs.org/sdr/CALA9600799.md): Blkhd Stiffener · cracked · Apr 30, 1996 · N16232 · Boeing 737217 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-21.
- [SDR CALA9600809](https://openairdocs.org/sdr/CALA9600809.md): Skin · dented · Apr 29, 1996 · N16232 · Boeing 737217 · Cargo/Baggage Doors
  > INSPECTION FOUND SEVERAL DENTS IN FORWARD CARGO DOOR SKIN. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2 AND 51-10-2.
- [SDR CALA9600808](https://openairdocs.org/sdr/CALA9600808.md): Skin · creased · Apr 29, 1996 · N16232 · Boeing 737217 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3 INCH CREASE IN FUSELAGE SKIN AT STA 1120, BL 0. THE CREASED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9600800](https://openairdocs.org/sdr/CALA9600800.md): Aux Track · cracked · Apr 29, 1996 · N16232 · Boeing 737217 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9600804](https://openairdocs.org/sdr/CALA9600804.md): Slide · inoperative · Apr 27, 1996 · N16232 · Boeing 737217 · Escape Slide
  > THE L-1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. THE COVER LANYARD WOULD NOT RELEASE AND THE SLIDE ONLY PARTIALLY INFLATED. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-30.
- [SDR CALA9600807](https://openairdocs.org/sdr/CALA9600807.md): Sign · inoperative · Apr 26, 1996 · N16232 · Boeing 737217 · Emergency Lighting
  > THE SELF ILLUMINATING EXIT SIGN IN AFT CABIN FAILED ILLUMINOSITY CHECK. THE EXIT SIGN WAS REMOVED AND REPLACED.
- [SDR CALA9600805](https://openairdocs.org/sdr/CALA9600805.md): Wire · damaged · Apr 26, 1996 · N16232 · Boeing 737217 · Light System Wiring
  > A SECTION OF FORWARD CABIN EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. THE WIRING AT FORWARD TRACK SECTION WAS REPAIRED IAW MM 33-50-0.
- [SDR CAL950860](https://openairdocs.org/sdr/CAL950860.md): Chord · cracked · Sep 22, 1995 · N16232 · Boeing 737217 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A 2 INCH CRACK FROM FORWARD HOLE TO AFT HOLE OF RT CHORD AT STA 727, STR 18A. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03165 AND EA 5310-02918. (X)
- [SDR CAL950235](https://openairdocs.org/sdr/CAL950235.md): Hyd Module · inoperative · Mar 27, 1995 · N16232 · Boeing 737217 · Hydraulic System, Main
  > MSY - FLT 1275 - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. THE GEAR WAS CYCLED AND RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED AGAIN WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION, BUT
- [SDR CAL950120](https://openairdocs.org/sdr/CAL950120.md): Hyd Valve · leaking · Feb 13, 1995 · N16232 · Boeing 737217 · Hydraulic System, Main
  > BWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MANUAL SHUT-OFF VALVE IN THE TAIL COMPARTMENT L

## 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 = 'N16232' AND deregistration_id = 'N16232-1999-06-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16232-1999-06-15/reports

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