# Service difficulty reports: N10248, cancelled Feb 9, 2000

A list on [N10248, cancelled Feb 9, 2000](https://openairdocs.org/deregistered/N10248-2000-02-09.md).

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

- [SDR CALA9801174](https://openairdocs.org/sdr/CALA9801174.md): Line · leaking · Jun 28, 1998 · N10248 · Boeing 737219 · Hydraulic System, Main
  > THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE. THE A-SYSTEM PUMPS WERE TURNED OFF AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE AT A-HYDRAULIC SYSTEM MODULE LEAKING. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE
- [SDR CALA9800825](https://openairdocs.org/sdr/CALA9800825.md): Hyd Line · leaking · May 9, 1998 · N10248 · Boeing 737219 · Hydraulic System, Main
  > AFTER 1 HOUR OF FLIGHT, A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT FLICKERED. FOUND HYD LINE LEAKING IN LEFT GEAR AREA. INSTALLED FLEX LINE REPAIR PER GMM 10-799-78.
- [SDR CALA9800106](https://openairdocs.org/sdr/CALA9800106.md): Battery Pack · discharged · Jan 25, 1998 · N10248 · Boeing 737219 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 4 FORWARD. THE BATTERY PACK WAS REMOVED AND REPLACED.
- [SDR CALA9701332](https://openairdocs.org/sdr/CALA9701332.md): Connector · loose · Sep 4, 1997 · N10248 · Boeing 737219 · Emergency Lighting
  > INSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND PIN HAD SLID OUT OF CANNON PLUG INSIDE OVERWING BODY FAIRING. THE PIN WAS REINSTALLED AND OPERATION OF EXIT LIGHT CHECKED GOOD.
- [SDR CALA9701145](https://openairdocs.org/sdr/CALA9701145.md): Doubler · corroded · Jul 5, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous Structure
  > STATION 259.5 AT STRINGER 27L BONDED DOUBLER CORRODED. INSTALLED BONDED DOUBLER IN ACCORDANCE WITH EC/RA 5330-02549 AND DRWG DHCSK 248-084.
- [SDR CALA9701153](https://openairdocs.org/sdr/CALA9701153.md): Skin · cracked · Jul 1, 1997 · N10248 · Boeing 737219 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH SRM 55-10-4 FIG 4 AND 55-10-3 FIG 829.
- [SDR CALA9701144](https://openairdocs.org/sdr/CALA9701144.md): Bulkhead Frame · corroded · Jun 26, 1997 · N10248 · Boeing 737219 · Fuselage Main, Bulkhead
  > CORROSION ON FRAME 1016 SURFACE STG 29L AND 29R AT BOTTOM OF AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA. INSTALLED PART IN ACCORDANCE WITH SRM 51-10-1 AND DRWG DHCSK 248-024.
- [SDR CALA9701220](https://openairdocs.org/sdr/CALA9701220.md): Skin · corroded · Jun 25, 1997 · N10248 · Boeing 737219 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 210.3 TO 259.9. THE SKIN WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9701147](https://openairdocs.org/sdr/CALA9701147.md): Skin · cracked · Jun 24, 1997 · N10248 · Boeing 737219 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LEADING EDGE DENTED AND CRACKED. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLR AND INSTALLED IN ACCORDANCE WITH SRM 55-10-03 AND 51-30-2.
- [SDR CALA9701151](https://openairdocs.org/sdr/CALA9701151.md): Seat Track · gouged · Jun 23, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 742B AT LBL24 UPPER LIP GOUGED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 51-10-6, 51-30-2, AND 53-10-5.
- [SDR CALA9701150](https://openairdocs.org/sdr/CALA9701150.md): Skin · cracked · Jun 23, 1997 · N10248 · Boeing 737219 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS 2 CRACK AT STATION 727A AND STRINGER 17L. REMOVED DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IN ACCORDANCE WITH SRM 53-30-3 FIG 25.
- [SDR CALA9701146](https://openairdocs.org/sdr/CALA9701146.md): T Cord · corroded · Jun 23, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous Structure
  > 'T' CHORD CORRODED AT STATION 340 STG 23R. REMOVED AND REPLACED CORRODED SECTION OF CHORD IN ACCORDANCE WITH SRM 51-30-2 AND 53-10-2.
- [SDR CALA9701154](https://openairdocs.org/sdr/CALA9701154.md): Seat Track · gouged · Jun 22, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach Fittings
  > NUMBER 4 SEAT TRACK GOUGED AFT OF FRAME STATION 767. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 51-30-2, 53-10-2, 53-10-5, AND 51-10-6.
- [SDR CALA9701148](https://openairdocs.org/sdr/CALA9701148.md): Frame · cracked · Jun 22, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous Structure
  > E/E DOOR FRAME CENTER U CHANNEL CRACKED IN 2 PLACES. REPAIRED CRACKED DOOR FRAME IN ACCORDANCE WITH SRM 51-40-6 AND 51-10-6.
- [SDR CALA9701143](https://openairdocs.org/sdr/CALA9701143.md): Skin · corroded · Jun 22, 1997 · N10248 · Boeing 737219 · Fuselage Main, Plate/Skin
  > FORWARD FUSELAGE FS 450, STA 26L SKIN BULGING. REMOVED DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 57-10-6 AND 53-30-3.
- [SDR CALA9701142](https://openairdocs.org/sdr/CALA9701142.md): Track · gouged · Jun 22, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach Fittings
  > NUMBER 4 SEAT TRACK GOUGED AFT OF FRAME STATION 767. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IN ACCORDANCE WITH SRM 51-30-2, 53-10-2, 53-10-5, AND 51-10-6.
- [SDR CALA9701050](https://openairdocs.org/sdr/CALA9701050.md): Chord · corroded · Jun 16, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-CHORD CORRODED AT STA 351, RBL 16. THE CHORD WAS REPAIRED IAW SRM 51-10-6 AND 53-10-1.
- [SDR CALA9701005](https://openairdocs.org/sdr/CALA9701005.md): Chord · corroded · Jun 16, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-CHORD CORRODED AT STA 340, STRINGER 23R. THE CHORD WAS REPLACED IAW SRM 51-30-2 AND 53-10-2.
- [SDR CALA9701004](https://openairdocs.org/sdr/CALA9701004.md): Skin · dented · Jun 13, 1997 · N10248 · Boeing 737219 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD FUSELAGE SKIN DENTED FIVE INCHES BELOW S17L AT STA 380 TO 400. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.
- [SDR CALA9701149](https://openairdocs.org/sdr/CALA9701149.md): Seat Track · gouged · Jun 11, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach Fittings
  > NUMBER 4 SEAT TRACK GOUGED AT FS 727. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5 AND BAC 1520-1342.
- [SDR CALA9701152](https://openairdocs.org/sdr/CALA9701152.md): Seat Track · gouged · Jun 10, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK GOUGED AT FS 727 TO 731A AT LBL24. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5.
- [SDR CALA9700234](https://openairdocs.org/sdr/CALA9700234.md): Power Contl Unit · inoperative · Feb 21, 1997 · N10248 · Boeing 737219 · Aileron Control System
  > THE AIRCRAFT HAD A BRIEF HISTORY OF STIFF AILERONS. MAINTENANCE FOUND THE B-SYSTEM AILERON POWER CONTROL UNIT AT FAULT. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71, PAGE 401. AN ADJUSTMENT/TEST WAS PERFORMED ON THE AILERON PCU IAW MM 27-11-71,
- [SDR CALA9700131](https://openairdocs.org/sdr/CALA9700131.md): Circuit Breaker · tripped · Feb 3, 1997 · N10248 · Boeing 737219 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR COULD NOT BE RETRACTED AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEVER LATCH AND PRESS WARNING
- [SDR CALA9601316](https://openairdocs.org/sdr/CALA9601316.md): Wheel Half · detached · Sep 15, 1996 · N10248 · Boeing 737219 · Wheel/Ski/Float
  > WHILE REPLACING THE NR 4 MLG TIRE/WHEEL ASSEMBLY DUE TO TIRE WEAR, THE INNER WHEEL ASSEMBLY HUB WAS FOUND DETACHED FROM WHEEL HALF. THE NR 4 TIRE/WHEEL ASSEMBLY WAS REMOVED AND REPLACED. IN ADDITION, THE NR 3 MLG TIRE/WHEEL ASSEMBLY WAS REMOVED AND REPLACED
- [SDR CALA9601306](https://openairdocs.org/sdr/CALA9601306.md): Fuel Pump · failed · Sep 12, 1996 · N10248 · Boeing 737219 · Engine Fuel Pump
  > THE NR 1 ENGINE SURGED AND ROLLED BACK TO APPROXIMATELY 1.6 EPR AND 85 PERCENT ON TAKEOFF AT ROTATION. THE ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENTS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED TH
- [SDR CALA9601167](https://openairdocs.org/sdr/CALA9601167.md): T1 Blade · fractured · Aug 13, 1996 · N10248 · Boeing 737219 · Turbine Section
  > THE NR 1 ENGINE ROLLED BACK TO 1.4 EPR AND AIRCRAFT VIBRATION WAS FELT AFTER GEAR RETRACTION. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO CAE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DAMAGED. THE NR 1 ENGINE WAS
- [SDR CALA9601111](https://openairdocs.org/sdr/CALA9601111.md): Skin · cracked · Jul 30, 1996 · N10248 · Boeing 737219 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.4375 INCH CRACK IN FUSELAGE SKIN BELOW FIRST OFFICER'S EYEBROW WINDOW. THE SKIN WAS REPAIRED IAW SRM 53-30-3, PAGES 26 TO 28E, REPAIR NR 7.
- [SDR CAL960441](https://openairdocs.org/sdr/CAL960441.md): Control Cable · broken · Apr 5, 1996 · N10248 · Boeing 737219 · Trailing Edge Flap Control System
  > EWR - FLT 1160 - THE AIRCRAFT ROLLED LEFT ON FLAP EXTENSION FOR LANDING ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD TRAILING EDGE FLAP JAMMED DUE TO A BROKEN FOLLOW-UP CABLE ON INBOARD JACKSCREW. CABLES BC-3 AN
- [SDR CAL950589](https://openairdocs.org/sdr/CAL950589.md): Rib · corroded · Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge Devices
  > GSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT THE NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS CLEANED UP AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3 AND SRM 51-30-2. (X)
- [SDR CAL950588](https://openairdocs.org/sdr/CAL950588.md): Intercostal · cracked · Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge Devices
  > GSO - THE NR 6 SLAT INTERIOR HAD TWO EACH INTERCOSTALS CRACKED AT INBOARD SLAT TRACK ATTACH FITTING. EACH CRACK WAS APPROXIMATELY.50 INCH LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-50-3. (X)
- [SDR CAL950587](https://openairdocs.org/sdr/CAL950587.md): Skin · cracked · Jul 1, 1995 · N10248 · Boeing 737219 · Wing, Plate/Skin
  > GSO - A.50 INCH CRACK WAS FOUND IN LT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUT-OUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (X)
- [SDR CAL950586](https://openairdocs.org/sdr/CAL950586.md): Intercostal · cracked · Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge Devices
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN INTERCOSTAL OF NR 2 SLAT INBOARD SLAT TRACK, AT SLAT TRACK ATTACH FITTING AREA. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X)
- [SDR CAL950585](https://openairdocs.org/sdr/CAL950585.md): Rib · cracked · Jul 1, 1995 · N10248 · Boeing 737219 · Wing, Rib/Bulkhead
  > GSO - INSPECTION FOUND A.25 INCH CRACK IN RADIUS OF RT RIB AT LOWER FORWARD ATTACH HOLE, STA 738. THE CRACK WAS STOP-DRILLED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-10-5. (X)
- [SDR CAL950584](https://openairdocs.org/sdr/CAL950584.md): Webbing · cracked · Jul 1, 1995 · N10248 · Boeing 737219 · Wing Miscellaneous Structure
  > GSO - THE RIGHT WING CENTER INBOARD OF STA 139 HAD WEBBING WITH CRACKS AROUND FASTENER HOLES. THE CRACKS WERE.25 INCH LONG. THE CRACKED AREAS WERE REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-40-6. (X)
- [SDR CAL950354](https://openairdocs.org/sdr/CAL950354.md): Eel Power Supply · inoperative · May 1, 1995 · N10248 · Boeing 737219 · Emergency Lighting
  > GSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE 95ZZZW711.
- [SDR 95ZZZW711](https://openairdocs.org/sdr/95ZZZW711.md): Eel Batt · discharged · May 1, 1995 · N10248 · Boeing 737219 · Emergency Lighting
  > GSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE CAL950354.
- [SDR CAL950341](https://openairdocs.org/sdr/CAL950341.md): Eel Wiring · broken · Apr 30, 1995 · N10248 · Boeing 737219 · Emergency Lighting
  > FLT NR 1275 - GSO - AIRCRAFT ARRIVED WITH EMERGENCY PATH LIGHTS ON, LIGHTS WOULD NOT GO OUT REPLACED BATTERY PACK OPS CHECK GOOD. THE BATTERY PACK WAS NOT AT FAULT. MAINTENANCE FOUND WIRING BROKEN AT BOTH THE AFT BULLNOSE LIGHT ASSEMBLY AND AT THE EMERGENCY
- [SDR CAL950010](https://openairdocs.org/sdr/CAL950010.md): Engine · malfunctioned · Jan 3, 1995 · N10248 · Boeing 737219 · Engine (Turbine/Turboprop)
  > FLT NR 1629 - ATL - THE NR 2 ENGINE OIL TEMPERATURE REACHED RED LINE WHILE EN ROUTE TO MSY. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL C

## 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 = 'N10248' AND deregistration_id = 'N10248-2000-02-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10248-2000-02-09/reports

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