# Service difficulty reports: N14245, cancelled Mar 11, 1999

A list on [N14245, cancelled Mar 11, 1999](https://openairdocs.org/deregistered/N14245-1999-03-11.md).

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

- [SDR CALA9802174](https://openairdocs.org/sdr/CALA9802174.md): Accessory Unit · malfunctioned · Dec 11, 1998 · N14245 · Boeing 7372C0 · Landing Gear Position and Warning
  > THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON FINAL APPROACH TO EWR. THE RED LIGHT WAS ON, A MANUAL GEAR EXTENSION WAS PERFORMED DURING GO-AROUND AND THE GEAR WAS VISUALLY CHECKED THROUGH VIEW PORT. THE GREEN LIGHT ILLUMINATED ON SEC
- [SDR CALA9801990](https://openairdocs.org/sdr/CALA9801990.md): Battery Pack · discharged · Oct 29, 1998 · N14245 · Boeing 7372C0 · Emergency Lighting
  > INSPECTION FOUND THE AISLE PATH EMERGENCY LIGHTING STRIP IS INOPERATIVE FORWARD OF ROW 12 AND AFT OF ROW 20. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA9801802](https://openairdocs.org/sdr/CALA9801802.md): Skin · corroded · Sep 16, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 294.5 BETWEEN S26L AND S27L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5330-02708 AND ECRA 5330-02707.
- [SDR CALA9801760](https://openairdocs.org/sdr/CALA9801760.md): Skin · cracked · Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD GALLEY DOOR CUTOUT UPPER FORWARD CORNER CRACKED AT STA 312. THE CRACKED AREA WAS ROUTED OUT. REPAIR FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30, ECRA 5330-02703 AND BOEING DRAWING 65C33800.
- [SDR CALA9801759](https://openairdocs.org/sdr/CALA9801759.md): Skin · cracked · Sep 14, 1998 · N14245 · Boeing 7372C0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK IN AFT CARGO DOOR SKIN CUTOUT AT LOWER AFT CORNER. THE EXISTING DOUBLERS WERE REMOVED, FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5330-02710.
- [SDR CALA9801758](https://openairdocs.org/sdr/CALA9801758.md): Strap · punctured · Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A HOLE IN STRAP JUST FORWARD OF E & E COMPARTMENT ENTRANCE. A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND ECRA 5330-02712.
- [SDR CALA9801757](https://openairdocs.org/sdr/CALA9801757.md): Doubler · corroded · Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERNAL DOUBLER CORRODED AT STA 294.5 LEFT. THE CORRODED SECTION OF DOUBLER WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5330-02709.
- [SDR CALA9801712](https://openairdocs.org/sdr/CALA9801712.md): Floor · cracked · Sep 10, 1998 · N14245 · Boeing 7372C0 · Fuselage Floor Panel
  > INSPECTION FOUND A 1 INCH CRACK AT SCREW IN FLOOR PANEL AT AFT CARGO COMPARTMENT DOOR ENTRANCE. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11. THE FLOOR PANEL WAS REINSTALLED IAW SRM 51-30-2.
- [SDR CALA9801711](https://openairdocs.org/sdr/CALA9801711.md): Cowl · cracked · Sep 10, 1998 · N14245 · Boeing 7372C0 · Engine Cowling System
  > INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN NR 2 ENGINE INBOARD ENGINE COWL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2. TWO REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-0.
- [SDR CALA9801708](https://openairdocs.org/sdr/CALA9801708.md): Skin · gouged · Sep 10, 1998 · N14245 · Boeing 7372C0 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD FOREFLAP GOUGED IN TWO PLACES AT INBOARD SIDE. THE GOUGED AREAS WERE TRIMMED OUT. AN ADHESIVE PRIMER AND BONDED FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-40-6, 51-40-9, AND MM 51-20-11.
- [SDR CALA9801624](https://openairdocs.org/sdr/CALA9801624.md): Skin · corroded · Sep 3, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND INSIDE OF SKIN CORRODED IN LT WHEEL WELL AT STA 219.8, STRINGER 27L. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-6, 53-10-1, 53-30-3, 51-10-2, AND MM 51-11-20.
- [SDR CALA9801604](https://openairdocs.org/sdr/CALA9801604.md): Angle · corroded · Sep 1, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND VERTICAL ANGLE CORRODED AT FS 277. THE VERTICAL ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801603](https://openairdocs.org/sdr/CALA9801603.md): Longeron · delaminated · Sep 1, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND NLG WHEEL WELL LONGERON 28L DELAMINATED AT BS 287. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, 51-30-2, AND MM 51-20-11.
- [SDR CALA9801602](https://openairdocs.org/sdr/CALA9801602.md): Clip · corroded · Aug 31, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR CLIP CORRODED AT STA 277, LBL 17. THE SHEAR CLIP WAS REMOVED AND REPLACED IAW SRM 53-10-2 AND 51-30-2.
- [SDR CALA9801583](https://openairdocs.org/sdr/CALA9801583.md): Stiffener · cracked · Aug 28, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL STIFFENER AT AFT CARGO FORWARD PRESSURE BULKHEAD STA 727, LBL 18. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801569](https://openairdocs.org/sdr/CALA9801569.md): Angle · corroded · Aug 27, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT STA 294.5 TO 325.38, LBL 8. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9801536](https://openairdocs.org/sdr/CALA9801536.md): Skin · cracked · Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.0625 AND 1.5 INCH CRACK IN FUSELAGE SKIN DOUBLER FORWARD OF COCKPIT WINDOW AT STA 178, BL 0. THE SKIN DOUBLER WAS REMOVED IAW SRM 51-30-2. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5310-03754.
- [SDR CALA9801535](https://openairdocs.org/sdr/CALA9801535.md): Floorbeam · cracked · Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER CHORD AT STA 675, BBL 0.07. THE LOWER CHORD WAS REMOVED AND A NEW LOWER CHORD ANGLE AND TWO REINFORCING SPLICE ANGLES WERE INSTALLED IAW ECRA 5710-01929.
- [SDR CALA9801523](https://openairdocs.org/sdr/CALA9801523.md): Angle · cracked · Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN LT FORWARD WING TO BODY FAIRING ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5350-01227 AND 51-30-2.
- [SDR CALA9801522](https://openairdocs.org/sdr/CALA9801522.md): Floorbeam · cracked · Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM WEB AT STA 663, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5710-01931.
- [SDR CALA9801489](https://openairdocs.org/sdr/CALA9801489.md): Casting · cracked · Aug 19, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon Structure
  > INSPECTION FOUND NR 1 ENGINE PYLON PANEL LOWER SIDE NUT PLATE AREA CRACKED AND FOUND A 1 CRACK IN INBOARD FORWARD ATTACH CASTING. THE CASTING WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-20-11.
- [SDR CALA9801482](https://openairdocs.org/sdr/CALA9801482.md): Rib · gouged · Aug 18, 1998 · N14245 · Boeing 7372C0 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A GOUGE IN LT WING LEADING EDGE RIB INBOARD OF NR 3 SLAT. A REPAIR ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-21-31.
- [SDR CALA9801468](https://openairdocs.org/sdr/CALA9801468.md): Angle · cracked · Aug 15, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD ANGLE IN AFT CARGO COMPARTMENT AT STA 727, BL 0, STRINGER 29L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801466](https://openairdocs.org/sdr/CALA9801466.md): Fairing · cracked · Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 1 INCH CRACK ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 183.4. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2, 51-40-2, FIGURE 1, AND 51-30-2.
- [SDR CALA9801465](https://openairdocs.org/sdr/CALA9801465.md): Fairing · cracked · Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 181.0. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2 AND 51-40-2, FIGURE 1
- [SDR CALA9801464](https://openairdocs.org/sdr/CALA9801464.md): Longeron · cracked · Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon, Longeron/Stringer
  > INSPECTION FOUND A 2.5 INCH CRACK ON END CAP (LONGERON) PANEL NR 2 ENGINE FAIRING. THE LONGERON WAS REMOVED AND A NEW LONGERON WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801463](https://openairdocs.org/sdr/CALA9801463.md): Fairing · chafed · Aug 15, 1998 · N14245 · Boeing 7372C0 · Engine Thrust Reverser
  > INSPECTION FOUND A HOLE CHAFED THROUGH NR 1 ENGINE THRUST REVERSER EXTENSION UPPER CLOSE OUT FAIRING. THE AREA WAS REPAIRED IAW SRM 51-20-1, FIGURE 7.
- [SDR CALA9801081](https://openairdocs.org/sdr/CALA9801081.md): Tat Indicator · shorted · Jun 16, 1998 · N14245 · Boeing 7372C0 · Outside Air Temperature Indicator/Sensor
  > THE TAT CIRCUIT BREAKER POPPED FOLLOWED BY SMOKE IN THE COCKPIT AFTER TAKEOFF. THE SMOKE APPEARED TO COME FROM THE TAT GUAGE. THE AIRCRAFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TAT INDICATOR AT FAULT. THE INDICATOR WAS
- [SDR CALA9800903](https://openairdocs.org/sdr/CALA9800903.md): Web · cracked · May 27, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN SHEAR BEAM WEB IN LT WHEEL WELL AT STA 727. REPAIRED IAW DRAWING 65C29228.
- [SDR CALA9800415](https://openairdocs.org/sdr/CALA9800415.md): Circuit Breaker · inoperative · Mar 12, 1998 · N14245 · Boeing 7372C0 · Landing Gear Selector
  > THE LANDING GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION AFTER TAKEOFF FROM MSY. THE GEAR LIGHTS CIRCUIT BREAKER WAS FOUND POPPED. THE CIRCUIT BREAKER WAS RESET AND THE GEAR RAISED NORMALLY. A FEW MINUTES LATER THE LIGHTS CIRCUIT BREAKER POPPED AGA
- [SDR CALA9800391](https://openairdocs.org/sdr/CALA9800391.md): Fire Loop · chafed · Mar 5, 1998 · N14245 · Boeing 7372C0 · Fire Detection
  > THE NR 2 ENG FIRE WARNING LIGHT AND BELL ACTIVATED BRIEFLY SEVERAL TIMES IN FLIGHT. THE DURATION OF EACH WARNING WAS LESS THAN ONE SECOND. THE NR 2 ENG FIRE LIGHT AND WARNING BELL CAME ON STEADY AFTER LANDING AT CLE. BOTH FIRE BOTTLES WERE DISCHARGED, AND S
- [SDR CALA9700859](https://openairdocs.org/sdr/CALA9700859.md): Web · cracked · May 24, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK AT LIGHTENING HOLE OF WEB, STA 360 JUST ABOVE STRINGER 17L. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1.
- [SDR CALA9700858](https://openairdocs.org/sdr/CALA9700858.md): Support · corroded · May 19, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CLOSET FLOOR SUPPORT CORRODED AT FS 1010, RBL 17.0 TO RBL 46.5. THE FLOOR SUPPORT WAS REMOVED, A FLOOR SUPPORT AND HAT CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-30-2.
- [SDR CALA9700764](https://openairdocs.org/sdr/CALA9700764.md): Web · corroded · May 15, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR WEB CORRODED AT STA 1016 RBL 15. THE CORRODED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.
- [SDR CALA9700762](https://openairdocs.org/sdr/CALA9700762.md): Web · corroded · May 15, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR WEB CORRODED AT STA 1016 RBL 30 TO 36. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-00-6, 51-30-8, AND 51-40-3.
- [SDR CALA9700761](https://openairdocs.org/sdr/CALA9700761.md): Floorbeam · corroded · May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT FS 520 LBL 24.5. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-6.
- [SDR CALA9700760](https://openairdocs.org/sdr/CALA9700760.md): Floor Support · corroded · May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344 RBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-10-2.
- [SDR CALA9700759](https://openairdocs.org/sdr/CALA9700759.md): Strap · corroded · May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LAV FLOOR WEB STRAP CORRODED AT STA 1006 TO 1024 LBL 28. THE STRAP WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-2, 51-10-2.
- [SDR CALA9700758](https://openairdocs.org/sdr/CALA9700758.md): Intercostal · cracked · May 13, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN FS 303.9 AND 294.5 AT STRINGER 15L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-1, 51-10-2.
- [SDR CALA9700757](https://openairdocs.org/sdr/CALA9700757.md): Floor Support · corroded · May 13, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312 LBL 12. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, FIGURE 7, 51-20-0 AND 51-10-2.
- [SDR CALA9700755](https://openairdocs.org/sdr/CALA9700755.md): Skin · dented · May 12, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND, FUSELAGE SKIN DENTED AT STA 940, LONGERON 20L. THE DENTED AREA WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 6.
- [SDR CALA9700763](https://openairdocs.org/sdr/CALA9700763.md): Skin · corroded · May 11, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 410, STRINGER 16L. THE SKIN WAS REMOVED, A DOUBLER WAS FABRICATED IAW SRM 53-30-3, FIGURE 6 AND 53-30-3, FIGURE 6 SHEET 4.
- [SDR CALA9700756](https://openairdocs.org/sdr/CALA9700756.md): Intercostal · cracked · May 8, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN MAIN DECK FLOOR INTERCOSTAL AT FS 520, LBL 24.5. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-01, 51-40-2, FIGURE 1 AND 51-30-2.
- [SDR CALA9601322](https://openairdocs.org/sdr/CALA9601322.md): Solenoid Valve · malfunctioned · Sep 22, 1996 · N14245 · Boeing 7372C0 · Rudder Control System
  > THE AIRCRAFT BECAME HARD TO CONTROL ABOUT THE VERTICAL AXIS WHILE ON FINAL APPROACH. THE AIRCRAFT WANTED TO DUTCH ROLL AND YAW EXCESSIVELY AND DIDN'T RESPOND EFFECTIVELY TO PILOT CONTROLLED INPUTS ON RUDDER. THE AIRCRAFT HANDLED THE SAME WITH AND WITHOUT YAW
- [SDR CALA9601057](https://openairdocs.org/sdr/CALA9601057.md): Fitting · cracked · Jul 11, 1996 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A CRACK IN VERTICAL LEG OF FORWARD HALF OF LOWER LT FITTING AT B.S. 695, STRINGER 18A. THE CRACKED FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW DRAWING NR 65C34490 AND SA008-5310-02456 THROUGH SA0013-5310-02456.
- [SDR CALA9601061](https://openairdocs.org/sdr/CALA9601061.md): Skin · corroded · Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT OUTFLOW VALVE. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 51-10-6, AND 51-10-2.
- [SDR CALA9601060](https://openairdocs.org/sdr/CALA9601060.md): Skin · corroded · Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED JUST AFT OF AFT CARGO DOOR AFT LOWER CORNER. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND SPLICE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2.
- [SDR CALA9601059](https://openairdocs.org/sdr/CALA9601059.md): Bulkhead Web · cracked · Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD WEB AT WL 218, STA 178 ON BOTH LT AND RT SIDES. BOTH CRACKED AREAS OF BULKHEAD WEB WERE CUT OUT. FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM'S 53-10-2, 51-10-2, AND 51-30-2.
- [SDR CALA9601058](https://openairdocs.org/sdr/CALA9601058.md): Chord · cracked · Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A CRACK PAST SECOND FASTENER HOLE OF CHORD AT STRINGER 18A ON BOTH THE LT AND RT SIDES OF B.S. 727. THE CHORD SEGMENTS WERE REMOVED AND REPLACED IAW BOEING DRAWING 65C33722 AND CAL WORK CARD 15-5310-1-0023.
- [SDR CAL950597](https://openairdocs.org/sdr/CAL950597.md): Hyd Line · leaking · Jul 17, 1995 · N14245 · Boeing 7372C0 · Hydraulic System, Main
  > EWR - FLT 1216 - THE A-SYSTEM HYDRAULIC FLUID DROPPED IN-FLIGHT. THE NR 2 A-HYDRAULIC PUMP WAS TURNED OFF AND THE QUANTITY WAS MAINTAINED AT THREE-FOURTHS GALLON WITH PRESSURE HOLDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN A-SYSTEM HYDR

## 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 = 'N14245' AND deregistration_id = 'N14245-1999-03-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14245-1999-03-11/reports

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