# Service difficulty reports: N14241, cancelled Jun 15, 1999

A list on [N14241, cancelled Jun 15, 1999](https://openairdocs.org/deregistered/N14241-1999-06-15.md).

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

- [SDR CALA9801914](https://openairdocs.org/sdr/CALA9801914.md): Line · chafed · Oct 7, 1998 · N14241 · Boeing 7372C0 · Hydraulic System, Main
  > THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO EWR. THE GEAR AND FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE IN WING ROOT CHAFED ON CLAMP. THE HYDRAULIC LINE WAS REM
- [SDR CALA9801626](https://openairdocs.org/sdr/CALA9801626.md): Skin · corroded · Sep 4, 1998 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3.
- [SDR CALA9801617](https://openairdocs.org/sdr/CALA9801617.md): Skin · cracked · Sep 1, 1998 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE KEEL BEAM LOWER SKIN AT STA 727, RBL 5. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 40.
- [SDR CALA9800902](https://openairdocs.org/sdr/CALA9800902.md): Web · cracked · May 24, 1998 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN LT WHEEL WELL SHEAR WEB AT STA 727. A REPAIR WAS INSTALLED IAW DRAWING 65C29228.
- [SDR CALA9701214](https://openairdocs.org/sdr/CALA9701214.md): Skin · cracked · Jul 25, 1997 · N14241 · Boeing 7372C0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN BETWEEN STA 111.1 AND 126.6. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01369.
- [SDR CALA9701218](https://openairdocs.org/sdr/CALA9701218.md): Floorbeam · corroded · Jul 16, 1997 · N14241 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED FROM FRAME TO FRAME AT STA 986.5. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-9.
- [SDR CALA9701215](https://openairdocs.org/sdr/CALA9701215.md): Support · corroded · Jul 14, 1997 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967 TO 986, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND 51-10-2.
- [SDR CALA9701217](https://openairdocs.org/sdr/CALA9701217.md): Support · corroded · Jul 13, 1997 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312, RBL 56. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 53-10-9, FIGURE 6.
- [SDR CALA9701216](https://openairdocs.org/sdr/CALA9701216.md): Support · corroded · Jul 9, 1997 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5 TO 995. THE CORRODED SECTION WAS REMOVED, A REPAIR T-SECTION AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.
- [SDR CALA9700076](https://openairdocs.org/sdr/CALA9700076.md): Hyd Line · chafed · Jan 26, 1997 · N14241 · Boeing 7372C0 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO SHORTLY AFTER TAKEOFF. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 A-SYSTEM LOW PRESSURE LIGHT. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOU
- [SDR CALA9601643](https://openairdocs.org/sdr/CALA9601643.md): Fuel Pump · failed · Nov 14, 1996 · N14241 · Boeing 7372C0 · Engine Fuel Pump
  > THE NR 1 ENGINE FLAMED OUT WHILE CRUISING AT FL 250 EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED, LEAK CHECK WAS GOOD AND ALL PARAME
- [SDR CALA9601317](https://openairdocs.org/sdr/CALA9601317.md): Skin · cracked · Sep 15, 1996 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > THE AIRCRAFT SKIN WAS CRACKED AT C1 DOOR DURING CARGO LOADING. THE CRACK WAS LOCATED AT STA 472.4 BETWEEN STRINGER 20R AND 21R AND MEASURED 1.5 INCH LONG. A REPAIR WAS INSTALLED IAW ECRA 5330-02437.
- [SDR CALA9601105](https://openairdocs.org/sdr/CALA9601105.md): Skin · bulged · Jul 25, 1996 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9601104](https://openairdocs.org/sdr/CALA9601104.md): Floor Beam · cracked · Jul 25, 1996 · N14241 · Boeing 7372C0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER T-CHORD AT STA 675, BBL ZERO AND A 2 INCH CRACK WAS ALSO FOUND IN CHORD AT STA 685, BBL ZERO. A REPAIR AT STA 675 WAS PERFORMED IAW BOEING DRAWING 65C17173. A REPAIR ANGLE WAS INSTALLED AT STA 685 IAW ECRA 5
- [SDR CALA9601103](https://openairdocs.org/sdr/CALA9601103.md): Web · cracked · Jul 25, 1996 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB AT STA 675, BL ZERO TO LBL 1.5. THE CRACKED WEB AREA WAS REMOVED AND A NEW SECTION OF WEB WAS INSTALLED IAW ECRA 5710-01748.
- [SDR CALA9601106](https://openairdocs.org/sdr/CALA9601106.md): Battery Pack · discharged · Jul 17, 1996 · N14241 · Boeing 7372C0 · Emergency Lighting
  > INSPECTION FOUND THE R-2 DOOR SLIDE LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE LANYARD SWITCH WAS CLEANED. THE LIGHT TESTED GOOD IAW MM 33-51-0.
- [SDR CAL960382](https://openairdocs.org/sdr/CAL960382.md): Hyd Line · chafed · Mar 21, 1996 · N14241 · Boeing 7372C0 · Hydraulic System, Main
  > FLT NR 1598 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY LINE IN PYLON CHAFED THROUGH. THE LINE WAS REPLACED AND LEAK CH
- [SDR CAL951017](https://openairdocs.org/sdr/CAL951017.md): Accessory Unit · inoperative · Nov 3, 1995 · N14241 · Boeing 7372C0 · Landing Gear Position and Warning
  > ORF - FLT 1215 - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO ORF, THE NOSE GEAR INITIALLY INDICATED GREEN, THEN THE RED LIGHT ILLUMINATED AND THE GREEN LIGHT WENT OUT. THE CREW PERFORMED A MANUAL GEAR EXTENSION, BUT THE LIGHT REMAINED RED. THE GEAR WAS CON
- [SDR CAL950996](https://openairdocs.org/sdr/CAL950996.md): Air Data Comp · inoperative · Oct 30, 1995 · N14241 · Boeing 7372C0 · Air Data Computer
  > CLE - FLT 1255 - WHILE CRUISING AT FL 220 EN ROUTE FROM BDL TO CLE AND WITH AUTOPILOT ENGAGED IN 'B' MODE, THE AIRCRAFT MADE AN ABRUPT BANK TO THE RIGHT. THE AUTOPILOT WAS DISCONNECTED AND THE AIRCRAFT FLEW NORMAL FOR REMAINDER OF FLIGHT. THE 'B' AUTOPILOT W
- [SDR CAL950583](https://openairdocs.org/sdr/CAL950583.md): Skin · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND A.25 INCH CRACK IN SKIN AT FASTENER STA 727A, S10R. THE CRACKED AREA OF SKIN WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X)
- [SDR CAL950582](https://openairdocs.org/sdr/CAL950582.md): Tear Strap · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND A.50 INCH CRACK IN TEAR STRAP AT FASTENER HOLE BELOW STR 14, LT STA 727A. A TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)
- [SDR CAL950581](https://openairdocs.org/sdr/CAL950581.md): Stringer · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Longeron/Stringer
  > GSO - INSPECTION FOUND.25 INCH CRACKS AT THREE FASTENERS ON BOTTOM ROW OF STR 14R AT STA 727A. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)
- [SDR CAL950580](https://openairdocs.org/sdr/CAL950580.md): Doubler · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.25 INCH CRACK AT UPPER FORWARD FASTENER ON DOUBLER REPAIR AT BS 727A, S17L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 25, PAGE 87. (X)
- [SDR CAL950579](https://openairdocs.org/sdr/CAL950579.md): Web · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 616 AND 639L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)
- [SDR CAL950578](https://openairdocs.org/sdr/CAL950578.md): Stringer Ties · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.25 INCH CRACK IN EACH OF TWO STRINGER TIES AT STRINGERS 4L AND 4R, STATION 702. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)
- [SDR CAL950577](https://openairdocs.org/sdr/CAL950577.md): Web · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.5 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 638 AND 663L. A WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)
- [SDR CAL950576](https://openairdocs.org/sdr/CAL950576.md): Stringer Ties · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.25 INCH CRACK IN EACH OF THE STRINGER TIES AT STRINGERS 5R, 2L, 3L, AND 4L, STATION 685. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)
- [SDR CAL950575](https://openairdocs.org/sdr/CAL950575.md): Stringer Ties · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND STRINGER TIES CRACKED AT STATION 767 STRINGERS 4L AND 5L. THE CRACKS WERE.25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)
- [SDR CAL950573](https://openairdocs.org/sdr/CAL950573.md): Web · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A 2 INCH CRACK IN WEB AT BS 947 FORWARD OF R-2 DOOR. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)
- [SDR CAL950572](https://openairdocs.org/sdr/CAL950572.md): Tear Strap · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.5 INCH CRACK IN TEAR STRAP AT FASTENER HOLE RT STATION 752 BELOW STRINGER 14. A NEW TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M)
- [SDR CAL950571](https://openairdocs.org/sdr/CAL950571.md): Angle · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN RT OUTBOARD STIFFENER ANGLE AT STATION 291 TO 294. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-0. (M)
- [SDR CAL950570](https://openairdocs.org/sdr/CAL950570.md): Stringer Ties · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND STRINGER TIES AT STATION 597 STRINGERS 5R, 4R, AND 4L CRACKED. THE CRACKS WERE.25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (M)
- [SDR CAL950569](https://openairdocs.org/sdr/CAL950569.md): Frame · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.75 INCH CRACK THROUGH INBOARD CHORD AND WEB OF STATION 639 FRAME AT STRINGER 16R. A NEW CHORD AND WEB WERE INSTALLED PER BOEING DRAWING 65C31658. (M)
- [SDR CAL950568](https://openairdocs.org/sdr/CAL950568.md): Skin · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE SKIN ON RIGHT SIDE AT STATION 727 BELOW S18. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING 65C28086 AND SERVICE BULLETIN 737-53-1077. (M)
- [SDR CAL950565](https://openairdocs.org/sdr/CAL950565.md): Skin · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND A.5 INCH CRACK IN LEFT FORWARD ENTRY DOOR LOWER FRAME SKIN. THE SKIN WAS REPAIRED IAW ECRA 5330-02294 AND BAC DRAWING 65C27257. (M)
- [SDR CAL950564](https://openairdocs.org/sdr/CAL950564.md): Rib · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Horizontal Stabilizer, Spar/Rib
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN INBOARD SIDE NR 5 RIB FROM THE FRONT OF THE LEFT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 55-10-4, AND 51-10-1. (M)
- [SDR CAL950562](https://openairdocs.org/sdr/CAL950562.md): Intercostal · corroded · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND CORROSION ON INTERCOSTAL FLANGE AT STATION 847-867 BELOW STRINGER 24. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (M)
- [SDR CAL950561](https://openairdocs.org/sdr/CAL950561.md): Floor Support · corroded · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN CABIN FLOOR SUPPORT AND ANGLE AT BS 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)
- [SDR CAL950560](https://openairdocs.org/sdr/CAL950560.md): Support · corroded · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND CORROSION ON FLOOR SUPPORT PANEL ABOVE S25L BETWEEN BS 887 AND BS 907. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)
- [SDR CAL950559](https://openairdocs.org/sdr/CAL950559.md): Frame · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.5 INCH CRACK IN FRAME AT BS 400 BETWEEN S20L AND S21L. A NEW FRAME AND FASTENERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C25113-A AND SRM 51-30-2. (M)
- [SDR CAL950558](https://openairdocs.org/sdr/CAL950558.md): Frame · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.5 INCH CRACK IN FRAME AT BS 420 BETWEEN S20L AND S21L AND A.5 INCH CRACK IN FRAME AT BS 420 S22L. REPAIR WAS INSTALLED IAW BOEING DRAWING 65C25113A AND SRM 51-30-2. (M)
- [SDR CAL950557](https://openairdocs.org/sdr/CAL950557.md): Stringer · corroded · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Longeron/Stringer
  > GSO - INSPECTION FOUND STRINGER 22R CORRODED AT BS 355. A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-30-2. (M)
- [SDR CAL950556](https://openairdocs.org/sdr/CAL950556.md): Frame · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN FRAME AT BS 500. A NEW FRAME AND FASTENERS WERE INSTALLED IAW B737 DRAWING 65C25113-A AND SRM 51-30-2. (M)
- [SDR CAL950555](https://openairdocs.org/sdr/CAL950555.md): Frame · cracked · Jun 30, 1995 · N14241 · Boeing 7372C0 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND THE FRAME AT BS 460 CRACKED BETWEEN S22L AND S21L AND BETWEEN S21L AND S20L. BOTH CRACKS WERE.5 INCH LONG. A NEW FRAME AND SPLICE WERE INSTALLED IAW B737 DRAWING 65C25113-7. (M)

## 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 = 'N14241' AND deregistration_id = 'N14241-1999-06-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14241-1999-06-15/reports

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