# Service difficulty reports: N44214, cancelled Feb 18, 1998

A list on [N44214, cancelled Feb 18, 1998](https://openairdocs.org/deregistered/N44214-1998-02-18.md).

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

- [SDR CALA9701680](https://openairdocs.org/sdr/CALA9701680.md): Hyd Line · leaking · Nov 26, 1997 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE FLEX LINE LEAKING. THE LINE WAS REPLACED WI
- [SDR CALA9701355](https://openairdocs.org/sdr/CALA9701355.md): Hyd Line · ruptured · Sep 12, 1997 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ILLUMINATION OF A PUMP LOW PRESSURE LIGHTS. THE A-SYSTEM HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULC PRESSURE LI
- [SDR CALA9701250](https://openairdocs.org/sdr/CALA9701250.md): Stud · failed · Aug 28, 1997 · N44214 · Boeing 737130 · Turbine Engine Accessory Drive
  > THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE ENROUTE FROM CAE TO EWR. THE ENG WAS SHUTDOWN AND THE A/C WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTTOM STUD ON NR 1
- [SDR CALA9701223](https://openairdocs.org/sdr/CALA9701223.md): Hyd Line · leaking · Aug 15, 1997 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHT WHILE AT CRUISE. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SUPPLY LINE LE
- [SDR CALA9700843](https://openairdocs.org/sdr/CALA9700843.md): Hydraulic Line · chafed · Jun 6, 1997 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO NEAR ZERO WHILE EN ROUTE. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM HYDRAULIC PRESSURE LINE ON RT WING IN ENGINE PYLON
- [SDR CALA9700071](https://openairdocs.org/sdr/CALA9700071.md): Hyd Line · leaking · Jan 20, 1997 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS FLICKERED AND THE A-SYSTEM HYRDAULIC QUANTITY GAUGE READ ZERO ON APPROACH PRIOR TO GEAR AND FLAP EXTENSION. THE HYDRAULIC FAILURE CHECKLIST WAS COMPLETED AND A MANUAL GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDE
- [SDR CALA9601911](https://openairdocs.org/sdr/CALA9601911.md): Hydraulic Line · leaking · Dec 30, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY FLEX LINE IN RIGHT ENGINE PYLON AREA LEAKING. THE LINE WAS REMOVED AND REPLACED AND LEAK CHE
- [SDR CALA9601876](https://openairdocs.org/sdr/CALA9601876.md): Hyd Line · leaking · Dec 24, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > THE A HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT INTO EWR. THE A SYSTEM PUMPS WERE TURNED OFF AND THE HYDRAULIC LOSS CHECKLIST WAS ACCOMPLISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT ENGINE A SYSTEM PRESSURE LI
- [SDR CALA9601603](https://openairdocs.org/sdr/CALA9601603.md): Skin · cracked · Nov 4, 1996 · N44214 · Boeing 737130 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF C-2 DOOR AFT CUTOUT. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLERS WERE INSTALLED IAW ECRA 5330-02460.
- [SDR CALA9601561](https://openairdocs.org/sdr/CALA9601561.md): Bulkhead Skin · cracked · Nov 1, 1996 · N44214 · Boeing 737130 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-11.
- [SDR CALA9601560](https://openairdocs.org/sdr/CALA9601560.md): Shear Web · cracked · Nov 1, 1996 · N44214 · Boeing 737130 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN INBOARD RADIUS OF SHEAR WEB AT S18A, LT B.S. 664. NEW REPAIR ANGLES WERE INSTALLED IAW BOEING DRAWING NR 65C29228 AND SRM 51-30-2.
- [SDR CALA9601555](https://openairdocs.org/sdr/CALA9601555.md): Skin · cracked · Oct 31, 1996 · N44214 · Boeing 737130 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN INBOARD SKIN AT LOWER AFT CORNER OF C-2 DOOR CUTOUT. THE CRACKED SECTION OF SKIN WAS REMOVED. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND ENGINEERING ORDER REO-02348.
- [SDR CALA9601554](https://openairdocs.org/sdr/CALA9601554.md): Bulkhead Skin · cracked · Oct 31, 1996 · N44214 · Boeing 737130 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2.
- [SDR CALA9601553](https://openairdocs.org/sdr/CALA9601553.md): Bulkhead Skin · cracked · Oct 31, 1996 · N44214 · Boeing 737130 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFENER AT WL 218, RT SIDE. THE CRACKED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2
- [SDR CALA9601556](https://openairdocs.org/sdr/CALA9601556.md): Frame · cracked · Oct 30, 1996 · N44214 · Boeing 737130 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE AT LOWER AFT CORNER OF LT STA 520 WING TO BODY ATTACH FRAME. THE FASTENERS AND EXISTING ANGLE WERE REMOVED. AN ATTACH ANGLE, REPAIR ANGLE, AND CLIPS WERE FABRICATED AND INSTALLED IAW ECRA 5350-01227, SRM
- [SDR CAL960560](https://openairdocs.org/sdr/CAL960560.md): Hydraulic Line · chafed · May 6, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > EWR - FLT 0674 - THE B-HYDRAULIC SYSTEM LOW QUANTITY ILLUMINATED ON APPROACH TO DWR. THE 'A' AND 'B' SYSTEMS REMAINED AT 3,000 PSI WITH 2 GALLONS QUANTITY. THE GEAR AND FLAPS EXTENDED NORMALLY. THE QUANTITY WENT TO 1 GALLON WITH T/R ACTIVATED AND RETURNED T
- [SDR CAL960386](https://openairdocs.org/sdr/CAL960386.md): Hyd Line · leaking · Mar 24, 1996 · N44214 · Boeing 737130 · Passenger/Crew Doors
  > BUF - FLT 1420 - AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM EWR TO BUF. THE AIRCRAFT LANDED IN BUF WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT SYSTEM 'A' MODULAR UNIT LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLA
- [SDR CAL960185](https://openairdocs.org/sdr/CAL960185.md): Hyd Line · chafed · Feb 22, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > FLT NR 1036 - GSO - THE 'A' HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM BNA TO EWR. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE IN L
- [SDR CAL960067](https://openairdocs.org/sdr/CAL960067.md): Hyd Line · leaking · Jan 30, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > FLT NR 1069 - TPA - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE IN FLIGHT WITH THE QUANTITY GAUGE INDICATING ZERO. THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO 'A' HYDRAULIC SYSTEM PRESSURE MODULE LEAKING. THE LINE WAS REPLACED US
- [SDR CAL960062](https://openairdocs.org/sdr/CAL960062.md): Hyd Line · chafed · Jan 24, 1996 · N44214 · Boeing 737130 · Hydraulic System, Main
  > FLT NR 1069 - TPA - AIRCRAFT LOST THE 'A' SYSTEM HYDRAULICS WHILE EN ROUTE FROM GSO TO TPA. QRH CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM HYDRAULIC PRESSURE LINE ABOVE LEFT MLG CHAFED
- [SDR CAL951157](https://openairdocs.org/sdr/CAL951157.md): Tee Chord · cracked · Dec 15, 1995 · N44214 · Boeing 737130 · Wing Miscellaneous Structure
  > GSO - INSPECTION FOUND A 2 INCH CRACK IN TEE CHORD AT STA 685, BL ZERO. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5710-01705. (X)
- [SDR CAL950440](https://openairdocs.org/sdr/CAL950440.md): Lap Seam · corroded · May 11, 1995 · N44214 · Boeing 737130 · Fuselage Miscellaneous Structure
  > 31J - INSPECTION FOUND CORROSION IN THE LAP SEAM AT BS 420, STR 27R. THE CORRODED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-03. (X)
- [SDR CAL950437](https://openairdocs.org/sdr/CAL950437.md): Fitting · cracked · May 9, 1995 · N44214 · Boeing 737130 · Fuselage Miscellaneous Structure
  > 31J - INSPECTION FOUND A.3750 INCH CRACK IN THE RT BS 695 FRAME AFT LOWER FITTING AT THE OUTBOARD FASTENERS IN THE AFT HORIZONTAL FLANGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SB 737-53-1080, REV. 2 AND BOEING DRAWING 65C34490. (X)
- [SDR CAL950439](https://openairdocs.org/sdr/CAL950439.md): Shear Beam · cracked · May 8, 1995 · N44214 · Boeing 737130 · Fuselage Miscellaneous Structure
  > 3LJ - A.3750 INCH CRACK WAS FOUND IN THE RADIUS OF THE INBOARD FLANGE AT THE FORWARD END OF THE LT S18A SHEAR BEAM, AFT SIDE OF BS 664 BULKHEAD. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-40-3, SRM 51-10-2, SRM
- [SDR CAL950438](https://openairdocs.org/sdr/CAL950438.md): Frame · cracked · May 8, 1995 · N44214 · Boeing 737130 · Passenger/Crew Doors
  > 31J - A 1 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF THE L-2 DOOR FRAME. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5210-01224. (X)
- [SDR CAL950101](https://openairdocs.org/sdr/CAL950101.md): Battery Charger · inoperative · Feb 8, 1995 · N44214 · Boeing 737130 · Battery/Charger System
  > TPA - FLT 1790 - THE FLIGHT ATTENDANT REPORTED A SMOKY ODOR IN CABIN DURING CLIMB-OUT. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE ODOR SUBSIDED. THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BATTERY CHA
- [SDR CAL950001](https://openairdocs.org/sdr/CAL950001.md): Hyd Line · chafed · Jan 1, 1995 · N44214 · Boeing 737130 · Hydraulic System, Main
  > FLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A' SYSTEM LOW PRESSURE LIGHTS BEGAN TO FLICKER ON AND OFF WHILE ON FINAL APPROACH. THE AIRCRAFT LA

## 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 = 'N44214' AND deregistration_id = 'N44214-1998-02-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N44214-1998-02-18/reports

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