# Service difficulty reports: N77215, cancelled Mar 11, 1998

A list on [N77215, cancelled Mar 11, 1998](https://openairdocs.org/deregistered/N77215-1998-03-11.md).

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

- [SDR CALA9701432](https://openairdocs.org/sdr/CALA9701432.md): Slide · low pressure · Oct 11, 1997 · N77215 · Boeing 737130 · Escape Slide
  > L-1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH MM 25-61-311.
- [SDR CALA9700860](https://openairdocs.org/sdr/CALA9700860.md): Skin · dented · May 20, 1997 · N77215 · Boeing 737130 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 360, STRINGER 17L. THE DENTED SECTION OF SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 28 AND ECRA 5330-02523.
- [SDR CALA9601542](https://openairdocs.org/sdr/CALA9601542.md): Hyd Line · leaking · Oct 31, 1996 · N77215 · Boeing 737130 · Hydraulic System, Main
  > THE A-HYDRAULIC SYSTEM QUANTITY GRADUALLY DECREASED TO 1 GALLON WHILE EN ROUTE. THE A-SYSTEM HYDRAULIC PUMPS WERE TURNED OFF. WHEN THE PUMPS WERE TURNED ON TO LOWER FLAPS THE SYSTEM FAILED AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED AT EWR WITHOUT INCI
- [SDR CALA9601447](https://openairdocs.org/sdr/CALA9601447.md): Line · leaking · Oct 12, 1996 · N77215 · Boeing 737130 · Hydraulic System, Main
  > LOSS OF A-SYSTEM HYDRAULICS. FOUND PRESSURE LINE FROM NR 2 ENGINE LEAKING. REPLACED LINE AND BOTH ENGINE DRIVEN AND ELECTRIC HYDRAULIC PUMPS AND REPLACED ALL FILTERS PER MM 29-11-32 AND 29-12-21.
- [SDR CALA9601325](https://openairdocs.org/sdr/CALA9601325.md): Air Dist Fan · inoperative · Sep 23, 1996 · N77215 · Boeing 737130 · Air Distribution Fan
  > A STRONG ELECTRICAL ODOR WAS SMELLED IN THE COCKPIT AFTER TAKEOFF. THE FLIGHT ATTENDANT'S REPORTED SMOKE IN THE AFT/MID CABIN. THE AIR DISTRIBUTION FAN WAS TURNED OFF AND THE SMOKE APPEARED TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO IAD WHERE IT LANDED WITH
- [SDR CALA960491](https://openairdocs.org/sdr/CALA960491.md): Battery · discharged · Apr 15, 1996 · N77215 · Boeing 737130 · Emergency Lighting
  > GSO - THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE RIGHT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X
- [SDR CAL960492](https://openairdocs.org/sdr/CAL960492.md): Battery · discharged · Apr 15, 1996 · N77215 · Boeing 737130 · Emergency Lighting
  > GSO - THE LEFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE LEFT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X)
- [SDR CAL960485](https://openairdocs.org/sdr/CAL960485.md): Chord · cracked · Mar 27, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND LT OUTBOARD CHORD CRACKED PAST SECOND FASTENER HOLE AT STA 727. THE CHORD SEGMENT WAS REMOVED AND RPELACED IAW BOEING DRAWING 65C33722. (X)
- [SDR CAL960484](https://openairdocs.org/sdr/CAL960484.md): Floor Beam · cracked · Mar 25, 1996 · N77215 · Boeing 737130 · Fuselage Main, Floor Beam
  > GSO - INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FLOOR BEAM LOWER T-CHORD AT BBL ZERO, STA 675. THE FLOOR BEAM CHORD WAS REPAIRED IAW ECRA 5710-01462 AND BOEING DRAWINGS 65C19643, 65C17173, ND 65C17103. (X)
- [SDR CAL960483](https://openairdocs.org/sdr/CAL960483.md): Skin · delaminated · Mar 25, 1996 · N77215 · Boeing 737130 · Ailerons
  > GSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-6, SRM 51-10-2, AND SRM 51-20-21. (X)
- [SDR CAL960487](https://openairdocs.org/sdr/CAL960487.md): Skin · corroded · Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/Skin
  > GSO - INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 259 TO STA 306, STR 24L TO STR 27L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A NEW SECTION OF SKIN AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (X)
- [SDR CAL960486](https://openairdocs.org/sdr/CAL960486.md): Stringer · corroded · Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Longeron/Stringer
  > GSO - INSPECTION FOUND STR 21R AND SKIN PANEL CORRODED AT STA 294.5. THE STRINGER AND SKIN PANEL WERE REMOVED. A NEW STRINGER, SKIN SECTION, AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-4. (X)
- [SDR CAL960489](https://openairdocs.org/sdr/CAL960489.md): Skin · delaminated · Mar 21, 1996 · N77215 · Boeing 737130 · Rudder, Plate/Skin
  > GSO - INSPECTION FOUND UPPER AFT TRAILING EDGE SECTION OF RUDDER DELAMINATING. THE LENGTH OF DELAMINATION WAS APPROXIMATELY 12 INCHES. THE DELAMINATED SECTION OF RUDDER WAS REMOVED. A NEW CORE SECTION AND SKIN PLIES WERE FABRICATED AND BONDED IAW SRM 51-40-
- [SDR CAL960488](https://openairdocs.org/sdr/CAL960488.md): Chord · corroded · Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND LOWER CHORD CORRODED AT LEFT AND RIGHT ENDS ON UPPER AND LOWER SURFACES OF HORIZONTAL FLANGE, STA 294.5. THE CORRODED CHORD SEGMENT WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW SRM 51-30-2, SRM 51-30-5, AND SRM 51-10-2. (X)
- [SDR CAL960482](https://openairdocs.org/sdr/CAL960482.md): Skin · cracked · Mar 21, 1996 · N77215 · Boeing 737130 · Wing, Plate/Skin
  > GSO - INSPECTION FOUND A 0.3 INCH CRACK IN RT WING LEADING EDGE SKIN ON OUTBOARD EDGE OF OUTBOARD SLAT TRACK CUT-OUT, WBL 304. THE CRACK WAS ROUTED OUT IAW ECRA 5720-01512. (X)
- [SDR CAL960481](https://openairdocs.org/sdr/CAL960481.md): Angle · cracked · Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESSURE PANEL AT BS 663.75. BOTH ANGLES WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-10-2. (X)
- [SDR CAL960480](https://openairdocs.org/sdr/CAL960480.md): Skin · cracked · Mar 4, 1996 · N77215 · Boeing 737130 · Wing, Plate/Skin
  > GSO - INSPECTION FOUND A 1 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT NR 2 SLAT AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, SR 51-10-2, AND SRM 51-30-2. (X)
- [SDR CAL960490](https://openairdocs.org/sdr/CAL960490.md): Frame · cracked · Mar 3, 1996 · N77215 · Boeing 737130 · Cargo/Baggage Doors
  > GSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME. THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED WEB WAS CUT OUT. REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND SRM 51-30-2. (X)
- [SDR CAL960152](https://openairdocs.org/sdr/CAL960152.md): Hyd Line · leaking · Feb 14, 1996 · N77215 · Boeing 737130 · Hydraulic System, Main
  > FLT NR 1446 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE LEAKING AT CLAMP. THE PRESSURE LINE WAS R
- [SDR CAL950519](https://openairdocs.org/sdr/CAL950519.md): T-Angle · corroded · Jun 5, 1995 · N77215 · Boeing 737130 · Fuselage Miscellaneous Structure
  > 31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X)
- [SDR CAL950518](https://openairdocs.org/sdr/CAL950518.md): Pressure Panel · corroded · Jun 1, 1995 · N77215 · Boeing 737130 · Fuselage Miscellaneous Structure
  > 31J - THE NOSE WHEEL WELL PRESSURE BULKHEAD WAS FOUND WITH A CORROSION BULGE 1 INCH IN DIAMETER, AT THE AFT FORWARD OUTBOARD CORNER OF THE LEFT ACCESS PANEL BETWEEN THE SKIN AND INVERTED 'T'. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03128, REV IR. (M)
- [SDR CAL950241](https://openairdocs.org/sdr/CAL950241.md): Hydraulic Line · chafed · Mar 30, 1995 · N77215 · Boeing 737130 · Hydraulic System, Main
  > EWR - FLT 1204 - THE B-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE TO EWR. THE A-SYSTEM QUANTITY GAUGE DECREASED TO ONE GALLON. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A B-SYSTEM HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE 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 = 'N77215' AND deregistration_id = 'N77215-1998-03-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N77215-1998-03-11/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.