# Service difficulty reports: N14629, cancelled Oct 3, 2014

A list on [N14629, cancelled Oct 3, 2014](https://openairdocs.org/deregistered/N14629-2014-10-03.md).

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

- [SDR CALA2012051400346](https://openairdocs.org/sdr/CALA2012051400346.md): Control Lever · failed · May 13, 2012 · N14629 · Boeing 737524 · Landing Gear Selector
  > ABOUT 400 FT FROM TOUCHDOWN, GEAR UNSAGE LIGHT CAME ON AND GPWS " TO LOW GEAR" ANNOUNCED WENT AROUND GEAR RETRACTED NORMALLY AND EXTENDED NORMALLY ON 2ND LANDING REF TO N/R 4572410 FOR REPLACEMENT OF LANDING CONTROL LEVER IAW MM-32-31-11. SWUNG GEAR SEVERAL T
- [SDR CALA2012042500296](https://openairdocs.org/sdr/CALA2012042500296.md): Iru · failed · Apr 24, 2012 · N14629 · Boeing 737524 · Navigation System
  > AT ROTATION CAPTS EADI PITCH & AMP; ROLL FLAGS APPEARED. F/O EADI WENT BLANK. RT IRS FAULT LIGHT ILLUMINATED. TAXI IN CAPTS COMPARITOR LIGHT ILLUMINATED. SEE NR 4537211 & AMP; 4537213 FOR C/A. ALSO, PERFORMED LAND VERIFY IAW MM 22-03-10 & AMP; GMM 05-35-40.
- [SDR CALA2012041800272](https://openairdocs.org/sdr/CALA2012041800272.md): Wire Harness · defective · Apr 18, 2012 · N14629 · Boeing 737524 · Engine Indicating System Wiring
  > CLIMBING THROUGH FL 200 NR 1 EGT AND RED LIGHT SPIKED ON POWER R EDUCTION EGT WAS SWUNG FULL RANGE 0 - RED LINE BOTH DIGITAL AND ANALOG T/S TO BAD EGT HARNESS. REF TO N/R 4537204 FOR REPLACEMENT OF HARNESS ON NR 1 ENG. PERFORMED TEST NR 5 REF MM-71-00-00-7
- [SDR CALA2011110800725](https://openairdocs.org/sdr/CALA2011110800725.md): Unknown · malfunctioned · Nov 8, 2011 · N14629 · Boeing 737524 · Fuel Storage
  > AT APROXIMATELY 3000FT ON DEPARTURE THE AIRCRAFT REQUIRED SIGNIFICANT RIGHT AILERON TO HOLD WINGS LEVEL FLIGHT. A CHECK OF THE FUEL GAUGES SHOWED NR 1 TANK FULL NR 2 TANK WITH 6400 LBS, CTR TANK 4900 LBS. ALL PUMPS WERE ON XFEED (CONTINUE ON L/P 8961987). (
- [SDR CALA2011092100615](https://openairdocs.org/sdr/CALA2011092100615.md): Power Supply · inoperative · Sep 21, 2011 · N14629 · Boeing 737524 · Emergency Lighting
  > REF L/P 8870953, 8870954 AND 8870955 EMERG EXIT PATH LIGHTING ROWS 21-27 INOP. REMOVED AND REPLACED EMERG EXIT POWER SUPPLY CHARGER AT ROW 25 REF AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2011070700459](https://openairdocs.org/sdr/CALA2011070700459.md): Unknown · malfunctioned · Jul 3, 2011 · N14629 · Boeing 737524 · Landing Gear Retraction/Extension System
  > AFTER PUTTING GEAR IN DOWN POSITION 3 RED LIGHTS REMAINED ILLUMINATED. HANDLE WAS DOWN AND IN. WENT AROUND. PERFORMED QRH PROCEDURE. LANDING GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. PERFORMED MLG EXTENSION AND RETRACTION TEST REF M/M 32-32-00 NUMEROUS TI
- [SDR CALA2010121500620](https://openairdocs.org/sdr/CALA2010121500620.md): Skin · dented · Dec 15, 2010 · N14629 · Boeing 737524 · Cargo/Baggage Doors
  > SUPPORT TASK - WHEN PERFORM DMG LOG PAGE 6311298 INSP ON ABB DOOR FOUND DENT OUT OF LIMIT PER SRM 52-00-01. A/Y =18.8. LOCATED 16 IN FROM AFT EDGE AND 21 IN FROM TOP CUT OUT DAMAGED AREA, FABRICATED DOUBLER, ALODINED AND PRIMED AND INSTALLED REPAIR DOUBLER PE
- [SDR CALA2010121500617](https://openairdocs.org/sdr/CALA2010121500617.md): Hinge Fitting · cracked · Dec 14, 2010 · N14629 · Boeing 737524 · Passenger/Crew Doors
  > L-1 DOOR LOWER HINGE FITTING IS CRACKED. REMOVED AND REPLACED L-1 DOOR LOWER HINGE FITTING REF SRM 51-40-02.
- [SDR CALA2010121300615](https://openairdocs.org/sdr/CALA2010121300615.md): Crease Beam · corroded · Dec 13, 2010 · N14629 · Boeing 737524 · Fuselage Main, Structure
  > CREASE BEAM WEB HAS CORROSION STA 847LT TO 867LT. REMOVED AND REPLACED WEB AT STA 847-867 LT REF SRM 51-40-02.
- [SDR CALA2010121300611](https://openairdocs.org/sdr/CALA2010121300611.md): Frame · cracked · Dec 13, 2010 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK, FUSELAGE FRAME WEB AT STA 303.9 AND STRINGER 16LT HAS CRACKS AROUND THE OVAL HOLE. PERFORMED REPAIR AT FUSELAGE FRAME AT STA 303.9 PER EA 5310- 04659 OP 02.
- [SDR CALA2010121300610](https://openairdocs.org/sdr/CALA2010121300610.md): Intercostal · cracked · Dec 11, 2010 · N14629 · Boeing 737524 · Fuselage Miscellaneous Structure
  > E&E COMPT, INTERCOSTAL LOCATED AT LBL 10.0 AND BETWEEN FRAMES 344 AND 360 CRACKED IN TWO PLACES (MARKED) IN UPPER "L"ANGLE REMOVED &AMP. INSTALLED NEW ANGLE / SRM 51-40-02.
- [SDR CALA0800743](https://openairdocs.org/sdr/CALA0800743.md): Frame · cracked · Jul 25, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 360 S-9L. REPAIED CABIN FRAME STATION 360 S-8L TO S-9L PER ECRA5310-04808 AND CREATED A DIP FOR INTERCOSTAL CLIP ON N/R LOG 9695077, DIP 89478 PER ECRA 5310-04808 STEP 11. CREATED A SECOND DIP FOR FRAME INSPECTION ON N/R LOG 9695078 DIP
- [SDR CALA0822739](https://openairdocs.org/sdr/CALA0822739.md): Frame · cracked · Jul 23, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED AT STATION 827 S-9LT. PERFORMED INTERIM REPAIR BY REMOVING DAMAGE, PERFORMING NDT INSPECTION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ECRA 5310-04807 PART 1. INITIATED DIP 089441 TO PERFORM THE INSPECTION PER ECRA 5310-04807 PART 2 ON TH
- [SDR CALA0800701](https://openairdocs.org/sdr/CALA0800701.md): Frame · cracked · Jul 10, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 747 AT S-9L. INSTALLED REPAIR ON FRAME AT STATION 747 S-9L PER EA 5310-04498.
- [SDR CALA0800696](https://openairdocs.org/sdr/CALA0800696.md): Frame · cracked · Jul 10, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 907 AT S-9L. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2.
- [SDR CALA0800693](https://openairdocs.org/sdr/CALA0800693.md): Frame · cracked · Jul 8, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 400 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
- [SDR CALA0800692](https://openairdocs.org/sdr/CALA0800692.md): Frame · cracked · Jul 8, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 380 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
- [SDR CALA0800690](https://openairdocs.org/sdr/CALA0800690.md): Frame · cracked · Jul 8, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 867 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2.
- [SDR CALA0800689](https://openairdocs.org/sdr/CALA0800689.md): Frame · cracked · Jul 8, 2008 · N14629 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STATION 867 AT S9L. REPAIRED FRAME PER EA 5310-04498 OP2.
- [SDR CALA0600021](https://openairdocs.org/sdr/CALA0600021.md): Spar · corroded · Jan 19, 2006 · N14629 · Boeing 737524 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP CORRODED JUST O/B OF STAB STA 193.90. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5510-01826. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR PER PART 3 OF ECRA 5510-01826 WITH NO FURTHER INSPECTIONS
- [SDR CALA0300469](https://openairdocs.org/sdr/CALA0300469.md): Skin · gouged · Aug 16, 2003 · N14629 · Boeing 737524 · Elevator, Plate/Skin
  > INSPECTION FOUND SKIN UPPER SURFACE OF LT ELEVATOR GOUGED. THE SKIN WAS REPAIRED IAW ECRA 5520-01335.

## 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 = 'N14629' AND deregistration_id = 'N14629-2014-10-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14629-2014-10-03/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.