# Service difficulty reports: N18622, cancelled Feb 26, 2013

A list on [N18622, cancelled Feb 26, 2013](https://openairdocs.org/deregistered/N18622-2013-02-26.md).

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

- [SDR CALA2010110100512](https://openairdocs.org/sdr/CALA2010110100512.md): Connector · defective · Nov 1, 2010 · N18622 · Boeing 737524 · Fire Protection System Wiring
  > WHEEL WELL FIRE INDICATION CAME ON DURING CLIMBOUT. FOLLOWED QRH PROCEDURES AND RETURNED TO CLE. REMOVED AND REPLACED D WHEEL WELL DETECTOR ELEMENT M270 IAW AMM 26-17-11. REMOVED AND REPLACED D M270 DISCONNECT CONNECTOR D842 IAW 20-62-14. WHEEL WELL OVERHE
- [SDR CALA2010110100511](https://openairdocs.org/sdr/CALA2010110100511.md): Fire Warning · false activation · Nov 1, 2010 · N18622 · Boeing 737524 · Fire Detection
  > CRUISE FLT FL300 MASTER WARNING WHEEL WELL FIRE LIGHT AND BELL W/ 3 GEAR UNSAFE LIGHTS. RAN QRH LIGHTS EXTINGUISHED AFTER 3-4 MIN. LANDING NORMAL 3 GREEN ONCE GEAR EXTENDED AND LOCKED. INSPECTED CONNECTORS D4574P AND D4834P FOR CONTAMINATION /MOISTURE, NO D
- [SDR CALA2010081300389](https://openairdocs.org/sdr/CALA2010081300389.md): Skin · cracked · Aug 12, 2010 · N18622 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK, UPPER HINGE CUTOUT, FASTENER HOLE IDENTIFIED NR1 ON EA 5330-03736 FIG 4, HAS CRACK INDICATION. REPAIRED DAMAGED AREA IAW EC/RA 5330-04045. SEE L/P NR 9719567 FOR DIP FOR REPEAT INSPECTION.
- [SDR CALA2010081300388](https://openairdocs.org/sdr/CALA2010081300388.md): Frame · cracked · Aug 11, 2010 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK CRACK IN FRAME AT STA 303.9, S16L IN INSP ARE IAW FIG 7 OF EA5310-04659. LWR OTBD RADIUS OF OVAL HOLE APPROX.700 IN LONG. REPAIRED CRACK IAW ECRA 5311-01501. DIP INITIATED LP 9719570 LOG PAGE ENTERED IN DEF STATUS IN ERROR. DIP FOR THIS L/P WAS
- [SDR CALA2010080900380](https://openairdocs.org/sdr/CALA2010080900380.md): Hinge Fitting · cracked · Aug 5, 2010 · N18622 · Boeing 737524 · Fuselage, Door Hinge
  > SUPPORT TASK, L1 CUTOUT, UPPER HINGE FITTING HAVE A.25 INCH CRACK. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-40-02.
- [SDR CALA2010080300373](https://openairdocs.org/sdr/CALA2010080300373.md): Hinge Fitting · cracked · Aug 2, 2010 · N18622 · Boeing 737524 · Fuselage, Door Hinge
  > L-1 CUTOUT, LOWER HINGE FITTING HAVE A.25 INCH CRACK. REMOVED AND REPLACED L-1 LOWER HINGE FITTING REF SRM 51-40-02.
- [SDR CALA2009102300648](https://openairdocs.org/sdr/CALA2009102300648.md): Oven · defective · Oct 23, 2009 · N18622 · Boeing 737524 · Buffet/Galleys
  > F/A REPORTED A STRONG ELECTRICAL SMELL COMING FROM THE VENT IN THE AFT GALLEY CEILING. TROUBLESHOOTING REVEAL, NR 3 AFT OVEN FAN MOTOR BURNING. REMOVED AND REPLACED NR 3 AFT OVEN PER M/M 25-34-00, OPS CHECKS NORMAL, OK FOR SVC. ROTABLE PARTS CHANGE WAS INDI
- [SDR CALA2009081000441](https://openairdocs.org/sdr/CALA2009081000441.md): Unknown · malfunctioned · Aug 7, 2009 · N18622 · Boeing 737524 · Fuel Storage
  > AFTER TAKEOFF, RIGHT FUEL TANK SHOWED 3,500LBS FROM 10,000LBS ON TAKEOFF. RETURNED FOR LANDING. LANDING WEIGHT 106.8LBS. FOUND UPON ARRIVAL RT WING TANK PER STICK NR 1 & INDICATOR 2,900 LBS & AMP; LEFT TANK AT 7,700 LBS. VERIFIED NO LEAKS NOTED. VERIFIED
- [SDR CALA2009022300104](https://openairdocs.org/sdr/CALA2009022300104.md): Actuator · failed · Feb 21, 2009 · N18622 · Boeing 737524 · Landing Gear Actuator
  > ON TWO CONSECUTIVE TAKEOFFS THE NOSE GEAR MADE A VERY LOUD CLUNK WHEN GEAR HANDLE RAISED. ALL INDICATIONS AND OPERATIONS NORMAL INCLUDING EXTENSION. REMOVED AND REPLACED NLG ACTUATOR AND NLG LOCK MECHANISM PER MM 32-33-21 AND 32- 33-51.
- [SDR CALA0800208](https://openairdocs.org/sdr/CALA0800208.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 867 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800207](https://openairdocs.org/sdr/CALA0800207.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 787 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800206](https://openairdocs.org/sdr/CALA0800206.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 747 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800205](https://openairdocs.org/sdr/CALA0800205.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 727B ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800204](https://openairdocs.org/sdr/CALA0800204.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 482 BETWEEN S9L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800203](https://openairdocs.org/sdr/CALA0800203.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 400 BETWEEN S8R AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800202](https://openairdocs.org/sdr/CALA0800202.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Longeron/Stringer
  > FRAME CRACKED STA 767 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800201](https://openairdocs.org/sdr/CALA0800201.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 787 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800200](https://openairdocs.org/sdr/CALA0800200.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 747 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800199](https://openairdocs.org/sdr/CALA0800199.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 440 BETWEEN S8R AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800198](https://openairdocs.org/sdr/CALA0800198.md): Frame · cracked · Mar 6, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 400 BETWEEN S8L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A.
- [SDR CALA0800195](https://openairdocs.org/sdr/CALA0800195.md): Frame · cracked · Mar 5, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED AT STA 360 BETWEEN STRINGER 8L AND 9L. TRIMMED OUT CRACKED AREA ON FRAME AND INSTALLED REPAIR DOUBLERS PER ECRA 5310-04728. REPLACED INTERCOSTAL CLIP AT STA 360 STRINGER 8L PER ECRA 5310-04728.
- [SDR CALA0800194](https://openairdocs.org/sdr/CALA0800194.md): Frame · cracked · Mar 4, 2008 · N18622 · Boeing 737524 · Fuselage Main, Frame
  > FOUND CRACK AROUND HI-LOK HOLE AT STA 188 LBL 10. FABRICATED AND INSTALLED REPAIR PER ECRA 5311-01397.
- [SDR CALA0800183](https://openairdocs.org/sdr/CALA0800183.md): Shear Tie · corroded · Feb 29, 2008 · N18622 · Boeing 737524 · Fuselage Internal Mounting Structure
  > FOUND CORROSION AT AFT CARGO COMPARTMENT SHEAR TIE AT STA 787 LBL-4. REPAIRED SHEAR TIE AT STA 787 BETWEEN STRINGER 27L AND 27R PER SRM 53-00-07.
- [SDR CALA0800178](https://openairdocs.org/sdr/CALA0800178.md): Skin · cracked · Feb 27, 2008 · N18622 · Boeing 737524 · Passenger/Crew Doors
  > L-1 DOOR INNER SKIN CRACKED AT AFT EDGE 6TH STOP FROM TOP. REPAIRED L-1 DOOR INNER SKIN PER ECRA 5210-02001.
- [SDR CALA0800177](https://openairdocs.org/sdr/CALA0800177.md): Door Frame · cracked · Feb 27, 2008 · N18622 · Boeing 737524 · Passenger/Crew Doors
  > L-1 DOOR PAN CRACKED ON AFT EDGE 6TH STOP FROM TOP. REPAIRED L-1 DOOR PAN PER ECRA 5210-02001.
- [SDR CALA0800176](https://openairdocs.org/sdr/CALA0800176.md): Door Frame · cracked · Feb 26, 2008 · N18622 · Boeing 737524 · Fuselage Main, Structure
  > FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP FITTING FOOTPRINT. REMOVED AND REPLACED FORWARD CARGO AFT FRAME PER SRM 51-40-02.
- [SDR CALA0800161](https://openairdocs.org/sdr/CALA0800161.md): Torque Tube · corroded · Feb 20, 2008 · N18622 · Boeing 737524 · Trailing Edge Flap Control System
  > RIGHT INBOARD MID FLAP BOTH I/B AND O/B TORQUE TUBES CORRODED. REMOVED AND REPLACED BOTH TORQUE TUBES PER CMM 57-53-17.
- [SDR CALA0500254](https://openairdocs.org/sdr/CALA0500254.md): Floorbeam · corroded · Aug 5, 2005 · N18622 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND THE AFT CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 986.5, LBL 48 TO RBL 48. REPAIRED IAW ECRA 5311-01234.
- [SDR CALA0500091](https://openairdocs.org/sdr/CALA0500091.md): Socket · shorted · Mar 30, 2005 · N18622 · Boeing 737524 · Central Warning
  > SMOKE WITH A BURNING ODOR BEGAN COMING FROM UNDER THE CAPTAIN'S GLARESHIELD SHORTLY AFTER TAKEOFF FROM MSY. THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CAPTAIN'S AMBER MASTER CAUTION LIGHT SOCKET SHORTED. THE SOC
- [SDR CALA0300194](https://openairdocs.org/sdr/CALA0300194.md): Skin · punctured · Apr 7, 2003 · N18622 · Boeing 737524 · Elevator, Plate/Skin
  > THE UPPER SURFACE SKIN PANEL OF THE RT ELEVATOR SUFFERED SMALL PUNCTURE DAMAGE AT APPROXIMATELY ELEVATOR STATION 105.1 WHILE AIRCRAFT WAS IN 1/4D CHECK AT HOU. THE DAMAGE WAS THROUGH ALL PLIES, BUT THERE WAS NO CORE DAMAGE. THE PUNCTURE WAS APPROXIMATELY 4.2
- [SDR CALA0300148](https://openairdocs.org/sdr/CALA0300148.md): Cable · out of rig · Mar 27, 2003 · N18622 · Boeing 737524 · Landing Gear Position and Warning
  > THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM EWR. APPROPRIATE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN GEAR AIR/GROUND SENSE TELEFLEX CABLE OUT OF ADJUSTMENT
- [SDR CALA0100089](https://openairdocs.org/sdr/CALA0100089.md): Wire · loose · Feb 1, 2001 · N18622 · Boeing 737524 · Light System Wiring
  > THE L-1 DOOR OVERHEAD EMERGENCY LIGHT FAILED TO ILLUMINATE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND NUT ON GROUND LUG AT GROUND 622 BACKED OFF AND GROUND WIRE LOOSE. REPLACED NUT AND TIGHTENED. ALSO REPLACED DAMAGED PIN ON LIGHT ASSEMBLY.
- [SDR CALA9800015](https://openairdocs.org/sdr/CALA9800015.md): Hyd Pwr Panel · inoperative · Jan 12, 1998 · N18622 · Boeing 737524 · Hydraulic System, Main
  > CREW REPORTED, LOOSING BOTH ENGINE DRIVEN HYDRAULIC PUMPS WHILE EN ROUTE. THE NR 1 AND NR 2 HYDRAULIC PUMP LOW PRESSURE LIGHTS ILLUMINATED. WHILE TRYING TO ISOLATE PROBLEM THE SYSTEM CAME BACK ON LINE. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOU
- [SDR CAL960557](https://openairdocs.org/sdr/CAL960557.md): Lever Latch Assy · out of adjust · May 5, 1996 · N18622 · Boeing 737524 · Landing Gear Selector
  > IAH - FLT 1691 - THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A GEAR RETRACTION WAS PERFORMED AND THE PROBLEM COULD NOT BE DUPLICATED. ADJUSTMENT OF TH

## 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 = 'N18622' AND deregistration_id = 'N18622-2013-02-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18622-2013-02-26/reports

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