# Service difficulty reports: N58606, cancelled Jan 2, 2013

A list on [N58606, cancelled Jan 2, 2013](https://openairdocs.org/deregistered/N58606-2013-01-02.md).

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

- [SDR CALA2012101800681](https://openairdocs.org/sdr/CALA2012101800681.md): Pcu · leaking · Oct 18, 2012 · N58606 · Boeing 737524 · Aileron Control System
  > DURING CRUSE ENG 1 A HYD PUMP LOW PRESS LIGHT ILLUMINATED. FOLLOWED BY GRADUAL DEPLETION OF SYS A HYD. FLUID LEVEL, FOLLOWED B Y ELECT HYD A PUMP, PUMP LOW PRESSURE LIGHT. FOUND A SYS LOWER AILERON PCU LEAKING REMOVED & REPLACED SYS A AILERON PCU IN REF TO A
- [SDR CALA2012010600013](https://openairdocs.org/sdr/CALA2012010600013.md): Warning System · false activation · Jan 6, 2012 · N58606 · Boeing 737524 · Landing Gear Position and Warning
  > DURING CLIMBOUT, AFTER LANDING GEAR LEVER TO NEUTRAL LEFT GEAR MAIN INDICATED GREEN AND RED, RIGHT GEAR INDICATED GREEN. REFERENCE T/S 32-61-00-101, C/W MAIN GEAR PROX SENSOR RESISTANC E CHECKS, CHECK OF E-11 SHELF FOR MOISTURE CONTAMINATION AND TEST OF THE L
- [SDR CALA2011032900214](https://openairdocs.org/sdr/CALA2011032900214.md): Frame · cracked · Dec 4, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > BS 303.9 FRAME CRACKED AT STR 16L FORWARD SIDE AROUND OVAL HOLE. INSTALLED REPAIR PER ECRA 5311-01515. GENERATED DIP TO REINSPECT BEFORE THE ACCUMULATION OF 66000 TOTAL A/C FLY CYCLES PER PART 2 OF ECRA 5311-01515 REF DIP 08205 FRAME CRACKED STA 303.9 PER E
- [SDR CALA2010120100600](https://openairdocs.org/sdr/CALA2010120100600.md): Skin · cracked · Dec 1, 2010 · N58606 · Boeing 737524 · Fuselage Main, Plate/Skin
  > CRACK INDICATION FOUND AT FWD ENTRY DOOR UPPER HINGE CUTOUT AFT FASTENER HOLE 4TH FROM TOP, REF EA 5330-03736 REV B, STEP 14, INSTALLED REPAIR IAW ECRA 5330-04091.
- [SDR CALA2010120100599](https://openairdocs.org/sdr/CALA2010120100599.md): Skin · worn · Dec 1, 2010 · N58606 · Boeing 737524 · Trailing Edge Flaps
  > SUPPORT TASK - RT OTBD MIDFLAP, INBD L/E WORN. MARKED, TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW E CRA 5752-01496.
- [SDR CALA2010120100597](https://openairdocs.org/sdr/CALA2010120100597.md): Beltframe · cracked · Nov 29, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK BELTFRAME STA 706 HAS CRACK INDICATION BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) AREA PER MID-FREQ EDDY CURRENT INSPECTION (MFEC). REPAIRED FRAME STA 706-R, PER EC/RA 5311-01514 AND E
- [SDR CALA2011031500140](https://openairdocs.org/sdr/CALA2011031500140.md): Support Fitting · corroded · Nov 24, 2010 · N58606 · Boeing 737524 · Trailing Edge Flaps
  > SUPPORT TASK LT WING NR 2 FLAP TRACK MOUNT HOLES SPOT FACE HAS SURFACE CORROSION UPPER SIDE. REMOVED AND REPLACED FLAP TRACK SUPPORT FITTING REF BOEING DWG 65C80736, SOPM 20-50-19, AND SRM 51-40-02.
- [SDR CALA2010112400596](https://openairdocs.org/sdr/CALA2010112400596.md): Skin · dented · Nov 24, 2010 · N58606 · Boeing 737524 · Cargo/Baggage Doors
  > SUPPORT TASK: WHEN PERFORMED DMG LOG 9593545 INSP ON A/B/B DOOR FOUND DENT AT 15 INCHES FROM TOP AND 14 INCHES FROM FWD EDGE OUT OF LIMITS PER SRM 52-00-01. A=1.6 Y=.063 A/Y=25 LESS THAN MIN LIMIT 30 CUT OUT SECTION OF DAMAGE AND INSTALLED DOUBLER REF SRM 52-
- [SDR CALA2010112200595](https://openairdocs.org/sdr/CALA2010112200595.md): Hinge Fitting · cracked · Nov 22, 2010 · N58606 · Boeing 737524 · Fuselage, Door Hinge
  > L-1 DOOR LOWER HINGE FITTING CRACK INDICATION. INSTALLED NEW LOWER HINGE FITTING SRM 51-40-02, AFTER DISCOVERY LOWER HINGE FITTING WAS CRACKED.
- [SDR CALA2010112200594](https://openairdocs.org/sdr/CALA2010112200594.md): Hinge Fitting · cracked · Nov 22, 2010 · N58606 · Boeing 737524 · Fuselage, Door Hinge
  > L-1 DOOR UPPER HINGE FITTING CRACK INDICATION. INSTALLED NEW UPPER HINGE FITTING / SRM 51-40-02, AFTER DISCOVERY UPPER HINGE FITTING WAS CRACKED.
- [SDR CALA2010112200591](https://openairdocs.org/sdr/CALA2010112200591.md): Shear Tie · cracked · Nov 19, 2010 · N58606 · Boeing 737524 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED STA 967 AT S4L CABIN CTN 53-304-108. REMOVED AND REPLACED SHEAR TIE REF SRM 51-40-02 AND BOEING DWG 65-46563.
- [SDR CALA2010111900589](https://openairdocs.org/sdr/CALA2010111900589.md): Attach Fitting · cracked · Nov 19, 2010 · N58606 · Boeing 737524 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - BS 360L STR 11L, CRACK ON ATTACH CLIP. REMOVED CLIP, INSPECTED HOLES IN AREA AND INSTALLED NEW CLIP PER ECRA 5311-01513.
- [SDR CALA2010111900588](https://openairdocs.org/sdr/CALA2010111900588.md): Beltframe · cracked · Nov 19, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELFRAME STA 827 HAS CRACK AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED FRAME-REF-EC/RA 5311-01512,DIP PER EA-5310-04498 STEP 35 TO PERFORM A ONE TIME INSPECTION.
- [SDR CALA2010111900587](https://openairdocs.org/sdr/CALA2010111900587.md): Skin · cracked · Nov 19, 2010 · N58606 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK - RIVET HOLE STA 420 BETWEEN S-17 AND S-17 SHOWS CRACK INDICATION ON HFEC HOLE PROBE INSP REF NDT PT 6 51-00-00 FIG 16. REMOVED RIVET, REPAIRED SKIN PER SRM 53-00-01 FIG 201 SECTION 2 REPAIR 19, REMOVED AND REPLACED SHEAR TIE.
- [SDR CALA2011031500139](https://openairdocs.org/sdr/CALA2011031500139.md): Flap Track · corroded · Nov 17, 2010 · N58606 · Boeing 737524 · Trailing Edge Flaps
  > RT WING NR 7 FLAP TRACK AFT ATTACH POINT EMITTING RUST. CORRECTED 11/10/2010 HOU 66274 INSTALLED NEW SERVICEABLE NR 7 FLAP TRACK; REF AMM 27-51-49-404-006. ROTABLE PARTS CHANGE WAS INDICATED - TT 1441858 S/N OFF 01606 TRACK, FLAP, O/B OFF 24-5753-9-9001 1606
- [SDR CALA2010111500541](https://openairdocs.org/sdr/CALA2010111500541.md): Frame · cracked · Nov 15, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > MAIN FRAME CRACKED AT STA 616 JUST BELOW FLOOR DECK LT SIDE. COMPLETED REPAIR OF STA 616 FRAME REF EC/RA 5311-01158.
- [SDR CALA2010111500540](https://openairdocs.org/sdr/CALA2010111500540.md): Frame · cracked · Nov 15, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > MAIN FRAME CRACKED STA 616 RT JUST BELOW MAIN DECK FLOOR. COMPLETED REPAIR FRAME STA 616R REF EC/RA 5311-01158.
- [SDR CALA2010111000534](https://openairdocs.org/sdr/CALA2010111000534.md): Beltframe · cracked · Nov 10, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME STA. 747 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLES A & B REF EA 5310-04498.
- [SDR CALA2010110900533](https://openairdocs.org/sdr/CALA2010110900533.md): Beltframe · cracked · Nov 9, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME STA 360, CRACKED AT FASTENERS HOLE BETWEEN STR 8L & 9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLE A & B AND INSTALLED NEW CLIP PER EC/RA 5311-01511.
- [SDR CALA2010110900532](https://openairdocs.org/sdr/CALA2010110900532.md): Beltframe · cracked · Nov 8, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME AT STA 727B HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED FRAME AT STA727B BETWEEN STRINGERS 8L AND 9L PER EA 5310-04498 OP2.
- [SDR CALA2010110900531](https://openairdocs.org/sdr/CALA2010110900531.md): Beltframe · cracked · Nov 8, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. REPAIRED BELTFRAME STA 867 STRINGERS 8L-9L REF EA 5310-04498.
- [SDR CALA2010110800528](https://openairdocs.org/sdr/CALA2010110800528.md): Beltframe · cracked · Nov 8, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME STA 440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8L AND S9L AT THE A/C OUTLET SUPPORT BRACKET ATTACHMENT AREA (ALL WORK ACCOMPLISHED ON FORMS 44.008 AND 43.0150). REMOVED DAMAGED FRAME SECTION INSTALLED REPAIR DOUBLERS REF EA 5
- [SDR CALA2010110800527](https://openairdocs.org/sdr/CALA2010110800527.md): Beltframe · cracked · Nov 8, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - BELTFRAME STA 400 CRACKED AT FASTENER HOLE BETWEEN STR 8L & 9L AT A/C OUTLET EXTRUSION SUPPORT BRACKET ATTACHMENT AREA. INSTALLED REPAIR ANGLE A & B REF EA 5310-04498 OP.02.
- [SDR CALA2010110800526](https://openairdocs.org/sdr/CALA2010110800526.md): Beltframe · cracked · Nov 8, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK. BELTFRAME STA 400 CRACK INDICATION BETWEEN STR 8R AND 9R AT A/C OULET EXTRUSION SUPPORT BRACKET ATTACHMENT (RIVET BUCKED TAIL) AREA PER MID-FREQ EDDY CURRENT INSPECTION (MFEC). INSTALLED REPAIR ANGLE A & B REF EA 5310-04498 OP2.
- [SDR CALA2010110800525](https://openairdocs.org/sdr/CALA2010110800525.md): Beltframe · cracked · Nov 7, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK BELTFRAME STA 380 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET SUPPORT BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 380 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.
- [SDR CALA2010110800524](https://openairdocs.org/sdr/CALA2010110800524.md): Beltframe · cracked · Nov 7, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK BELTFRAME STA 867 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT A/C OUTLET EXTRUSION BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 867 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.
- [SDR CALA2010110800523](https://openairdocs.org/sdr/CALA2010110800523.md): Beltframe · cracked · Nov 7, 2010 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK BELTFRAME STA440 HAS CRACKED AT FASTENER HOLE BETWEEN STRINGERS S8R AND S9R AT THE A/C OUTLET EXTRUSION SUPPORT BRACKET DAMAGED AREA REMOVED FROM FRAME AT STA 440 B/W STR S8R AND S9R. AREA REPAIRED PER EA 5310-04498 OP2.
- [SDR CALA2010110800522](https://openairdocs.org/sdr/CALA2010110800522.md): Intercostal · cracked · Nov 6, 2010 · N58606 · Boeing 737524 · Fuselage Miscellaneous Structure
  > FWD ENTRY BETWEEN STA 344 - 360 BL-0 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL, ALL HOLES DRILLED AS NEEDED REF SRM 51-40-02 & 51-40-05.
- [SDR CALA0700252](https://openairdocs.org/sdr/CALA0700252.md): Frame · cracked · May 16, 2007 · N58606 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 400, S17R TO S28R. A NEW FRAME WAS INSTALLED IAW SRM 51-10-02 AND 51-40-00.
- [SDR CALA0500453](https://openairdocs.org/sdr/CALA0500453.md): Slide · low · Dec 25, 2005 · N58606 · Boeing 737524 · Escape Slide
  > THE L-2 DOOR SLIDE WAS FOUND WITH LOW PRESSURE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.
- [SDR CALA0300528](https://openairdocs.org/sdr/CALA0300528.md): Fire Detector · inoperative · Sep 13, 2003 · N58606 · Boeing 737524 · Fire Detection
  > THE APU FIRE DETECTION LIGHT ILLUMINATED WHILE ENROUTE FROM PHL TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE WARNING LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. TH
- [SDR CALA0000583](https://openairdocs.org/sdr/CALA0000583.md): Engine · leaking · Apr 28, 2000 · N58606 · Boeing 737524 · Turbine Engine Oil System
  > ON TAKE-OFF AND LANDING WITH THROTTLES ADVANCED COCKPIT AND CABIN HAS STRONG UNPLEASANT ODOR. REMOVED AND REPLACED ENGINE DUE TO OIL LEAK PER MM 71-00-00.
- [SDR CALA0000437](https://openairdocs.org/sdr/CALA0000437.md): Access Door · worn · Apr 7, 2000 · N58606 · Boeing 737524 · Wing, Plate/Skin
  > INSPECTION FOUND LEFT WING TANK NR 1 FUEL BOOST PUMP ACCESS PANEL UNSECURABLE DUE TO WORN SPOTS ON LOWER WING SKIN AT WBL 146. REPAIRED AREA IAW ECRA 5720-01793.
- [SDR CALA0000436](https://openairdocs.org/sdr/CALA0000436.md): Skin · dented · Apr 7, 2000 · N58606 · Boeing 737524 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN LAP DENTED AT STA 967, STRINGER 26L. REPAIRED IAW ECRA 5360-01039.
- [SDR CALA0000364](https://openairdocs.org/sdr/CALA0000364.md): Angle · corroded · Mar 28, 2000 · N58606 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR R-1 DOOR THRESHOLD Z-ANGLE ATTACH CHORD CORRODED AT STA 294 - 298. THE ATTACH CHORD STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0000152](https://openairdocs.org/sdr/CALA0000152.md): Skin · dented · Feb 13, 2000 · N58606 · Boeing 737524 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 295,S23L. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02924.
- [SDR CAL950483](https://openairdocs.org/sdr/CAL950483.md): Sensor Target · out of adjust · Jun 14, 1995 · N58606 · Boeing 737524 · Landing Gear Position and Warning
  > EWR - FLT 1535 - THE NLG RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANIDNG AT IAH. THE GEAR WAS CYCLED WITH NO CHANGE. EMERGENCY PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY CONFIRMED THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDEN
- [SDR CAL950466](https://openairdocs.org/sdr/CAL950466.md): Egt Indicator · inoperative · Jun 7, 1995 · N58606 · Boeing 737524 · Engine EGT/TIT Indicating System
  > FLT NR 1646 - DFW - THE NR 1 ENGINE OVERHEATED ACCOMPANIED BY ILLUMINATION OF RED LIGHT WHILE AT CRUISE. THE THROTTLE WAS REDUCED TO IDLE AND THE ENGINE SHUTDOWN MOMENTS LATER. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE B

## 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 = 'N58606' AND deregistration_id = 'N58606-2013-01-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N58606-2013-01-02/reports

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