# Service difficulty reports: N11612, cancelled Mar 14, 2013

A list on [N11612, cancelled Mar 14, 2013](https://openairdocs.org/deregistered/N11612-2013-03-14.md).

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

- [SDR CALA2012041600264](https://openairdocs.org/sdr/CALA2012041600264.md): Uplock Sensor · faulty · Apr 13, 2012 · N11612 · Boeing 737524 · Landing Gear Position and Warning
  > AFTER TAKEOFF LEFT MAIN GEAR RED LIGHT REMAINED ON. AFTER GEAR RETRACTION RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN BOTH UP AND OFF. FOUND LT MLG UPLOCK SENSOR AT FAULT. REF MM 32-61-00-101 R/R LT MLG UPLOCK SENSOR REF MM 32-61-21. CYCLED GE
- [SDR CALA2012032900216](https://openairdocs.org/sdr/CALA2012032900216.md): Flex Line · torn · Mar 28, 2012 · N11612 · Boeing 737524 · Hydraulic System, Main
  > AFTER T/O B-SYS HYD WENT TO ZERO AND BOTH PRESSURE LOW LIGHT CAME ON. RAN QRH, RETURN TO EWR. FOUND FLEX LINE TORN. REMOVED AND REPLACED FLEX LINE REF L/P 4556125 LINE, OPS CK NORMAL. OK TO CONTINUE.
- [SDR CALA2011050200328](https://openairdocs.org/sdr/CALA2011050200328.md): Fuse · blown · Apr 30, 2011 · N11612 · Boeing 737524 · Emergency Lighting
  > FLT DECK EMERGENCY DOME LIGHT FAILED DURING TEST, L273. FOUND EMERGENCY BATT PWR PACK M1675 AT STA 318, F4 PICO FUSE BAD. REPLACED FUSE REF AMM 33-5151-910-817C1, OPS CHECK GOOD.
- [SDR CALA2011030700126](https://openairdocs.org/sdr/CALA2011030700126.md): Skin · damaged · Mar 6, 2011 · N11612 · Boeing 737524 · Fuselage Main, Plate/Skin
  > LT UPPER FUSELAGE SKIN DAMAGED AT APPROX STA 1121 BENEATH VERTICAL STAB ATTACH ANGLE. INSTALLED REPAIR DOUBLER REF EC/RA 5331-01553.
- [SDR CALA2011030400117](https://openairdocs.org/sdr/CALA2011030400117.md): Skin · dented · Mar 4, 2011 · N11612 · Boeing 737524 · Fuselage Main, Plate/Skin
  > LARGE SHALLOW DENT RT SIDE OF FUSELAGE STARTING AT STA 362.5 AND EXTENDING TO STA 372.75 AND LOCATED BETWEEN S-18R AND S-19R. REPAIRED FUSELAGE PER ECRA 5331-01552 AND INITIATED DIP 09510 TO RE-INSPECT PER PART 2 OF ECRA 5331-01552 ON OR BEFORE THE ACCUMULATI
- [SDR CALA2011030700122](https://openairdocs.org/sdr/CALA2011030700122.md): Skin · cracked · Mar 2, 2011 · N11612 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK: PER STEP 20.0 OF EA 5330-03736 REV B CRACK INDICATION VERIFIED IN HOLE MARKED NR 1 ON FIG 5 SHEET 2 OF WORKCARD. REPAIR ACCOMPLISHED PER ECRA 5330-04106. SEQ N959 FOR DIP INITIATED.
- [SDR CALA2011022800111](https://openairdocs.org/sdr/CALA2011022800111.md): Skin · dented · Feb 28, 2011 · N11612 · Boeing 737524 · Cargo/Baggage Doors
  > SUPPORT TASK - DENT ON AFT CARGO DOOR EXTERNAL SKIN LOCATED 12 INCHES FROM FWD EDGE A/Y IS LESS THAN 30. INSTALLED REPAIR DOUBLER ON AFT CARGO EXTERNAL SKIN REF SRM 52-00-01 REPAIR 3.
- [SDR CALA2011022400108](https://openairdocs.org/sdr/CALA2011022400108.md): Skin · worn · Feb 24, 2011 · N11612 · Boeing 737524 · Electrical/Electronic Compartment Doors
  > SUPPORT TASK E&E DOOR HAS LARGE BLEND OUT ON SKIN EDGE. REPAIRED E&E DOOR OUT SKIN REF SRM 52-00-01 PAGE 201 TO 204 (REPAIR NR 2).
- [SDR CALA2011021800099](https://openairdocs.org/sdr/CALA2011021800099.md): Plate · cracked · Feb 18, 2011 · N11612 · Boeing 737524 · Service Doors
  > R1 DOOR-AFT LOWER CORNER STOP FITTING IS CRACKED THROUGH HI-LOK HOLE (MARKED) SEEN FROM INTERIOR P/N 65-51674-501. INSPECT STOP FITTING AND NO CRACK WAS FOUND. HOWEVER, REINFORCING PLATE ON BACK SIDE OF FITTING WAS CRACKED. REMOVED AND REPLACED REINFORCING
- [SDR CALA2011021800098](https://openairdocs.org/sdr/CALA2011021800098.md): Hinge Fitting · cracked · Feb 18, 2011 · N11612 · Boeing 737524 · Fuselage, Door Hinge
  > SUPPORT TASK-L-1 DOOR FWD JAMB UPPER HINGE FITTING IS CRACKED. REMOVED & REPLACED L-1 FWD JAMB UPPER HINGE FITTING REF SRM 51-40-02.
- [SDR CALA2011021700096](https://openairdocs.org/sdr/CALA2011021700096.md): Frame · cracked · Feb 17, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK - LT SIDE MAIN FRAME CRACK STA 616 AT JUST BELOW MAIN DECK FLOOR ACCOMPLISHED FRAME REPAIR ON (SEE) EA 5310-05331 OP1 STEP 24.1 THRU STEP 24.14.
- [SDR CALA2011032400176](https://openairdocs.org/sdr/CALA2011032400176.md): Frame · cracked · Feb 11, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 867 AT S-9R. INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A OP2.
- [SDR CALA2011032400175](https://openairdocs.org/sdr/CALA2011032400175.md): Frame · cracked · Feb 11, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 907 AT S-9L. CTN53-304-108 INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A.
- [SDR CALA2011032400177](https://openairdocs.org/sdr/CALA2011032400177.md): Frame · cracked · Feb 11, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > FRAME CRACKED STA 907 AT S-9R CTN53-304-108 INSTALLED REPAIR ANGLES A&B PER EA.5310-04498, REV-A.
- [SDR CALA2011020900077](https://openairdocs.org/sdr/CALA2011020900077.md): Angle · corroded · Feb 9, 2011 · N11612 · Boeing 737524 · Fuselage Miscellaneous Structure
  > SMALL AREAS OF LIGHT CORROSION (MARKED) ON FLOOR STRUCT. "Z" ANGLE AT R2 DOOR OPENING. REMOVED DAMAGE, FOUND OUT OF LIMITS SRM 53-60-15 FIG 101. REMOVED AND REPLACED "Z" ANGLE AT R2 DOOR SRM 51-40-02.
- [SDR CALA2011020800072](https://openairdocs.org/sdr/CALA2011020800072.md): Frame · cracked · Feb 8, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > FRAME IS CRACKED AT O/H BIN RAIL STA 360 S-8L. INSTALLED REPAIR DOUBLERS IN REF ECRA 5310-05351.
- [SDR CALA2011020800071](https://openairdocs.org/sdr/CALA2011020800071.md): Support Bracket · cracked · Feb 8, 2011 · N11612 · Boeing 737524 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - STA 482 AIR CONDITIONING SUPPORT BRACKET BTWN S-8 LT & S-9 LT I/B RIVET HOLE CRACKED. INSTALLED REPAIR ANGLES REF EA 5310-04498 REV A OP 02.
- [SDR CALA2011020700066](https://openairdocs.org/sdr/CALA2011020700066.md): Frame · cracked · Feb 6, 2011 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > FRAME IS CRACKED AT O/H BIN RAIL STA 400 S-8L. INSTALLED REPAIR DOUBLERS AT O/H BIN RAIL STA 400 STR 8L REF EA 5310-04498 REV A.
- [SDR CALA0700630](https://openairdocs.org/sdr/CALA0700630.md): Frame · cracked · Oct 31, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME BETWEEN STRINGER 8R AND 9R, STA 727-827. A DOUBLER AND STRAP WERE INSTALLED IAW ECRA 5310-04668, REV B.
- [SDR CALA0700620](https://openairdocs.org/sdr/CALA0700620.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A. 5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 440 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700619](https://openairdocs.org/sdr/CALA0700619.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 380 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700618](https://openairdocs.org/sdr/CALA0700618.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700617](https://openairdocs.org/sdr/CALA0700617.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A 5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 867 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700616](https://openairdocs.org/sdr/CALA0700616.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 827 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700615](https://openairdocs.org/sdr/CALA0700615.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700614](https://openairdocs.org/sdr/CALA0700614.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 747 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700613](https://openairdocs.org/sdr/CALA0700613.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700612](https://openairdocs.org/sdr/CALA0700612.md): Frame · cracked · Oct 26, 2007 · N11612 · Boeing 737524 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.
- [SDR CALA0700607](https://openairdocs.org/sdr/CALA0700607.md): Fitting · cracked · Oct 24, 2007 · N11612 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK AT DOOR FITTING FASTENER IN L-1 DOOR OPENING AFT SIDE STRUCTURAL STRAP, STA 349, S16L. A REPAIR WAS INSTALLED IAW SRM 53-10-04.
- [SDR CALA0700606](https://openairdocs.org/sdr/CALA0700606.md): Structure · cracked · Oct 24, 2007 · N11612 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0700601](https://openairdocs.org/sdr/CALA0700601.md): Angle · corroded · Oct 22, 2007 · N11612 · Boeing 737524 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AN L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 43 TO LBL 60. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-52878.
- [SDR CALA0700599](https://openairdocs.org/sdr/CALA0700599.md): Floorbeam · corroded · Oct 22, 2007 · N11612 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 4. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.
- [SDR CALA0700598](https://openairdocs.org/sdr/CALA0700598.md): Floorbeam · corroded · Oct 22, 2007 · N11612 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 40. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.

## 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 = 'N11612' AND deregistration_id = 'N11612-2013-03-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N11612-2013-03-14/reports

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