# Service difficulty reports: N17614, cancelled Oct 9, 2012

A list on [N17614, cancelled Oct 9, 2012](https://openairdocs.org/deregistered/N17614-2012-10-09.md).

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

Page 1 of 2 · 53 reports

- [SDR CALA2012041100253](https://openairdocs.org/sdr/CALA2012041100253.md): Sensor · out of rig · Apr 11, 2012 · N17614 · Boeing 737524 · Navigation System
  > AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. AIR RETURN PER QRH, SUSPECT FAILURE OF AIR/GROUND SENSING LOGIC. EXPERIENCED DEGRADED SYSTEMS INDICATED IN CHECKLIST. CHECKED INTERLOCK VALUE TELEFLEX CABLE RIGGING IAW AMM 32-09-01-825 -002, O
- [SDR CALA2011120700796](https://openairdocs.org/sdr/CALA2011120700796.md): Wire Harness · shorted · Dec 5, 2011 · N17614 · Boeing 737524 · Window System Wiring
  > F/O SIDE WINDOW SHORTHED OUT DURING T/O. FOUND SHORTHED WIRE BUNDLE (COILED HARNESS) ON F/O SIDE AT WINDOW BASE. REMOVED AND REPLACED COILED HARNESS FOR WINDOW HEAT CONTROL ON F/O SLIDE WINDOW IN REF TO WDM 30-41-11 AND OPS CHECKED IN REF TO AMM 56-12-11-404
- [SDR CALA2010061400276](https://openairdocs.org/sdr/CALA2010061400276.md): Skin · cracked · Jun 11, 2010 · N17614 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK, FWD ENTRY DOOR CUTOUT AREA, HOLE CRACK INDICATION AT STA 302.9 THIRD FASTENER BELOW WL 236.68 (REF EA 5330-03736 CIRCLE NOTE 3 FIG 5 LAST LWR HOLE). INSTALLED REPAIR DOUBLERS IN REF ECRA 5330-04031. INITIATED DIP AS FOLLOW;" BEFORE ACCUMULATION
- [SDR CALA2010061400275](https://openairdocs.org/sdr/CALA2010061400275.md): Web · worn · Jun 10, 2010 · N17614 · Boeing 737524 · Wing Miscellaneous Structure
  > RIGHT WING AT APPROX RSS 500 HAS A WORN AREA ON I/B SIDE OF WEB ABOUT 3 INCHES AFT OF AILERON CABLE GROMMET. INSTALLED DOUBLERS REPAIR REF ECRA 5720-02138 PART 1. INITIATED DIP AS FOLLOW; "ACCOMPLISH PERMANENT REPAIR BEFORE 6-7-2012. PLANNING TO CONTACT ENG
- [SDR CALA2010061400274](https://openairdocs.org/sdr/CALA2010061400274.md): Frame · corroded · Jun 10, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > FRAME STA 380 AT S28R HAS CORROSION. REPAIRED PER ECRA 5311-01495 PART 1 REF NR LP 9717663 FOR DIP.
- [SDR CALA2010061400273](https://openairdocs.org/sdr/CALA2010061400273.md): Floor Support · corroded · Jun 10, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - STA 270 CORROSION AROUND SEVERAL FASTENER HOLES ON FLOOR SUPPORT STRUCTURE AT NLG DOWN LOCK VIEWER APPROXIMATELY BETWEEN LBL 6 TO LBL 9. REPAIRED PER ECRA 5311-01497.
- [SDR CALA2010061400272](https://openairdocs.org/sdr/CALA2010061400272.md): Skin · cracked · Jun 10, 2010 · N17614 · Boeing 737524 · Fuselage Main, Plate/Skin
  > SUPPORT TASK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, CRACK INDICATION AT LOWER, MOST FORWARD HOLE OF LWR FITTING LEG. FIG 4 CIRCLE NOTE 7 OF EA 5330-03736 REV B, REPAIRED PER ECRA 5330-04032.
- [SDR CALA2010061400271](https://openairdocs.org/sdr/CALA2010061400271.md): Skin · cracked · Jun 10, 2010 · N17614 · Boeing 737524 · Passenger/Crew Doors
  > L2 DOOR INNER SKIN IS CRACKED AT UPPER SECTION AT CENTER LIGHTENING HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02156.
- [SDR CALA2010061400270](https://openairdocs.org/sdr/CALA2010061400270.md): Floorbeam · corroded · Jun 10, 2010 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > ABB ALL FLOORBEAMS UNDER STRAP BETWEEN STA 767 & 787 CORRODED. REPAIRED PER ECRA 5320-01990. COMPLETED AND ATTACHED FORM 44.00 08.
- [SDR CALA2010061000266](https://openairdocs.org/sdr/CALA2010061000266.md): Skin · dented · Jun 9, 2010 · N17614 · Boeing 737524 · Fuselage Main, Plate/Skin
  > DENT ON BOTTOM OF FWD FUSELAGE AT STATION 197 AND A FEW INCHES RIGHT OF CENTER LINE REF ECRA 5331-01463. INSP DENT PER ECRA PART 1 STEP 1-5. NO DEF C/W ECRA 5331-01463 REV B PART 1A. PLACED ON DIP C/N 00814. ACCOMPLISH EC FOR WORK PERFORMED. DIP REMAINS R
- [SDR CALA2010061000269](https://openairdocs.org/sdr/CALA2010061000269.md): Attach Fitting · cracked · Jun 9, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > SUPPORT TASK, L-1 DOOR FUSELAGE OPENING AFT SIDE STR 15 INTERCOSTAL FWD ATTACH CLIP STA 348.2 CRACKED IN RADIUS I/B SIDE. REMOVED AND REPLACED ATTACH CLIP STA 348.2 STR 15L REF ECRA 5311-01496.
- [SDR CALA2010061000268](https://openairdocs.org/sdr/CALA2010061000268.md): Stringer Splice · cracked · Jun 9, 2010 · N17614 · Boeing 737524 · Fuselage Main, Longeron/Stringer
  > SUPPORT TASK, CRACK IN STR SPLICE CHANNEL AT STR 14L JUST FWD OF FRAME STA 360. REMOVED AND REPLACED STR SPLICE CHANNEL AT STR 14L STA 360 REF ECRA 5311-01496.
- [SDR CALA2010061000267](https://openairdocs.org/sdr/CALA2010061000267.md): Support Angle · cracked · Jun 9, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > L-1 DOOR SURROUND STRUCTURE HAS CRACK ON STR 11 SUPPORT AT STA 360. REMOVED AND REPLACED SUPPORT ANGLE AT STR 11L STA 360 REF ECRA 5311-01496.
- [SDR CALA2010060800257](https://openairdocs.org/sdr/CALA2010060800257.md): Fitting · corroded · Jun 7, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > ABB SKIN CLIP CORRODED STA 727C BETWEEN STR-26 RT. & 27 RT. REMOVED DAMAGED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 201 REPAIR 4.
- [SDR CALA2010060800252](https://openairdocs.org/sdr/CALA2010060800252.md): Flap Track · corroded · Jun 5, 2010 · N17614 · Boeing 737524 · Trailing Edge Flaps
  > RT WING NR 8 FLAP TRACK AFT ATTACH POINT EMITTING RUST. REMOVED NR 8 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACK REF M/M 27-51-49-404-006.
- [SDR CALA2010060800251](https://openairdocs.org/sdr/CALA2010060800251.md): Flap Track · corroded · Jun 5, 2010 · N17614 · Boeing 737524 · Trailing Edge Flaps
  > EVIDENCE OF RUST BETWEEN NR 7 FLAP TRACK AND LWR SURFACE OF REAR SPAR REMOVED NR 7 FLAP TRACK ASSY. ROTABLE PARTS CHANGE WAS INDICATED - 24-5753-9-9001 TRACK, FLAP, OB OFF 24-5753-9-9001 1614 ON. REMOVED NR 7 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRAC
- [SDR CALA2010060800250](https://openairdocs.org/sdr/CALA2010060800250.md): Fitting · corroded · Jun 5, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > ABB STA 747 BETWEEN STR 26 RT.& 27 RT SKIN CLIP CORRODED. REMOVED SHEAR TIE AND INSTALLED REPAIR REF SRM 53-00-07 FIG 20 1.
- [SDR CALA2010060100241](https://openairdocs.org/sdr/CALA2010060100241.md): Seat Track · corroded · Jun 1, 2010 · N17614 · Boeing 737524 · Fuselage, Seat/Cargo Attach Fittings
  > LT OTBD SEAT TRACK HAS CORROSION FROM STA 787 TO STA 887. REPAIRED LT OTBD SEAT TRACK BETWEEN STA 787-807, REF SRM 53-00-52, REPAIR 4, PAGE 201, SHEET 1-4, AND STA 807-927 REF SRM 53-00-52 REPAIR 3, PAGE 201, SHEET 1-4, ATTACH FROM 44.008 PAGE 1-2 AND ECRA 53
- [SDR CALA2010060100235](https://openairdocs.org/sdr/CALA2010060100235.md): Transition Panel · corroded · May 28, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > ABB LT TRANSITION PANEL CORRODED FROM 727C TO 947.5. REMOVED AND INSTALLED FABRICATED TRANSITION PANEL FROM STA 727- STA 947.5 IN REF TO SRM 53-60-53 AND SRM 53-30-53.
- [SDR CALA2010060100234](https://openairdocs.org/sdr/CALA2010060100234.md): Angle · corroded · May 28, 2010 · N17614 · Boeing 737524 · Fuselage Miscellaneous Structure
  > L1 DOOR LT ANGLE, STA 349 JUST AFT OF DRAIN AND ON UNDER SIDE HAS CORROSION. R & R LT ANGLE REF SRM 51-40-02.
- [SDR CALA2010052700227](https://openairdocs.org/sdr/CALA2010052700227.md): Seat Track · corroded · May 28, 2010 · N17614 · Boeing 737524 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT O/B SEAT TRACK HAS CORROSION STA 695 FOUND OUT OF LIMITS. CUT & REMOVED SEAT TRACK, FABRICATED NEW TRACK, APPLIED PROTECTIVE COATING, PRIMED & INSTALLED REF SRM 53 -00-52.
- [SDR CALA2010052700229](https://openairdocs.org/sdr/CALA2010052700229.md): Stop Fitting · cracked · May 27, 2010 · N17614 · Boeing 737524 · Service Doors
  > R-1 DOOR LOWER AFT STOP FITTING, INTERIOR LEG CRACKED THROUGH HI-LOK HOLE (MARKED). VERIFIED WITH HFEC P/N OF FITTING 65-51647-501. REMOVED CRACKED FRAME REINFORCEMENT, FABRICATED, ALODINED AND PRIMED NEW FRAME REINFORCEMENT AND INSTALLED REF BAC DRAWING 69-
- [SDR CALA2010052700228](https://openairdocs.org/sdr/CALA2010052700228.md): Fitting · corroded · May 26, 2010 · N17614 · Boeing 737524 · Trailing Edge Flap Control System
  > NR 3 MID FLAP O/B TORQUE TUBE HOUSING HAS CORROSION. REMOVED AND INSTALLED NEW FITTING PER SRM 51-40-02 PARAGRAPH 7 AND 51-20-02 PARAGRAPH 8.
- [SDR CALA2010052700222](https://openairdocs.org/sdr/CALA2010052700222.md): Frame · cracked · May 23, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > MAIN FRAME CRACKED AT STA 616 BELOW STR 17 RT. INSTALLED REPAIR PER ECRA 5311-01158.
- [SDR CALA2010051700205](https://openairdocs.org/sdr/CALA2010051700205.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > PAX CABIN HAS CRACKED FRAME STA 380 BETWEEN STR 8R AND 9R. REPAIRED FRAME PER EA 5310-04498.
- [SDR CALA2010051700210](https://openairdocs.org/sdr/CALA2010051700210.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > LEFT FRAME CRACKED STA 482 BETWEEN STR 8&9. REPAIRED LT FRAME AT STR 482 BETWEEN STR 8&9 REF EA5310-04498 OP2.
- [SDR CALA2010051700209](https://openairdocs.org/sdr/CALA2010051700209.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > SUPPORT TASK LT FUSELAGE FRAME CRACKED BETWEEN STR 8&9 STA 400. INSTALLED REPAIR ANGLES A&B PER EA 5310-04498.
- [SDR CALA2010051700208](https://openairdocs.org/sdr/CALA2010051700208.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > PAX CABIN HAS CRACKED FRAME STA 867 BETWEEN STA 8R AND 9R. REPAIRED CRACKED FRAME AT STA 867 BETWEEN STR 8R AND 9R REF EA 5310-04498 OP 2.
- [SDR CALA2010051700207](https://openairdocs.org/sdr/CALA2010051700207.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > PAX CABIN HAS CRACKED FRAME STA 787 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES REF EA5310-04498.
- [SDR CALA2010051700206](https://openairdocs.org/sdr/CALA2010051700206.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > PAX CABIN HAS CRACKED FRAME STA 440 BETWEEN STR 8R AND 9R. INSTALLED REPAIR ANGLES, REF EA5310-04498.
- [SDR CALA2010051700204](https://openairdocs.org/sdr/CALA2010051700204.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > RIGHT FRAME CRACKED STA 842 BETWEEN STR 8-9 FRAME WAS CRACKED DURING PSU RAIL BLOCK REMOVAL. REPAIRED RT FRAME AT STA 482 BETWEEN STR8-9 REF EA 5310-04498 OP2.
- [SDR CALA2010051700203](https://openairdocs.org/sdr/CALA2010051700203.md): Frame · cracked · May 17, 2010 · N17614 · Boeing 737524 · Fuselage Main, Frame
  > LEFT FRAME STA 440 BETWEEN STR 8 &9 CRACKED. REPAIRED FRAME STA 440 LT BETWEEN STR 8&9 LT PER EA 5310-04498 OP2.
- [SDR CALA2009122100748](https://openairdocs.org/sdr/CALA2009122100748.md): Battery · discharged · Dec 21, 2009 · N17614 · Boeing 737524 · Emergency Equipment
  > AFT RT EMERGENCY FLASHLIGHT INDICATOR DOES NOT FLASH. REMOVED AND REPLACED AFT RT EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD.
- [SDR CALA2009102300644](https://openairdocs.org/sdr/CALA2009102300644.md): Circuit Breaker · tripped · Oct 23, 2009 · N17614 · Boeing 737524 · Landing Gear Position and Warning
  > AT FLIGHT IDLE ONLY THE NOSE GEAR RED LIGHT IS ILLUMINATED NOT THE MAIN GEARS. FOUND AIR/GND RELAY C/B OUT (PG-3, ROW 17C) AS DIRECTED BY MAINTENANCE, RESET C/B (CONT L/P 8331803) RESET C/B AND TROUBLESHOT PER AMM 32-61-00/101. LANDING GEAR LEVER WAS CYCLED
- [SDR CALA2009082600500](https://openairdocs.org/sdr/CALA2009082600500.md): Cable · frayed · Aug 26, 2009 · N17614 · Boeing 737524 · Emergency Equipment
  > L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737AMM 25-61-35-402-007.
- [SDR CALA2009080600439](https://openairdocs.org/sdr/CALA2009080600439.md): Cable Assy · frayed · Aug 6, 2009 · N17614 · Boeing 737524 · Emergency Equipment
  > L2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED L2 EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 25-61-35-402-007.
- [SDR CALA2009080600438](https://openairdocs.org/sdr/CALA2009080600438.md): Cable Assy · frayed · Aug 6, 2009 · N17614 · Boeing 737524 · Emergency Equipment
  > R2 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR LATCH CABLE HAS BROKEN STRANDS (FCD 2561-01189). REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW 737 AMM 25-61-35-402-007.
- [SDR CALA2009080300404](https://openairdocs.org/sdr/CALA2009080300404.md): Uplock Actuator · malfunctioned · Jul 31, 2009 · N17614 · Boeing 737524 · Landing Gear Actuator
  > RIGHT MAIN GEAR UNSAFE AFTER TAKEOFF, AIRCRAFT DESCENDED TO LOWER ALT, AS THROTTLES ADVANCED RIGHT MAIN GEAR FREE FELL DOWN. EXECUTED UNSAFE GEAR INDICATION CHECK LIST, GEAR DOWN 3-GREEN, AIR RETURN ACCOMPLISHED. CYCLED LANDING GEAR SEVERAL TIMES, NO FAULTS
- [SDR CALA0700084](https://openairdocs.org/sdr/CALA0700084.md): Charger · inoperative · Feb 23, 2007 · N17614 · Boeing 737524 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS AT SEATS 20-25 WERE FOUND INOPERATIVE. THE CHARGER AND BATTERY PACK WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0600080](https://openairdocs.org/sdr/CALA0600080.md): Power Supply · inoperative · Mar 4, 2006 · N17614 · Boeing 737524 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY ESCAPE AISLE PATH LIGHTING INOPERATIVE AT ROWS 15-21. THE BATTERY PACK AND POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51.
- [SDR CALA0500432](https://openairdocs.org/sdr/CALA0500432.md): Wire · shorted · Dec 9, 2005 · N17614 · Boeing 737524 · Light System Wiring
  > INSPECTION FOUND THE EMERGENCY EXIT LIGHTS OUT ON SEAT ROWS 7-14ABC. MAINTENANCE FOUND A POWER WIRE SHORTED TO SEAT TRACK AT SEAT 7ABC. THE WIRE WAS REPAIRED IAW SRM 20-11-00.
- [SDR CALA0500130](https://openairdocs.org/sdr/CALA0500130.md): Floorbeam · corroded · Apr 26, 2005 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT STA 986.5, LBL 43. INSTALLED DOUBLER PER ECRA 5321-01210.
- [SDR CALA0500129](https://openairdocs.org/sdr/CALA0500129.md): Floorbeam · corroded · Apr 26, 2005 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT STA 986.5, RBL43. INSTALLED DOUBLER PER ECRA 5321-01209.
- [SDR CALA0500072](https://openairdocs.org/sdr/CALA0500072.md): Floorbeam · corroded · Mar 8, 2005 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FASTENER HOLE OF FORWARD FLANGE OF UPPER CHORD, STA 986, LBL 43. A REPAIR WAS INSTALLED IAW ECRA 5321-01210.
- [SDR CALA0500071](https://openairdocs.org/sdr/CALA0500071.md): Floorbeam · corroded · Mar 7, 2005 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM FORWARD FLANGE OF UPPER CHORD FASTENER HOLE CORRODED AT STA 986, RBL 43 TO RBL 44. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01209.
- [SDR CALA0500060](https://openairdocs.org/sdr/CALA0500060.md): Floorbeam · corroded · Feb 27, 2005 · N17614 · Boeing 737524 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT AFT FLANGE OF UPPER CHORD, STA 986, LBL 14 TO LBL 18. THE CORRODED AREA WAS CUT OUT AND ANGLES WERE INSTALLED IAW SRM 53-60-51.
- [SDR CALA0300332](https://openairdocs.org/sdr/CALA0300332.md): Circuit Breaker · failed · Jun 23, 2003 · N17614 · Boeing 737524 · AC Generation System
  > A HEAVY ELECTRICAL ODOR WAS NOTICED IN THE CABIN WHILE EN ROUTE TO DCA. THE ODOR WAS ACCOMPANIED BY FAILURE OF CABIN LIGHTS, OVEN, AND AUTOPILOT AND THE NR 1 ENGINE GENERATOR BUS OFF LIGHT, AND RIGHT EQUIP COOLING SUPPLY OFF LIGHT ILLUMINATED. THE AIRCRAFT L
- [SDR CALA9900769](https://openairdocs.org/sdr/CALA9900769.md): Megaphone · inoperative · Jul 5, 1999 · N17614 · Boeing 737524 · Emergency Equipment
  > THE AFT MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED.
- [SDR CALA9900696](https://openairdocs.org/sdr/CALA9900696.md): Light · inoperative · Jun 15, 1999 · N17614 · Boeing 737524 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT L-2 DOOR. THE EXIT LIGHT ASSEMBLY WAS REPLACED IAW MM 33-51-11.
- [SDR CALA9802181](https://openairdocs.org/sdr/CALA9802181.md): Circuit Breaker · tripped · Dec 17, 1998 · N17614 · Boeing 737524 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR HANDLE WOULD NOT RAISE BEYOND THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LATCH AND WARNING CIRCUIT BREAKER POPPE

Next page: https://openairdocs.org/deregistered/N17614-2012-10-09/reports.md?page=2

## 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 = 'N17614' AND deregistration_id = 'N17614-2012-10-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17614-2012-10-09/reports

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