# Service difficulty reports: N12536, cancelled Dec 21, 2006

A list on [N12536, cancelled Dec 21, 2006](https://openairdocs.org/deregistered/N12536-2006-12-21.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 5 · 238 reports

- [SDR GTIA030164](https://openairdocs.org/sdr/GTIA030164.md): Beam · cracked · Mar 18, 2003 · N12536 · Doug DC932 · Cargo/Baggage Doors
  > EDDY CURRENT INSPECTION REVEALED 2.25 INCH CRACKS EMANATING FROM FASTENER HOLE IN OUTER PAN OF AFT LOWER CARGO DOOR FWD EDGE AT BEAM 1. STOP DRILLED CRACKS AND INSTALLED PATCH ON AFT CARGO DOOR.
- [SDR GTIA030114](https://openairdocs.org/sdr/GTIA030114.md): Fitting · leaking · Feb 28, 2003 · N12536 · Doug DC932 · Aircraft Fuel Distribution System
  > RIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD.
- [SDR GTIA021045](https://openairdocs.org/sdr/GTIA021045.md): Isolator · corroded · Oct 6, 2002 · N12536 · Doug DC932 · Engine Mount Section
  > DTW - NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IS CORRODED AND PLATING IS FLAKING OFF ON INNER CONICAL AREA. REMOVED AND REPLACED NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR (CLOSED 10/15/02). (M)
- [SDR GTIA020965](https://openairdocs.org/sdr/GTIA020965.md): Odor · detected · Sep 10, 2002 · N12536 · Doug DC932 · Air Distribution System
  > ACY - FLT 276 - FLIGHT ATTENDANTS DETECTED A FAINT ODOR DURING THE INITIAL CLIMB BUT IT DISSIPATED BY LEVEL OFF. COULD NOT DETECT ANY ODOR WITH PACKS ON AND A/C RUNNING, OPS CHECK GOOD. (M)
- [SDR GTIA020843](https://openairdocs.org/sdr/GTIA020843.md): Light · inoperative · Jul 27, 2002 · N12536 · Doug DC932 · Landing Gear Position and Warning
  > FLT 276 - TPA - FOUND RIGHT LANDING GEAR BUTTON INDICATOR LIGHT INOPERATIVE, GREEN LENS. REMOVED AND REPLACED GEAR DOWNLOCK SWITCH ON RIGHT MAIN GEAR AND OPS CHECKED IAW MM 32-60-01. OPS CHECK NORMAL. CLOSED AS OF 8/28/02. (M)
- [SDR GTIA020831](https://openairdocs.org/sdr/GTIA020831.md): Structure · damaged · Jul 17, 2002 · N12536 · Doug DC932 · Trailing Edge Flaps
  > DTW - FOUND RIGHT FLAP TRAILING EDGE SPLICE APPROX 1.5 INCHES INBOARD END OF FLAP AT FIRST EXPANSION JOINT. SANDED AND INSTALLED FIBERGLASS LAYUP REPAIR ON RIGHT FLAP TRAILING EDGE. (M)
- [SDR GTIA020580](https://openairdocs.org/sdr/GTIA020580.md): Servo · faulty · Jun 3, 2002 · N12536 · Doug DC932 · Autopilot Main Servo
  > TPA - FLT 276 - AUTO PILOT AILERON SERVO IS ERRATIC IN ALL REQUIRES OF FLIGHT 276. REMOVED AND REPLACED SERVO AUTO DRIVE. OPS CHECK OK. BITE CHECK FOR SERVO PORTION OF CHECK ON ROLL COMP. NO DEFECTS NOTED. (M)
- [SDR GTIA020431](https://openairdocs.org/sdr/GTIA020431.md): Motor · malfunctioned · May 7, 2002 · N12536 · Doug DC932 · Stabilizer Actuator
  > ACY - PRIMARY TRIM HESITATES NOSE UP DIRECTION OCCURS USING BOTH CAPTAINS OR F/O'S YOKE SWITCHES AND USING SUIT CASE HANDLES. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPERATIONAL CHECKS GOOD. (M)
- [SDR GTIA020295](https://openairdocs.org/sdr/GTIA020295.md): Control Valve · malfunctioned · Apr 21, 2002 · N12536 · Doug DC932 · Landing Gear Retraction/Extension System
  > DTW - FLT 9536 - LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RECYCLED GEAR. UPLATCH CHECK GEAR DOOR OPEN LIGHT ILLUMINATED. REPLACED LANDING GEAR CONTROL VALVE AND ADJUSTED LEFT GEAR DOOR LATCH MECH. PERFORMED GEAR SWING. ALL SATISFACTORY AND LEAK CH
- [SDR GTIA020296](https://openairdocs.org/sdr/GTIA020296.md): Uplock Switch · faulty · Apr 21, 2002 · N12536 · Doug DC932 · Landing Gear Position and Warning
  > FLT 8019 - DTW - PUT GEAR UP, LEFT GEAR UNSAFE LIGHT CAM ON, UP LATCH CHECK RED LIGHT STAYED ON AND GEAR DOOR LIGHT (AMBER) CAME ON COMPLETED QRH PROCEDURE. REPLACED LT MLG UPLOCK SWITCH AND LT MLG DOOR SWITCH. VERIFIED LANDING GEAR RIGGING. NO DEFECTS. LU
- [SDR GTIA020294](https://openairdocs.org/sdr/GTIA020294.md): Latch · out of adjust · Apr 20, 2002 · N12536 · Doug DC932 · Landing Gear Door Retract Section
  > DTW - FLT 9536 - FOUND LEFT LANDING GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR RECYCLED IAW QRH SAME INDICATIONS. FOUND LEFT MAIN GEAR DOOR LATCH MECHANISM ASSEMBLY OUT OF ADJUSTMENT. ADJUSTED AND PERFORMED TEST IAW DC-9.
- [SDR GTIA020273](https://openairdocs.org/sdr/GTIA020273.md): Adc · faulty · Mar 30, 2002 · N12536 · Doug DC932 · Air Data Computer
  > FLT 616 - ACY - AUTO PILOT PITCH CONTROL PORPOISES DURING CLIMB AND DESCENTS AND WILL NOT HOLD ALTITUDE ALL OTHER FUNCTIONS OK FLT 616. REMOVED AND REPLACED AIR DATA COMPUTER PERFORMED PITOT STATIC LEAK CHECK. GROUND CHECK OK AT THIS TIME. (M)
- [SDR GTIA020242](https://openairdocs.org/sdr/GTIA020242.md): Controller · faulty · Mar 22, 2002 · N12536 · Doug DC932 · Autopilot System
  > ACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M)
- [SDR GTIA020220](https://openairdocs.org/sdr/GTIA020220.md): Computer · malfunctioned · Mar 8, 2002 · N12536 · Doug DC932 · Flight Controller
  > FLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMAL. (M)
- [SDR GTIA012218](https://openairdocs.org/sdr/GTIA012218.md): Web · cracked · Jan 17, 2002 · N12536 · Doug DC932 · Nacelle/Pylon, Main Frame
  > FTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED REPAIR ANGLE AND DOUBLERS. INSTALLED REPAIR ANGLE AND DOUBLERS IAW DC9
- [SDR GTIA020012](https://openairdocs.org/sdr/GTIA020012.md): Battery Pack · discharged · Jan 13, 2002 · N12536 · Doug DC932 · Emergency Lighting
  > DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM. OPS CHECK GOOD PER MM 33-53-01. (M)
- [SDR GTIA020009](https://openairdocs.org/sdr/GTIA020009.md): Battery Pack · discharged · Jan 13, 2002 · N12536 · Doug DC932 · Emergency Lighting
  > DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM, OPS CHECK GOOD PER DC9 MM 33-53-01. (M)
- [SDR GTIA012321](https://openairdocs.org/sdr/GTIA012321.md): Oxygen Mask · malfunctioned · Jan 3, 2002 · N12536 · Doug DC932 · Passenger Oxygen System
  > FTW - FOUND OXYGEN MASK DID NOT DROP IN AUTO. PERFORMED TROUBLE SHOOTING AND FOUND OXYGEN LEAK ON OXYGEN LINES. INSTALLED PROPERLY OXYGEN LINES. OPS CHECK GOOD IAW DC9 MM 35-20-0. (M)
- [SDR GTIA012319](https://openairdocs.org/sdr/GTIA012319.md): Rib · cracked · Dec 20, 2001 · N12536 · Doug DC932 · Leading Edge Devices
  > FTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012313](https://openairdocs.org/sdr/GTIA012313.md): Panel · warped · Dec 20, 2001 · N12536 · Doug DC932 · Spoilers
  > FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER WARP. REMOVED RIGHT INBOARD SPOILER PANEL. INSTALLED RIGHT INBOARD SPOILER PANEL IAW MM DC9 27-61-1. (M)
- [SDR GTIA012095](https://openairdocs.org/sdr/GTIA012095.md): Doubler · cracked · Dec 15, 2001 · N12536 · Doug DC932 · Engine Cowling System
  > FTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPAIR CRACKED. FORMED NEW SPLICE DOUBLER, INSTALLED NEW REPAIR IAW DC9 SRM 51-30-5. (M)
- [SDR GTIA012156](https://openairdocs.org/sdr/GTIA012156.md): Web · cracked · Dec 15, 2001 · N12536 · Doug DC932 · Engine Cowling System
  > FTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALUATION FOUND WEB ALSO CRACKED. CUT DAMAGED AREA (ON WEB). FABRICATED DRILLED AND LOCATED REPAIR PARTS FILLED DOUBLER. INSTALLED REPAIR PAR
- [SDR GTIA012191](https://openairdocs.org/sdr/GTIA012191.md): Splice · corroded · Dec 7, 2001 · N12536 · Doug DC932 · Wing Spar
  > FTW - FOUND LEFT WING LEADING EDGE UPPER FRONT SPAR PREVIOUS REPAIR HAS CORROSION FROM XFS 550-XFS 77. REMOVED CORROSION. SPLICE PLATE FOUND TO BE OUT OF LIMITS. FABRICATED SPLICE PLATE. INSTALLED SPLICE PLATE IAW MD80 SRM 51-30-5. (M)
- [SDR GTIA012122](https://openairdocs.org/sdr/GTIA012122.md): Channel · cracked · Dec 6, 2001 · N12536 · Doug DC932 · Fuselage Floor Panel
  > FTW - FOUND FORWARD ENTRY FLOOR PANEL HAT CHANNEL HAS CRACKED. REMOVED CRACKED CHANNEL. FABRICATED CHANNEL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012187](https://openairdocs.org/sdr/GTIA012187.md): Floorboard · damaged · Dec 4, 2001 · N12536 · Doug DC932 · Fuselage Floor Panel
  > FTW - CO-PILOT FLOORBOARD DAMAGED AT UPPER FACE. PUNCTURE AT STATION Y=150. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30-2. (M)
- [SDR GTIA012174](https://openairdocs.org/sdr/GTIA012174.md): Floorboard · damaged · Dec 4, 2001 · N12536 · Doug DC932 · Fuselage Floor Panel
  > FTW - FOUND FLOORBOARD WEB HAS HOLE Y211-X27. REMOVED DAMAGE. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED PER DC9 SRM 53-01. (M)
- [SDR GTIA012182](https://openairdocs.org/sdr/GTIA012182.md): Angle · chafed · Dec 3, 2001 · N12536 · Doug DC932 · Leading Edge Devices
  > NR 4 SLAT RIGHT CHORD ANGLE CHAFFED MORE THAN 50 PERCENT THICKNESS OF MATERIAL. REMOVED CHAFFED ANGLE. FABRICATED NEW CHORD ANGLE. INSTALLED NEW CHORD ANGLE IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012176](https://openairdocs.org/sdr/GTIA012176.md): Angle · chafed · Dec 2, 2001 · N12536 · Doug DC932 · Leading Edge Devices
  > FTW - FOUND NR 3 RIGHT SLAT OUTBOARD LOWER CHORD ANGLE CHAFFED MORE THAN 50 PERCENT OF MATERIAL THICKNESS. FORMED NEW CHORD ANGLE. INSTALLED FASTENERS IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012175](https://openairdocs.org/sdr/GTIA012175.md): Retainer · cracked · Dec 1, 2001 · N12536 · Doug DC932 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HAS TWO CRACKS AT RETAINER MOUNT HOLE 2 INCHES BELOW UPPER AFT CORNER. FABRICATED REPAIR DOUBLERS. INSTALLED DOUBLERS IAW DC9 SRM 52-01. (M)
- [SDR GTIA012308](https://openairdocs.org/sdr/GTIA012308.md): Floor Support · corroded · Nov 29, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -24 INCH TO -X43, FOUND AFTER G-1 REMOVED DUE A CORROSION BEYOND LIMITS AT FLOOR SUPPORT. DRILLED AND LOCATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-5. (M)
- [SDR GTIA012127](https://openairdocs.org/sdr/GTIA012127.md): Floor Support · corroded · Nov 29, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y = 160 FROM -X=1 TO -X=21. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-1. (M)
- [SDR GTIA012148](https://openairdocs.org/sdr/GTIA012148.md): Floor Support · corroded · Nov 29, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y=200 FROM -X47 INCHES TO -X=56 INCHES. REMOVED SUPPORT ANGLE. FORMED NEW FLOOR SUPPORT ANGLE IAW DC9 SRM 53-11-1. INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 53-11-1 OR 51-30-8. (M)
- [SDR GTIA012236](https://openairdocs.org/sdr/GTIA012236.md): Support Bracket · cracked · Nov 27, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND SUPPORT BRACKET CRACKED AT LEFT TRAPEZOIDAL PANEL STRUCTURE STA Y 729 X=59.500 Z=13.100. REMOVED BRACKET. INSTALLED NEW FILLER IAW DC9 SRM 51-30-1. (M)
- [SDR GTIA012109](https://openairdocs.org/sdr/GTIA012109.md): Skin · cracked · Nov 27, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/Skin
  > FTW - FOUND ANGLE SUPPORT HAS ELONGATED HOLES, AT LEFT TRAPEZOIDAL PANEL AFT UPPER AREA STA Y 730. UPON FURTHER INVESTIGATION, FOUND CRACK IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)
- [SDR GTIA012126](https://openairdocs.org/sdr/GTIA012126.md): Floor Support · cracked · Nov 27, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FLOOR SUPPORT CRACKED AT STATION Y=238 INCHES. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012171](https://openairdocs.org/sdr/GTIA012171.md): Doubler · cracked · Nov 26, 2001 · N12536 · Doug DC932 · Cargo/Baggage Doors
  > FTW - AFT LOWER CARGO, CARGO DOOR OUTBOARD LOWER CORNER DOUBLER PREVIOUS REPAIR CRACKED/WORN-OUT. REMOVED DAMAGE AREA. FORMED REPAIR. INSTALLED REPAIR IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012110](https://openairdocs.org/sdr/GTIA012110.md): Skin · cracked · Nov 26, 2001 · N12536 · Doug DC932 · Rudder, Plate/Skin
  > FTW - FOUND RUDDER RIGHT UPPER SKIN,.50 INCH DIAMETER DENT IN SKIN BETWEEN RIBS 17 AND 18. UPON FURTHER INVESTIGATION CRACK FOUND IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)
- [SDR GTIA012196](https://openairdocs.org/sdr/GTIA012196.md): Floor Support · corroded · Nov 25, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND ENTRY AREA, FLOOR SUPPORT CORRODED FROM STATION Y=160 TO STA Y=200. REMOVED FLOOR SUPPORT STA 160-200. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012223](https://openairdocs.org/sdr/GTIA012223.md): Floor Support · corroded · Nov 25, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FORWARD ENTRY FLOOR SUPPORT CORRODED FROM STA Y=162 TO Y=198. FABRICATED FLOOR SUPPORT. INSTALLED REPLACEMENT FLOOR SUPPORT IAW DC9 SRM 51-10-4 AND 51-30-1. (M)
- [SDR GTIA012222](https://openairdocs.org/sdr/GTIA012222.md): Floor Support · corroded · Nov 25, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STA Y=200 FROM X-24 INCH TO X-43 INCH. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT PER DC9 SRM 51-10-4. (M)
- [SDR GTIA012258](https://openairdocs.org/sdr/GTIA012258.md): Longeron · corroded · Nov 24, 2001 · N12536 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FTW - FOUND E/E BAY LONGERON 28 LEFT HAS CORROSION AT STATION 170-180. CUT OUT DAMAGE AND REMOVED. INSTALLED LONGERON AND SPLICE PER DC9 SRM 51-30-2. (M)
- [SDR GTIA012197](https://openairdocs.org/sdr/GTIA012197.md): Floor Support · corroded · Nov 23, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y200 FROM X2 INCHES TO -X21. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012264](https://openairdocs.org/sdr/GTIA012264.md): Angle · cracked · Nov 23, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FORWARD CARGO DOOR JAMB WEB STRAP AND ANGLES HAVE TOOLING MARKS, CORROSION AND CRACKS STATION 427-436. ONE ANGLE WAS CRACKED FORMED A NEW ANGLE. FORMED ANGLE. (M)
- [SDR GTIA012221](https://openairdocs.org/sdr/GTIA012221.md): Support · corroded · Nov 23, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - ANGLE SUPPORT CORRODED AT STATION Y916. FABRICATE NEW ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT IAW DC9 SRM 51-30-1. (M)
- [SDR GTIA012133](https://openairdocs.org/sdr/GTIA012133.md): Floor Support · corroded · Nov 23, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y200 FROM X= 1 INCH TO X= 20 INCHES. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)
- [SDR GTIA012146](https://openairdocs.org/sdr/GTIA012146.md): Strap · corroded · Nov 23, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND FORWARD CARGO DOOR JAMB AFT STATION 427-438 WEB STRAPS HAVE TOOLING MARKS AND SURFACE CORROSION. FORMED STRAP. LOCATED AND DRILLED STRAP IAW DC9 SRM 51-10-4. (M)
- [SDR GTIA012192](https://openairdocs.org/sdr/GTIA012192.md): Web · corroded · Nov 22, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND CUSP WEB CORRODED AT STATION Y=200 X=56. CORROSION WAS FOUND DURING OPEN UP FOR WEB REPAIR AT FRAME STATION -200, X=57. REMOVED CORROSION. REMOVED SECTION OF CUSP. WEB DAMAGED. FABRICATED AND LOCATED CUSPS WEB. INSTALLED IAW DC9 SRM 51-30-2.
- [SDR GTIA012124](https://openairdocs.org/sdr/GTIA012124.md): Web · damaged · Nov 21, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND LOWER INNER WEB FORWARD BAG DOOR FS 370 TO FS 427 HAS OVERSIZED HOLES, EXTRA HOLES, CORRODED HOLES, A BAD PREVIOUS REPAIR AND NUMEROUS DENTS FROM OVER DRIVEN RIVETS. LOCATED AND DRILLED NEW INNER WEB. INSTALLED INNER WEB IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA012263](https://openairdocs.org/sdr/GTIA012263.md): Structure · cracked · Nov 19, 2001 · N12536 · Doug DC932 · Fuselage Main, Structure
  > FTW - FORWARD CARGO COMPARTMENT HAS A CRACK BETWEEN STATION 465-484 BETWEEN LONGERON 30 AND 29L. FORMED INTERCOSTAL IAW DOUGLAS PRING SR09530005. FORMED AND INSTALLED REPAIR PARTS. (M)
- [SDR GTIA012112](https://openairdocs.org/sdr/GTIA012112.md): Web · corroded · Nov 19, 2001 · N12536 · Doug DC932 · Fuselage Miscellaneous Structure
  > FTW - FOUND CABIN LEFT SIDE CORRODED AT MEMBRANE WEB STATION 908. REMOVED MEMBRANE WEB FROM STATION 897 TO 964. FORMING MEMBRANE/WEB. INSTALLED NEW MEMBRANE/WEB IAW DC9 SRM 51-30-2. (M)

Next page: https://openairdocs.org/deregistered/N12536-2006-12-21/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 = 'N12536' AND deregistration_id = 'N12536-2006-12-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12536-2006-12-21/reports

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