# Service difficulty reports: N17535, cancelled Aug 29, 2001

A list on [N17535, cancelled Aug 29, 2001](https://openairdocs.org/deregistered/N17535-2001-08-29.md).

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

- [SDR 20000426SH015](https://openairdocs.org/sdr/20000426SH015.md): Jackscrew · making metal · Mar 31, 2000 · N17535 · Doug DC932 · Elevator Control System
  > DURING INSPECTION OF THE HORIZONTAL STABILIZER JACKSCREW ASSY, METAL SHAVINGS WERE FOUND WITHIN THE GREASE ON AND AROUND THE JACKSCREW. FURTHER, THE ACME SCREW AND NUT WEAR CHECK SHOWED THE END PLAY WAS BEYOND LIMITS. THE ESTABLISHED LIMITS ARE.003 INCH -
- [SDR GTIA9901084](https://openairdocs.org/sdr/GTIA9901084.md): Wire · failed · Aug 18, 1999 · N17535 · Doug DC932 · Light System Wiring
  > MYR - BOTH EMERGENCY NACELLE LIGHTS INOPERATIVE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 333. REPAIRED WIRING AT AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS 'TEST' SWITCH. FUNCTIONAL CHECK GOOD, REF DC-9 WIRING DIAGRAMS 33-31-01. (M)
- [SDR GTIA9900989](https://openairdocs.org/sdr/GTIA9900989.md): Wire · loose · Jun 22, 1999 · N17535 · Doug DC932 · Light System Wiring
  > FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRES OUT ON FLOOR ROW EIGHT RESECURED AS NECESSARY. OPERATION CHECK GOOD IAW DC-9 MM 33-50. (M)
- [SDR GTIA9900942](https://openairdocs.org/sdr/GTIA9900942.md): Wire · loose · Jun 22, 1999 · N17535 · Doug DC932 · Light System Wiring
  > FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRE OUT OF FLOOR ROW EIGHT. RESECURED AS NECESSARY. OPERATION CHECKS GOOD IAW DC-9 MM 33-50. (X)
- [SDR GTIA9800075](https://openairdocs.org/sdr/GTIA9800075.md): Light · inoperative · Jun 26, 1998 · N17535 · Doug DC932 · Emergency Lighting
  > OKC - FLT 902 - EMERGENCY FLOOR TRACK BROKE BETWEEN ROWS 11-15. REPAIRED FLOOR TRACK AND LIGHTING IAW DC-9 MM 33-51. OPERATIONAL CHECKS GOOD. (X)
- [SDR GTIA9800020](https://openairdocs.org/sdr/GTIA9800020.md): Slide · fell off · Feb 4, 1998 · N17535 · Doug DC932 · Emergency Equipment
  > MAIN CABIN DOOR SLIDE PACK FELL OFF. REINSTALLED MAIN CABIN DOOR SLIDE IAW DC-9 MM 25-62-0, INSTALLATION CHECKS GOOD. RII ACCOMPLISHED. (M)
- [SDR GTIA9700414](https://openairdocs.org/sdr/GTIA9700414.md): Battery Pack · discharged · Dec 19, 1997 · N17535 · Doug DC932 · Emergency Lighting
  > DTW - FLT 610 - ON DAILY INSPECTION, LEFT AND RIGHT EMERGENCY NACELLE LIGHTS WOULD NOT ILLUMINATE. REPLACED LEFT AND RIGHT EMERGENCY NACELLE LIGHTS BATTERY PACKS IAW CHAPTER 33-53-0. OPS CHECK GOOD. (M)
- [SDR GTIA9700413](https://openairdocs.org/sdr/GTIA9700413.md): Slide · fell off · Dec 15, 1997 · N17535 · Doug DC932 · Emergency Equipment
  > DTW - FLT 841 - DURING DAILY INSPECTION, FOUND GALLEY DOOR EMERGENCY SLIDE HAD FALLEN OFF. INSTALLED GALLEY DOOR EMERGENCY SLIDE IAW DC9 MM 25-62-0. RII INSPECTION PERFORMED. (M)
- [SDR GTIA9700405](https://openairdocs.org/sdr/GTIA9700405.md): Fire Loop · malfunctioned · Nov 25, 1997 · N17535 · Doug DC932 · Fire Detection
  > CLIMBING THROUGH 8,000 FEET THE 'A' LOOP LIGHT CAME ON AS WELL AS THE LIGHT FOR NR 1 ENGINE, WENT TO 'B', TEST OK. GROUND OPS CHECKED NR 1 ENGINE FIRE LOOP SYSTEM IAW 26-12-0. COULD NOT DUPLICATE PROBLEM. UNIT OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME
- [SDR CALA9701119](https://openairdocs.org/sdr/CALA9701119.md): Connector · dirty · Jul 19, 1997 · N17535 · Doug DC932 · Landing Gear Position and Warning
  > THE LT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE EMERGENCY GEAR EXTENSION LEVER WAS PULLED. A TOWER FLY-BY WAS PERFORMED AND THE GEAR WAS CONFIRMED DOWN. THE AIRCRAFT LANDED WITHOU
- [SDR CALA9601424](https://openairdocs.org/sdr/CALA9601424.md): Actuator · inoperative · Oct 8, 1996 · N17535 · Doug DC932 · Landing Gear Actuator
  > WHEN GEAR WAS RETRACTED ON TAKEOFF, THE GEAR DOOR OPEN AND RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. APPROXIMATELY 15 SECONDS LATER THE SPEED BRAKE SPOILER HANDLE SOUNDED AS THOUGH IT CYCLED TO AIR MODE AND BOTH GEAR UNSAFE LIGHTS EXTINGUISHED. THE
- [SDR CAL951067](https://openairdocs.org/sdr/CAL951067.md): Latch Spring · lack of lube · Nov 26, 1995 · N17535 · Doug DC932 · Landing Gear Door Retract Section
  > FLT NR 1090 - ATL - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. THE RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT EXTINGUISHED AFTER UPLATCH CHECK. 'ABNORMAL' PROCEDURES WE
- [SDR CAL951020](https://openairdocs.org/sdr/CAL951020.md): Skin · corroded · Oct 24, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/Skin
  > HOU - INSPECTION FOUND CORROSION ON SKIN AT STA 250 BELT FRAME, LONGERON 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (X)
- [SDR CAL950991](https://openairdocs.org/sdr/CAL950991.md): Fitting · corroded · Oct 24, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND INTERGRANULAR CORROSION AT BELTFRAME STATION 832, FITTING TO RIGHT CUSP. THE FITTING WAS REPLACED IAW SRM 51-30-0. (M)
- [SDR CAL951055](https://openairdocs.org/sdr/CAL951055.md): Bulkhead · corroded · Oct 21, 1995 · N17535 · Doug DC932 · Fuselage Main, Bulkhead
  > HOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 22. (M)
- [SDR CAL951023](https://openairdocs.org/sdr/CAL951023.md): Doubler · corroded · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 218, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL951022](https://openairdocs.org/sdr/CAL951022.md): Bracket · corroded · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND CABIN FLOOR SUPPORT BRACKET AT STA 160, AND 8 INCHES - 10 INCHES, LEFT OF CENTERLINE CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-0. (X)
- [SDR CAL951021](https://openairdocs.org/sdr/CAL951021.md): Belt Frame · cracked · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, Frame
  > HOU - INSPECTION FOUND A.25 INCH CRACK COMING FROM HI-LOCK HOLE ON BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED SECTION OF BELT FRAME WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-03, FIGURE 32. (X)
- [SDR CAL950993](https://openairdocs.org/sdr/CAL950993.md): Frame · cracked · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, Frame
  > HOU - INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM FASTENER HOLE ABOVE FLOOR ON FRAME AT STATION 813. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-03. (M)
- [SDR CAL950992](https://openairdocs.org/sdr/CAL950992.md): Floor Supports · corroded · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous Structure
  > HOU - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STATION 200. THE CORROSION EXTENDED THE FULL LENGTH FROM LEFT TO RIGHT SIDE OF FUSELAGE. FOUR FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. (M)
- [SDR CAL950988](https://openairdocs.org/sdr/CAL950988.md): Frame · cracked · Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, Frame
  > HOU - INSPECTION FOUND A 3 INCH CRACK EXTENDING FROM FASTENER IN FRAME AT STATION 794, STRINGER 18L. THE FRAME WAS REPAIRED IAW SRM 53-11-3, FIGURE 1. (M)
- [SDR CAL951057](https://openairdocs.org/sdr/CAL951057.md): Skin · cracked · Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/Skin
  > HOU - INSPECTION FOUND TWO.75 INCH CRACKS AT RIVETS IN SKIN LAP AT STA 1038 ABOVE RIGHT PYLON. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)
- [SDR CAL951056](https://openairdocs.org/sdr/CAL951056.md): Skin · cracked · Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/Skin
  > HOOU - INSPECTION FOUND A.75 INCH CRACK IN SKIN LAP AT STATION 1038 ABOVE LEFT PYLON. THE SKIN CRACK WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)
- [SDR CAL951024](https://openairdocs.org/sdr/CAL951024.md): Longeron · corroded · Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > HOU - INSPECTION FOUND LONGERON 30 AT STA 218 CORRODED IN TWO. A LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02. (X)
- [SDR CAL950995](https://openairdocs.org/sdr/CAL950995.md): Longeron · cracked · Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > HOU - INSPECTION FOUND A.25 INCH CRACK IN LONGERON 8L AT STATION 446. THE LONGERON WAS REPAIRED IAW SRM 53-02. (M)
- [SDR CAL951053](https://openairdocs.org/sdr/CAL951053.md): Splice · cracked · Oct 17, 1995 · N17535 · Doug DC932 · Wing Miscellaneous Structure
  > HOU - INSPECTION FOUND A 4 INCH CRACK IN LEADING EDGE SPLICE BETWEEN NR 6 AND NR 7 SLAT TRACK. THE LEADING EDGE SPLICE WAS REPAIRED IAW ECRA 5710-01701. (M)
- [SDR CAL950990](https://openairdocs.org/sdr/CAL950990.md): Le Splice · cracked · Oct 17, 1995 · N17535 · Doug DC932 · Wing Miscellaneous Structure
  > HOU - INSPECTION FOUND A 1 INCH CRACK IN LEADING EDGE SPLICE BETWEEN THE NR 3 AND NR 4 SLAT TRACK. A DOUBLER WAS INSTALLED IAW ECRA 5710-01697. (M)
- [SDR CAL950989](https://openairdocs.org/sdr/CAL950989.md): Spar Cap · corroded · Oct 17, 1995 · N17535 · Doug DC932 · Wing Spar
  > HOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M)
- [SDR CAL951054](https://openairdocs.org/sdr/CAL951054.md): Door Jamb · cracked · Oct 15, 1995 · N17535 · Doug DC932 · Fuselage Main, Bulkhead
  > HOU - INSPECTION FOUND A 2 INCH CRACK AT LEFT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03176 AND EA 653A006. (M)
- [SDR CAL950717](https://openairdocs.org/sdr/CAL950717.md): Beam · corroded · Aug 13, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous Structure
  > IAH - DURING INSPECTION, FOUND CORROSION ON LONGITUDINAL BEAM AT FORWARD AIRSTAIR CUTOUT BETWEEN STATION 160 AND 200. THE LONGITUDINAL BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-00. (M)
- [SDR CAL950716](https://openairdocs.org/sdr/CAL950716.md): Skin · cracked · Aug 13, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/Skin
  > IAH - DURING INSPECTION, FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD AIRSTAIR DOOR CUTOUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 57A. (M)
- [SDR CAL950306](https://openairdocs.org/sdr/CAL950306.md): Skin · cracked · Apr 20, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/Skin
  > IAH - A.875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 965R, THREE INCHES ABOVE L15. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B. (W)

## 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 = 'N17535' AND deregistration_id = 'N17535-2001-08-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17535-2001-08-29/reports

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