# Service difficulty reports: N996Z, cancelled Oct 19, 2005

A list on [N996Z, cancelled Oct 19, 2005](https://openairdocs.org/deregistered/N996Z-2005-10-19.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 3 · 101 reports

- [SDR ZW0A0109401](https://openairdocs.org/sdr/ZW0A0109401.md): Door · open · Oct 4, 2001 · N996Z · Doug DC932 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION PILOT NOTED A VIBRATION IN THE NOSE GEAR AREA. CREW ACCOMPLISHED FLY BY FOR VISUAL CHECK OF NOSE AREA, THEN RETURNED TO STL. FOUND LEFT NOSE GEAR DOOR NOT MANUALLY LATCHED. SECURED DOOR AND CHECKED MANUAL LOCK OPERATION.
- [SDR TWAA0017408](https://openairdocs.org/sdr/TWAA0017408.md): Seat Track · corroded · Oct 30, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 15 MAINT CHECK IN THE COCKPIT, CORROSION WAS FOUND IN FASTENER HOLES UNDER FLOOR PANEL NUMBER 3. REMOVED CORRODED TRACK SECTION. INSTALLED NEW SEAT TRACK PER SPM 6-70-01.
- [SDR TWAA0017407](https://openairdocs.org/sdr/TWAA0017407.md): Intercostal · corroded · Oct 30, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE ELECTRONIC COMPT BETWEEN STA 200 AND 218, BL 0, INTERCOSTAL WAS CORRODED AROUND FASTENER HOLES, LEVEL NUMBER 1. SENT TO SHOP FOR FABRICATION ON INTER SHOP TICKET 875048. INSTALLED PER SRM 51-30.
- [SDR TWAA0017406](https://openairdocs.org/sdr/TWAA0017406.md): Skin · corroded · Oct 30, 2000 · N996Z · Doug DC932 · Cargo/Baggage Doors
  > DURING OP 15 MAINT CHECK THE LT FUSELAGE SKIN WAS PILLOWING AT STA 935, BETWEEN LONGERON 22 AND 23L. REPLACED FUSELAGE SKIN FROM STA 784 TO 996, LONGERON 18L TO 26L, PER DRAWING 5911423.
- [SDR TWAA0017405](https://openairdocs.org/sdr/TWAA0017405.md): Pan · corroded · Oct 30, 2000 · N996Z · Doug DC932 · Cargo/Baggage Doors
  > DURING OP 15 MAINT CHECK ON THE AFT CARGO COMPT DOOR, THE FWD LOWER DOOR PAN AT STA 889 TO 937, AND RL 24 TO RL 29, HAD CORROSION. AFT CARGO DOOR ALSO HAD CORROSION ON BOTH FWD DOOR STOP ADJUSTMENT SCREWS, THE AFT DOOR JAMB STA 917 TO 935, THE INNER DOOR JAMB
- [SDR TWAA0017404](https://openairdocs.org/sdr/TWAA0017404.md): Floorbeam · corroded · Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor Beam
  > DURING OP 15 MAINT CHECK IN THE RT AFT LAVATORY, AT STA 996 THE FLOORBEAM WAS CORRODED, 55 INCHES RBL, UNDER TOP FLANGE. FABRICATED AND INSTALLED REPAIR PER SRM 53-05, FIG 18.
- [SDR TWAA0017215](https://openairdocs.org/sdr/TWAA0017215.md): Floorbeam · corroded · Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor Beam
  > DURING OP 15 MAINT CHECK AT RT AFT LAV AT STA 996, FLOORBEAM 8 PLACES HAD CORROSION ON TOP FLANGE. REMOVED THE CORROSION PER SPM 6-80-01. FABRICATED AND REPAIRED PER SRM 53-05, FIG 108.
- [SDR TWAA0017214](https://openairdocs.org/sdr/TWAA0017214.md): Angle · cracked · Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK THE AFT PRESSURE BULKHEAD ANGLE WAS CRACKED AT FASTENER TO L/E AND FASTENERS HAD TOOLING MARKS ABOVE LT DOOR JAMB FOR AFT AIRSTAIRS. BULKHEAD SKIN WAS NOT CRACKED UNDER ANGLE PER NDT PART L 51-00-3. REMOVED OLD PART AND MADE NEW PER
- [SDR TWAA0017213](https://openairdocs.org/sdr/TWAA0017213.md): Skin · damaged · Oct 27, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK FOUND FIELD SKIN REPAIR FWD OF STA 313, RL 24 TO 25. REPAIRED PER SRM 53-04, FIG 38.
- [SDR TWAA0017212](https://openairdocs.org/sdr/TWAA0017212.md): Intercostal · corroded · Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN AFT CARGO COMPT FOUND CORROSION ON UNDER SIDE OF RL 29, STA 897 TO 917. REPLACED INTERCOSTAL PER DOUGLAS PRINT 5910158.
- [SDR TWAA0017211](https://openairdocs.org/sdr/TWAA0017211.md): Longeron · cracked · Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 15 MAINT CHECK, FOUND LONGERON 17L WAS CRACKED AT STA 945. CRACK CONFIRMED BY NDT. REPLACED CRACKED LONGERON 17L AT STA 945 WITH NEW PER SRM 53-11-3, FIG 4 SHEET 3 PAGE 14. RE-INSTALLED RIVETS PER SRM 51-30-2. REINSTALLED HI-LOK PER SRM 51-30-5.
- [SDR TWAA0017210](https://openairdocs.org/sdr/TWAA0017210.md): Seat Track · corroded · Oct 26, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 15 MAINT CHECK, FOUND CORROSION ON SEAT TRACK AT STA 200, LBL 22. REPAIRED PER 53-05, PAGE 10L, FIG 4F SHEET 6.
- [SDR TWAA0017209](https://openairdocs.org/sdr/TWAA0017209.md): Web · cracked · Oct 26, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE AFT CARGO COMPT FOUND AT STA 889, LBL 45, A WEB CRACKED UNDER CABIN FLOOR TRACK FLANGE BETWEEN TIE BOLT AND RIVET. REPAIRED PER SRM 53-01, PAGE 9. STOP DRILLED CRACK, FABRICATED, PAINTED AND INSTALLED DOUBLER.
- [SDR TWAA0017208](https://openairdocs.org/sdr/TWAA0017208.md): Floor Support · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 160, RBL 0 TO 53. FABRICATED NEW SUPPORT PER SRM 53-10-1 AND SPM 6-70-01 AND REPLACED. INSTALLED PER SRM 51-30 PAGE 18.
- [SDR WAA0017207](https://openairdocs.org/sdr/WAA0017207.md): Web · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK FOUND MEMBRANE CORRODED BETWEEN TRACKS 3 AND 4, STA 200 TO 218. REMOVED OLD MEMBRANE AND INSTALLED PER 53-01, PAGE 18. MANUFACTURED AND REPLACED PER SPM 6-70-1.
- [SDR TWAA0017206](https://openairdocs.org/sdr/TWAA0017206.md): Floorbeam · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor Beam
  > DURING OP 15 MAINT CHECK AT STA 199, BETWEEN RBL 44 AND RBL 53, THE FLOOR WEB WAS CORRODED, JUST AFT OF SERVICE DOOR. REMOVED OLD MEMBRANE AND INSTALLED PER SRM 53-01, PAGE 18.
- [SDR TWAA0017205](https://openairdocs.org/sdr/TWAA0017205.md): Floorbeam · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, Floor Beam
  > DURING OP 15 MAINT CHECK AT STA 180 BETWEEN RBL 44 AND 52, LEVEL ONE CORROSION WAS FOUND ON FLOOR WEB IN 2 LOCATIONS, WHERE FLOOR PANEL RUBBED ON WEB. REMOVED OLD WEB. MANUFACTURED NEW PER SPM 6-70-01. INSTALLED PER SRM 53-01, PAGE 18.
- [SDR TWAA0017108](https://openairdocs.org/sdr/TWAA0017108.md): Web · damaged · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FOUND REPAIR TO FLOOR MEMBRANE NEEDED REPLACEMENT AT STA 205, RBL 0 TO 20. REMOVED OLD MEMBRANE. MANUFACTURED NEW PER 6-70-01. INSTALLED PER 53-01, PAGE 18.
- [SDR TWAA0017107](https://openairdocs.org/sdr/TWAA0017107.md): Floor Support · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FOUND 37 INCHES OF FLOOR SUPPORT CORRODED BETWEEN STA 162 AND 200, RBL 43. REPLACED OLD SUPPORT WITH NEW. MADE PER SPM 6-70-1. INSTALLED PER SRM 51-30 PAGE 18.
- [SDR TWAA0017106](https://openairdocs.org/sdr/TWAA0017106.md): Floor Support · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FOUND 11 INCH LONG SECTION OF FLOOR SUPPORT CORRODED AT STA 200 BETWEEN RBL 44 AND RBL 56, JUST AFT OF SERVICE DOOR. REMOVED OLD SUPPORT. NEW SUPPORT MADE PER SPM 6-70-01 AND SRM 53-10-01. INSTALLED PER SRM 51-30 P18.
- [SDR TWAA0017105](https://openairdocs.org/sdr/TWAA0017105.md): Floor Support · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, THE FLOOR SUPPORT WAS CORRODED AT RBL 0 TO 58 STA 200, AND AT BL 0 AT STA 160 TO 237. REMOVED OLD SUPPORTS. MADE NEW SUPPORTS PER SPM 6-70-01 AND SRM 53-10-1. INSTALLED PER SRM 51-30 PAGE 18.
- [SDR TWAA0017104](https://openairdocs.org/sdr/TWAA0017104.md): Floor Panel · cracked · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Floor Panel
  > DURING OP 15 MAINT CHECK, THE AFT CABIN FLOOR PANEL NUMBER 69 HAD AFT RT CORNER CRACKED AND CORRODED. FABRICATED NEW FLOOR PANEL PER SSRM 53-00-104.
- [SDR TWAA0017103](https://openairdocs.org/sdr/TWAA0017103.md): Frame · corroded · Oct 25, 2000 · N996Z · Doug DC932 · Fuselage Main, Frame
  > DURING OP 15 MAINT CHECK, FOUND CORROSION ON FRAME AT STA 503, BETWEEN LONGERONS 28R TO 28L. REMOVED 2 FOOT SECTION OF FRAME AND INSTALLED NEW SECTION PER SRM 53-03, P4A.
- [SDR TWAA0016810](https://openairdocs.org/sdr/TWAA0016810.md): Splice · cracked · Oct 23, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK AT STA 555, LONGERON 28L, FOUND A CRACK IN LONGERON SPLICES. INSTALLED NEW SPLICE PER SRM 53-02, FIG 18.
- [SDR TWAA0016809](https://openairdocs.org/sdr/TWAA0016809.md): Seat Track · worn · Oct 22, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 15 MAINT CHECK, NUMBER 3 CHAIR TRACK HAD WORN AREA AT STA 208 AND CORROSION AT STA 214 AND 233. REMOVED OLD TRACK AND FABRICATED NEW PER SRM 53-05, SPM 6-70-01, AND INSTALLED PER SRM 51-30.
- [SDR TWAA0016808](https://openairdocs.org/sdr/TWAA0016808.md): Seat Track · corroded · Oct 22, 2000 · N996Z · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 15 MAINT CHECK, FOUND NUMBER 4 CHAIR TRACK CORRODED ON TOP BETWEEN STA 200 AND 218, RBL 44, 18 INCHES LONG. REMOVED OLD TRACK AND FABRICATED NEW TRACK PER SRM 53-05, SPM 6-70-01, AND INSTALLED PER SRM 51-30.
- [SDR TWAA0016807](https://openairdocs.org/sdr/TWAA0016807.md): Skin · dented · Oct 22, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, FOUND 3 DENTS ON FUSELAGE SKIN AT STA 207, BETWEEN LONGERON 16R AND 18R. DENTS 1 INCH BY 1.5 INCH BY 0.090 DEEP. INSTALLED FLUSH REPAIR PER SRM 53-04, FIG 33.
- [SDR TWAA0016806](https://openairdocs.org/sdr/TWAA0016806.md): Frame · cracked · Oct 20, 2000 · N996Z · Doug DC932 · Fuselage Main, Frame
  > DURING OP 15 MAINT CHECK, FORMER REPAIR WAS CRACKED APPROX 2.5 INCH LONG, APPROX 3 INCHES UNDER RL 14, STA 980. REWORKED WITH MO 72J15. REMOVED CRACKED FORMER RT SIDE AT STA 908 AND INSTALLED NEW FORMER PER MO 72J14 AND DRAWING JO60119.
- [SDR TWAA0017403](https://openairdocs.org/sdr/TWAA0017403.md): Floor Panel · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Floor Panel
  > DURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR MEMBRANE HAD CORRODED AND WORN AT STA 160 TO 200, LBL 44 INCHES. REMOVED MEMBRANE AND FABRICATED NEW PART PER DRAWING AA9910078 AND SRM 51-30-3. INSTALLED PER SRM 51-30-0 AND 51-10-4 OF SRM.
- [SDR TWAA0016412](https://openairdocs.org/sdr/TWAA0016412.md): Web · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Floor Panel
  > DURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED AND WORN AT STA 200 TO STA 160, LBL 44 TO LBL 56. REMOVED MEMBRANE AND FABRICATED NEW PART PER DRAWING 9910078 AND SRM 51-30-3. INSTALLED PER SRM 51-30-0 AND 51-10-4.
- [SDR TWAA0016411](https://openairdocs.org/sdr/TWAA0016411.md): Web · cracked · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED THROUGH AND CRACKED AT STA 160, LBL 2. REMOVED AND REPLACED PART PER DRAWING 9910078. INSTALLED PART PER SRM 51-30-0.
- [SDR TWAA0016410](https://openairdocs.org/sdr/TWAA0016410.md): Floor Support · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE FWD CABIN CORROSION WAS FOUND ON THE FLOOR SUPPORT AT STA 218, LBL 0 TO LBL 44. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER DRAWING 9910078. INSTALLED PER SRM 51-30-0 AND SRM 51-10-4.
- [SDR TWAA0016409](https://openairdocs.org/sdr/TWAA0016409.md): Floor Support · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR SUPPORT WAS CORRODED AT STA 200 TO 237, LBL 14. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078. INSTALLED PER SRM 51-30-0.
- [SDR TWAA0016408](https://openairdocs.org/sdr/TWAA0016408.md): Floor Support · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, AT LBL 56, HAD CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078. INSTALLED NEW PART PER SRM 51-30-0.
- [SDR TWAA0016407](https://openairdocs.org/sdr/TWAA0016407.md): Floor Support · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, LBL 44, WAS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER DRAWING 9910078 AND SRM 51-10-3. INSTALLED PER SRM 51-30-0 AND 51-10-2.
- [SDR TWAA0016406](https://openairdocs.org/sdr/TWAA0016406.md): Frame · corroded · Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Main, Frame
  > DURING OP 15 MAINT CHECK, THE FRAME AT THE LAST LT WINDOW, AFT SIDE OF WINDOW CUT AT STA 918 TO 935 HAD CORROSION ON THE FLOOR WEB TO FUSELAGE SKIN. CUT OUT CORROSION PART OF FLOOR WEB PER SRM 51-70-4 FIG 2. REPAIRED WEB AREA PER SRM 57-70-04 FIG 2.
- [SDR TWAA0017402](https://openairdocs.org/sdr/TWAA0017402.md): Skin · corroded · Oct 18, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK ON THE AFT FUSELAGE, LONGERON 20L TO 21L, STA 965, THE TOP AFT CORNER OF THE PRESSURE OUTFLOW CONTROL VALVE CUTOUT HAD CORROSION, 4 INCH BY 5. REPLACED THE LT FUSELAGE SKIN FROM STA 784 TO 996, LONGERON 18 TO 26L, PER DRAWING 5911423.
- [SDR TWAA0016405](https://openairdocs.org/sdr/TWAA0016405.md): Membrane · cracked · Oct 18, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, THE MEMBRANE WAS CRACKED AT STA 892, RT SIDE. INSTALLED NEW MEMBRANE PER SRM 51-01 AND SRM 51-30-02.
- [SDR TWAA0016404](https://openairdocs.org/sdr/TWAA0016404.md): Skin · broken · Oct 17, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, THE TOP AFT CORNER OF THE LEFT LAV CUTOUT WAS FOUND WITH AN EXISTING REPAIR THAT WAS LOOSE AND THE AFT CORNER OF MATERIAL ON THE LIP WAS BROKEN OFF. REPLACED THE LT FUSELAGE SKIN FROM STA 784 TO 996, LONGERON 18L TO 26L, PER DRAWING
- [SDR TWAA0016205](https://openairdocs.org/sdr/TWAA0016205.md): Clip · broken · Oct 16, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, THE TOP FWD CORNER OF THE LAVATORY SERVICE PORT CUTOUT HAD A CLIP BROKEN OFF APPROXIMATELY.75 INCH LONG. FABRICATED NEW DOUBLER AND INSTALLED PER DRAWING 5911423-99.
- [SDR TWAA0016109](https://openairdocs.org/sdr/TWAA0016109.md): Finger Doubler · cracked · Oct 16, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, THE FINGER DOUBLER WAS CRACKED OUT AT LONGERON 26L, STA 784 TO 813. FABRICATED NEW FINGER DOUBLER FROM STA 784 TO 813, LONGERON 26L PER DRAWING 5911423.
- [SDR TWAA0016110](https://openairdocs.org/sdr/TWAA0016110.md): Doubler · corroded · Oct 16, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK FOUND INTERNAL DOUBLER DAMAGED AND CORRODED AT STA 870 TO 996, LONGERON 18 TO 23L. FABRICATED NEW DOUBLER AND INSTALLED PER DRAWING 5911423-99.
- [SDR TWAA0016108](https://openairdocs.org/sdr/TWAA0016108.md): Skin · corroded · Oct 16, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, FOUND STA 965 BETWEEN LONGERON 19L AND 20L, THE AFT CORNER OF THE LAV SERVICE PORT HAD 3 IN BY 4 IN AREA OF CORNER BULGING OUT WITH RIVET HEADS STRESSED. REPLACED FUSELAGE SKIN LT FROM STA 784 TO 996 AND LONGERON 18L TO 26L PER DRAWI
- [SDR TWAA0016107](https://openairdocs.org/sdr/TWAA0016107.md): Access Panel · corroded · Oct 16, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, FOUND THE AFT LAVATORY SERVICE PANEL LT FUSELAGE LOWER FWD CORNER OF THE CUT OUT INTERIOR OF EXTERIOR DOOR COVER HAD CORROSION AND METAL WAS GAPPED BETWEEN SHEETS. REMOVED AND REPLACED FUSELAGE SKIN FROM STA 784 TO 006, LONGERON 18L
- [SDR TWAA0016012](https://openairdocs.org/sdr/TWAA0016012.md): Angle · chafed · Oct 11, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FWD OF RT WHEEL WELL, FILLET FAIRING ATTACH ANGLE WAS WORN AND CHAFED WITH HEAVY PITTING. INSTALLED ANGLE REPAIR DOUBLERS PER SRM 53-01, FIG 2. MATERIAL PER SRM 53-11-3.
- [SDR TWAA0016011](https://openairdocs.org/sdr/TWAA0016011.md): Skin · corroded · Oct 10, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 15 MAINT CHECK, FOUND CORROSION ON SKIN UNDER DOOR PAN AT STA 936, RBL 13 INCHES. REMOVED CORROSION ON SKIN UNDER DOOR PAN AT STA 936, RBL 13 INCHES, PER SPM 6-80-01. AREA ALSO PAINTED.
- [SDR TWAA0016010](https://openairdocs.org/sdr/TWAA0016010.md): Finger Doubler · misinstalled · Oct 5, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FOUND INTERCOSTAL FINGER DOUBLERS NOT PROPERLY INSTALLED AT STA 965, BETWEEN LONGERON 13R AND 14R. INSTALLED NEW FINGER DOUBLER OF 0.025 2024-T3, FILLER AND INTERNAL REPAIR DOUBLER PER SRM 53-04 PAGE 218X, FIGURE 38 SHEET 34.
- [SDR TWAA0016009](https://openairdocs.org/sdr/TWAA0016009.md): Web · corroded · Oct 5, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED 8 INCHES INBD OF FWD GALLEY DRAIN PAN STA 152, AS SEEN FROM E AND E COMPT. CUT OUT CORRODED SECTION OF MEMBRANE. MADE AND INSTALLED REPAIR MEMBRANE PER SRM 51-70-4 FIG 1. MADE AND INSTALLED FLOOR SUPPO
- [SDR TWAA0016005](https://openairdocs.org/sdr/TWAA0016005.md): Longeron · cracked · Oct 5, 2000 · N996Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 15 MAINT CHECK, FOUND LONGERON CRACKED AT STA 586, LONGERON 25R. REPLACED PART AND FASTENERS PER SRM 51-30-01 AND SPM 6-70-01.
- [SDR TWAA0016008](https://openairdocs.org/sdr/TWAA0016008.md): Floor Support · corroded · Oct 4, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 15 MAINT CHECK FOUND FLOOR SUPPORT CORRODED AT STA 148 TO 160, RBL 34 INCHES. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 PAGE 3. INSTALLED FASTENERS PER SRM 51-30-0. REF SRM 53-11-1 AND DOUGLAS PRINT 99100078.

Next page: https://openairdocs.org/deregistered/N996Z-2005-10-19/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 = 'N996Z' AND deregistration_id = 'N996Z-2005-10-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N996Z-2005-10-19/reports

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