# Service difficulty reports: N16807, cancelled Feb 7, 2012

A list on [N16807, cancelled Feb 7, 2012](https://openairdocs.org/deregistered/N16807-2012-02-07.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 · 85 reports

- [SDR CALA0100008](https://openairdocs.org/sdr/CALA0100008.md): Intercostal · corroded · Jan 8, 2001 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL AND AFT ATTACH ANGLE IN MID PIT CORRODED BETWEEN STA 709 AND 788, L27R TO L28R. THE INTERCOSTAL AND ANGLE WERE REMOVED AND A NEW INTERCOSTAL AND ANGLE WERE INSTALLED IAW SRM 51-30-2, 51-30-3, 51-30-4, AND 51-30-5.
- [SDR CALA0100002](https://openairdocs.org/sdr/CALA0100002.md): Tab · loose · Jan 1, 2001 · N16807 · Doug DC982 · Rudder, Tab Structure
  > INSPECTION FOUND RUDDER TAB T/E METAL TAB LOOSE ON RT SIDE. THE RUDDER TRIM TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-02, PARAGRAPH B & C.
- [SDR CALA0002005](https://openairdocs.org/sdr/CALA0002005.md): Skin · dented · Dec 29, 2000 · N16807 · Doug DC982 · Spoilers
  > INSPECTION FOUND RT GROUND SPOILER SKIN DENTED IN TWO PLACES ON UPPER SURFACE. THE DENTED AREAS WERE REMOVED AND DOUBLERS WERE INSTALLED IAW SRM 57-04, FIGURE 5.
- [SDR CALA0002004](https://openairdocs.org/sdr/CALA0002004.md): Doubler · gouged · Dec 29, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND REPAIR DOUBLERS AT FORWARD AND AFT LOWER CORNER OF AFT CARGO DOOR GOUGED. THE DOUBLERS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0002003](https://openairdocs.org/sdr/CALA0002003.md): Pan · cracked · Dec 29, 2000 · N16807 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A 1.25 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. THE CRACK WAS STOP DRILLED IAW EA 9-52812-A0807. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0002002](https://openairdocs.org/sdr/CALA0002002.md): Doubler · gouged · Dec 29, 2000 · N16807 · Doug DC982 · Engine Thrust Reverser
  > INSPECTION FOUND DOUBLER AT NR 2 ENGINE LOWER T/R O/B CORNER BENT AND GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-0.
- [SDR CALA0002000](https://openairdocs.org/sdr/CALA0002000.md): Pan · cracked · Dec 27, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2" CRACK IN MID CARGO DOOR OUTER PAN AT LOWER EDGE AFT STOP AREA. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01554.
- [SDR CALA0001997](https://openairdocs.org/sdr/CALA0001997.md): Skin · bulged · Dec 26, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR SKIN BULGED AT RIVET NUTS HOLDING SEAL RETAINER AROUND DOOR. THE RIVET NUTS WERE REMOVED IAW SRM 51-30-7. A DOUBLER WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND ECRA 5230-01554. RIVET NUTS WERE INSTALLED IAW SRM 51-30-7.
- [SDR CALA0001996](https://openairdocs.org/sdr/CALA0001996.md): Angle · corroded · Dec 26, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN FS 1155-1174, LBL 50 (ATTACHED TO LOWER FACE OF CUSP WEB). THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0001995](https://openairdocs.org/sdr/CALA0001995.md): Intercostal · corroded · Dec 26, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL NUTPLATE HOLES CORRODED IN MID CARGO PIT AT FS 769-788, LONGERON 27L-28L. THE INTERCOSTAL AND FITTING WERE REMOVED AND A NEW INTERCOSTAL AND FITTING WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 51-10-3.
- [SDR CALA0001994](https://openairdocs.org/sdr/CALA0001994.md): Angle · cracked · Dec 26, 2000 · N16807 · Doug DC982 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK AT AFT END UPPER SURFACE OF NR 1 PYLON ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5.
- [SDR CALA0001992](https://openairdocs.org/sdr/CALA0001992.md): Door Frame · gouged · Dec 26, 2000 · N16807 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR JAMB UPPER LATCH CUTOUT GOUGED. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0822 AND ECRA 5330-03018.
- [SDR CALA0001983](https://openairdocs.org/sdr/CALA0001983.md): Seat Track · corroded · Dec 21, 2000 · N16807 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT FS 1079-1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5 AND 51-30-1.
- [SDR CALA0001982](https://openairdocs.org/sdr/CALA0001982.md): Angle · cracked · Dec 21, 2000 · N16807 · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > INSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 23A AND 23B.
- [SDR CALA0001981](https://openairdocs.org/sdr/CALA0001981.md): Stop · corroded · Dec 21, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR STOPS NR 8, 12, AND 14 CORRODED AND WORN. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5330-02819.
- [SDR CALA0001978](https://openairdocs.org/sdr/CALA0001978.md): Cargo Track · corroded · Dec 21, 2000 · N16807 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CORROSION AT FASTENER HOLES ON UPPER AND LOWER SURFACES OF RT CARGO TRACK IN MID PIT AT STA 541-636. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.
- [SDR CALA0001975](https://openairdocs.org/sdr/CALA0001975.md): Rib · cracked · Dec 21, 2000 · N16807 · Doug DC982 · Engine Thrust Reverser
  > INSPECTION FOUND NR 2 AND 5 I/B INTERNAL RIBS OF NR 2 ENGINE UPPER T/R BUCKET CRACKED. THE CRACKS WERE 0.025" LONG. NEW RIBS WER INSTALLED IAW SRM 51-30-1.
- [SDR CALA0001974](https://openairdocs.org/sdr/CALA0001974.md): Fitting · cracked · Dec 20, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR LOWER FORWARD INNER STOP SUPPORT FITTING CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
- [SDR CALA0001973](https://openairdocs.org/sdr/CALA0001973.md): Shear Tie · cracked · Dec 20, 2000 · N16807 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 1/2 INCH CRACK IN SHEAR FOOT ON BULKHEAD FRAME AT STA 1309, L14R. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND EA 9-5314-2-A0813.
- [SDR CALA0001972](https://openairdocs.org/sdr/CALA0001972.md): Cargo Track · corroded · Dec 20, 2000 · N16807 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT AFT PIT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES AT FS 1211-1332. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-01, FIGURE 1, 51-10-4, AND 51-10-3.
- [SDR CALA0001971](https://openairdocs.org/sdr/CALA0001971.md): Spar · corroded · Dec 20, 2000 · N16807 · Doug DC982 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND RT HORIZONTAL STABILIZER FRONT BARREL NUT HOLE CORRODED AT FORWARD LOWER BOLT HOLE. THE CORROSION WAS REMOVED IAW SRM 51-10-5. THE HOLE WAS REAMED AND A BUSHING WAS INSTALLED IAW EA 9-5511-2-A0815 AND ECRA 5511-01037.
- [SDR CALA0001970](https://openairdocs.org/sdr/CALA0001970.md): Web · corroded · Dec 20, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP WEB CORRODED FROM FS 1117-1174 FORWARD OF L-2 DOOR. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0001963](https://openairdocs.org/sdr/CALA0001963.md): Support · bent · Dec 19, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CENTER SUPPORT IN AFT PIT BENT AT BULKHEAD, STA 1003, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-3, AND 51-10-4.
- [SDR CALA0001962](https://openairdocs.org/sdr/CALA0001962.md): Angle · corroded · Dec 19, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT LT CARGO TRACK, FS 522 FALSE BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR CALA0001961](https://openairdocs.org/sdr/CALA0001961.md): Angle · corroded · Dec 19, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-ANGLE CORRODED IN AFT PIT BETWEEN STA 1136 AND 1155, LBL 50. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5.
- [SDR CALA0001959](https://openairdocs.org/sdr/CALA0001959.md): Skin · cracked · Dec 19, 2000 · N16807 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-34-0, FIGURE 7.
- [SDR CALA0001958](https://openairdocs.org/sdr/CALA0001958.md): Skin · cracked · Dec 19, 2000 · N16807 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND TWO 1 INCH CRACKS IN TAIL COMPARTMENT SKIN AT STA 1485 JUST FORWARD OF RUDDER TRIM ACTUATOR. THE DOUBLER AND ATTACH BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-34-0, FIGURE 7.
- [SDR CALA0001948](https://openairdocs.org/sdr/CALA0001948.md): Seat Track · corroded · Dec 18, 2000 · N16807 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 352-457. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, 51-10-3, 51-30-1, AND 51-30-5.
- [SDR CALA0001947](https://openairdocs.org/sdr/CALA0001947.md): Angle · cracked · Dec 18, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT ANGLE IN AFT PIT AT STA 1003, LBL 12. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 53-01, FIGURE 2, 53-14-3, FIGURE 5, 51-10-3, AND 51-30-2.
- [SDR CALA0001945](https://openairdocs.org/sdr/CALA0001945.md): Pan · cracked · Dec 18, 2000 · N16807 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND AN 8 INCH CRACK IN LT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER AND SHEAR CLIP WERE INSTALLED IAW EA 9-5281-2-A0807 AND SRM 51-10-3.
- [SDR CALA0001944](https://openairdocs.org/sdr/CALA0001944.md): Bracket · cracked · Dec 18, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 0.030 INCH CRACK IN SUPPORT BRACKET IN AFT PIT AT FORWARD BULKHEAD, STA 1003, LBL 10. THE SUPPORT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0001943](https://openairdocs.org/sdr/CALA0001943.md): Skin · dented · Dec 18, 2000 · N16807 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT SIDE OF AFT ENTRANCE AIRSTAIR DOOR EXTERIOR SKIN DENTED. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 51-30-2, 51-30-1, AND 52-01, FIGURE 2, SHEET 3.
- [SDR CALA0001942](https://openairdocs.org/sdr/CALA0001942.md): Channel · cracked · Dec 18, 2000 · N16807 · Doug DC982 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND TWO EACH 0.075 INCH CRACKS IN RT HORIZONTAL STABILIZER AFT SPAR HAT SECTION CHANNEL. THE HAT SECTION CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001932](https://openairdocs.org/sdr/CALA0001932.md): Seat Track · corroded · Dec 16, 2000 · N16807 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 427-925. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIGURE 4B.
- [SDR CALA0001931](https://openairdocs.org/sdr/CALA0001931.md): Skin · dented · Dec 16, 2000 · N16807 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 190, L21R. THE SKIN WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, AND 51-30-2.
- [SDR CALA0001928](https://openairdocs.org/sdr/CALA0001928.md): Floor Panel · bent · Dec 16, 2000 · N16807 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN RT O/B FLOOR PANEL BENT AT FS 465-541 AND AT FS 541-617. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-24-0, 53-01, 51-30-2, 51-30-3, AND 51-30-4.
- [SDR CALA0001927](https://openairdocs.org/sdr/CALA0001927.md): Pan · cracked · Dec 15, 2000 · N16807 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A 1.25 INCH CRACK IN LT I/B MLG DOOR AFT LOWER PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 28. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.
- [SDR CALA0001926](https://openairdocs.org/sdr/CALA0001926.md): Pan · cracked · Dec 15, 2000 · N16807 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND TWO 1/2 INCH CRACKS IN RT MLG I/B DOOR FORWARD LOWER PAN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5280-01254, 51-10-3, 51-30-2, AND EA 9-5281-2-A0808.
- [SDR CALA0001923](https://openairdocs.org/sdr/CALA0001923.md): Skin · corroded · Dec 15, 2000 · N16807 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD EDGE OF AFT CARGO DOOR SKIN CORRODED AT CENTER FITTING. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05,51-10-6, AND 51-30-2.
- [SDR CALA0001922](https://openairdocs.org/sdr/CALA0001922.md): Frame · corroded · Dec 15, 2000 · N16807 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT FS 1193, LONGERON 30, IN AFT PIT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, 51-30-1, AND 51-30-2.
- [SDR CALA0001921](https://openairdocs.org/sdr/CALA0001921.md): Expansion Joint · cracked · Dec 15, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND EXPANSION JOINTS CRACKED AND BUCKLED AT CABIN FLOOR PANEL CNTER STA 886-939. THE EXPANSION JOINTS WERE REMOVED AND NEW EXPANSION JOINTS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.
- [SDR CALA0001918](https://openairdocs.org/sdr/CALA0001918.md): Floorbeam · gouged · Dec 14, 2000 · N16807 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LOWER SIDE OF MAIN DECK FLOORBEAM GOUGED AT STA 1174, RBL 4 AND AT STA 1193, RBL 4. REPAIRS WERE PERFORMED AT EACH LOCATION IAW SRM 53-05, FIGURE 86, 51-10-3, 51-30-1, AND 51-30-5.
- [SDR CALA0001917](https://openairdocs.org/sdr/CALA0001917.md): Web · cracked · Dec 14, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1/4 INCH CRACK IN TANG ON TORQUE BOX WEB AT STA 220 AFT OF L-1 DOOR, LONGERON 15L. A DOUBLER WAS INSTALLED IAW EA 9-5314-2-A0811 AND SRM 51-30-5.
- [SDR CALA0001916](https://openairdocs.org/sdr/CALA0001916.md): Floor Support · corroded · Dec 14, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT SERVICE DOOR ENTRYWAY FLOOR SUPPORT CORRODED AT FS 1155 BETWEEN LT CENTER AND O/B SEAT TRACKS, LBL 44-54.
- [SDR CALA0001903](https://openairdocs.org/sdr/CALA0001903.md): Floor Support · corroded · Dec 12, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-1.
- [SDR CALA0001902](https://openairdocs.org/sdr/CALA0001902.md): Floorbeam · corroded · Dec 12, 2000 · N16807 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LT CABIN FLOORBEAM CORRODED AROUND NUT CLIP HOLES. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 20A.
- [SDR CALA0001898](https://openairdocs.org/sdr/CALA0001898.md): Floor Support · corroded · Dec 12, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 225, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 51-10-4.
- [SDR CALA0001897](https://openairdocs.org/sdr/CALA0001897.md): Floor Support · corroded · Dec 11, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.
- [SDR CALA0001896](https://openairdocs.org/sdr/CALA0001896.md): Floor Support · corroded · Dec 11, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 195-200, LBL 55 AND AT STA 200-256, LBL 14. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, 51-30-5, AND 51-30-1.
- [SDR CALA0001895](https://openairdocs.org/sdr/CALA0001895.md): Floor Support · corroded · Dec 11, 2000 · N16807 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1309-1361. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Next page: https://openairdocs.org/deregistered/N16807-2012-02-07/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 = 'N16807' AND deregistration_id = 'N16807-2012-02-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16807-2012-02-07/reports

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