# Service difficulty reports: N13891, cancelled May 12, 2003

A list on [N13891, cancelled May 12, 2003](https://openairdocs.org/deregistered/N13891-2003-05-12.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 · 59 reports

- [SDR CALA0100877](https://openairdocs.org/sdr/CALA0100877.md): Support · cracked · Sep 15, 2001 · N13891 · Doug DC982 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.
- [SDR CALA0001524](https://openairdocs.org/sdr/CALA0001524.md): Skin · cracked · Oct 9, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN WEB SKIN JUST FORWARD OF TRIM AT TAIL COMPARTMENT STA 1485, RT SIDE. THE AFT ACCESSORY VENT RT BOX WAS REMOVED IAW SRM 51-30-1. THE REPAIR DOUBLER WAS REMOVED AND A NEW REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53-01, F
- [SDR CALA0001523](https://openairdocs.org/sdr/CALA0001523.md): Web · corroded · Oct 9, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT STA 195, LBL 22-LBL 44. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-30-2.
- [SDR CALA0001522](https://openairdocs.org/sdr/CALA0001522.md): Beam · corroded · Oct 9, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LEFT LAV I/B FORWARD AFT BEAM ON FLOOR BENT AND CORRODED AT FORWARD END. THE LAV BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW 51-10-2, 51-10-3, AND 51-30-1.
- [SDR CALA0001507](https://openairdocs.org/sdr/CALA0001507.md): Skin · dented · Oct 6, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE LEFT FUSELAGE SKIN DENTED AT STA 389 - 436, LONGERON 22L. REPAIRED IAW ECRA 5331-01082 AND EA 9-5331-2-A0754.
- [SDR CALA0001492](https://openairdocs.org/sdr/CALA0001492.md): Web · torn · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > CUSP WEB TORN FS 214 AT RBL 10 TO RBL 14. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-30-8.
- [SDR CALA0001491](https://openairdocs.org/sdr/CALA0001491.md): Seat Track · corroded · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 TO 266. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 51-30-1, 51-30-2, 51-30-5, 53-05 FIG 4F AND 51-10-4.
- [SDR CALA0001490](https://openairdocs.org/sdr/CALA0001490.md): Skin · dented · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN DENTED AT STATION 265 AT LONGERON 20R. REWORKED DENT. FABRICATED AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND 51-30-2.
- [SDR CALA0001489](https://openairdocs.org/sdr/CALA0001489.md): Floor Support · corroded · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AT STATION 256 CENTER. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 53-14-2 FIG 4 SHEET 1.
- [SDR CALA0001488](https://openairdocs.org/sdr/CALA0001488.md): Skin · dented · Oct 5, 2000 · N13891 · Doug DC982 · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN CENTER AFT IS DENTED. REMOVED DAMAGED AREA. REPAIRED SKIN PER SRM 51-50-1 FIG 1 AND 52-05 FIG 3.
- [SDR CALA0001487](https://openairdocs.org/sdr/CALA0001487.md): Skin · dented · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > LEFT EXTERIOR SKIN DENTED AT STA 200 BETWEEN LONG 22L AND 23L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND 51-10-4.
- [SDR CALA0001486](https://openairdocs.org/sdr/CALA0001486.md): Longeron · cracked · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > TAIL COMPARTMENT STA 1446 LONG 6R IS CRACKED 1 INCH. REMOVED CRACKED LONGERON. FABRICATED AND INSTALLED NEW LONGERON PER SRM 53-02, 51-10-4 AND 51-10-3.
- [SDR CALA0001485](https://openairdocs.org/sdr/CALA0001485.md): Cargo Track · corroded · Oct 5, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > MID PIT RT AFT TRACK SECTION FORWARD END OUTBOARD EDGE CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 51-10-3, 53-01, 51-10-4, 51-30-1, AND 51-30-2.
- [SDR CALA0001432](https://openairdocs.org/sdr/CALA0001432.md): Floor Support · corroded · Sep 26, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 200 LBL 12 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 1-30-5.
- [SDR CALA0001431](https://openairdocs.org/sdr/CALA0001431.md): Floor Support · corroded · Sep 26, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 200 RBL 10 - RBL 46 FLOOR SUPPORT HAS ELONGATED HOLES AND CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5.
- [SDR CALA0001424](https://openairdocs.org/sdr/CALA0001424.md): Web · punctured · Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUB FLOOR PUNCTURED AT FS 170, RBL 15.5, 21, 26, 36, AND 41. THE PUNCTURED AREAS WERE CUT OUT IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4, 51-30-4, 51-10-3, AND 51-30-2.
- [SDR CALA0001423](https://openairdocs.org/sdr/CALA0001423.md): Web · corroded · Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT FS 1076 - 1086, RBL 58. THE FASTENERS AND FRAME FITTINGS WERE REMOVED FROM AROUND THE CORRODED AREA AND THE CORRODED AREA WAS CUT OUT. A REPAIR WEB AND FRAME FITTING WERE INSTALLED IAW SRM 51-30-2, 53-14-3, 51-10-3, AND
- [SDR CALA0001422](https://openairdocs.org/sdr/CALA0001422.md): Web · cracked · Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN CUSP WEB AT FS 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-4, AND 51-20-0.
- [SDR CALA0001426](https://openairdocs.org/sdr/CALA0001426.md): Structure · dented · Sep 18, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > UPPER AFT EMERGENCY WALKWAY DENTED AT AFT SECTION AFT OF EXIT PAINT. CUT OUT DAMAGED SECTION PER SRM 53-01 FIG 2. VERIFIED NO CRACKS PAST CUTOUT AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 2.
- [SDR CALA0001413](https://openairdocs.org/sdr/CALA0001413.md): Channel · corroded · Sep 18, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT VENTRAL DOOR THRESHOLD AREA UNDER FLOOR L-CHANNEL CORRODED AT FS 1338. SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND EA 9-5320-2-A0765.
- [SDR CALA0001401](https://openairdocs.org/sdr/CALA0001401.md): Skin · gouged · Sep 6, 2000 · N13891 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND LT WING NR 5 SLAT LOWER SKIN GOUGED AT I/B END. A DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 4, 51-10-3, AND 51-30-8.
- [SDR CALA0001396](https://openairdocs.org/sdr/CALA0001396.md): Floorbeam · corroded · Sep 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LT LAV FLOORBEAM BOLT HOLES CORRODED AT FS 1338. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-05, 51-30-02, AND EA 9-5321-2-A0762.
- [SDR CALA0001395](https://openairdocs.org/sdr/CALA0001395.md): Stop · cracked · Sep 5, 2000 · N13891 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN BOTH THE AFT AND FWD LOWER DOOR STOPS ON FWD CARGO DOOR. THE CRACKS WERE STOP DRILLED IAW SRM 52-03. DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-7, 52-03, FIGURE 8, AND ECRA 5230-01554.
- [SDR CALA0001394](https://openairdocs.org/sdr/CALA0001394.md): Web · cracked · Sep 4, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THREE.5 INCH CRACKS IN SUBFLOOR BETWEEN FS 150 AND 168, LBL 22. THE CRACKED AREA WAS REMOVED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-0.
- [SDR CALA0001463](https://openairdocs.org/sdr/CALA0001463.md): Support Bracket · chafed · Aug 30, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD FUSELAGE STATION 37 RIGHT HAND PAN SUPPORT HAS DEEP CHAFE. REMOVED AND REPLACED SUPPORT, FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 1, 51-30-2, 53-02-2 FIG 2 AND 51-10-4.
- [SDR CALA0001335](https://openairdocs.org/sdr/CALA0001335.md): Skin · damaged · Aug 28, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE EXTERIOR SKIN CREASED AT STA 218 BETWEEN LONGERON 18L AND 19L. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30, 51-30-5, AND 53-04, FIGURE 25.
- [SDR CALA0001459](https://openairdocs.org/sdr/CALA0001459.md): Seat Track · corroded · Aug 22, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > RT HAND OUTBOARD SEAT TRACKS STA 1125 - 1200 IS CORRODED OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK FROM STA 1125 - 1230 IAW SRM 53-05 FIG 4, RECEIVED SEAT TRACK ON TRAVELLER T9021, DRILLED AND LOCATED IAW SRM 51-10-4, TREATED AND PRIMED SEAT TRACK AND SPLI
- [SDR CALA0001305](https://openairdocs.org/sdr/CALA0001305.md): Web · cracked · Aug 22, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 886, RBL 44 - 45. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2A, 51-10-3, AND 51-30-2.
- [SDR CALA0001447](https://openairdocs.org/sdr/CALA0001447.md): Web · punctured · Aug 18, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > SUB FLOOR PUNCTURED APPROX FS 170 - RBL 10. CUT OUT DAMAGED AREA IAW SRM 53-01 FIG 1. FABRICATED DOUBLER IAW SRM 53-14-1 FIG 4. LOCATED AND DRILLED IAW SRM 51-30-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.
- [SDR CALA0001453](https://openairdocs.org/sdr/CALA0001453.md): Web · cracked · Aug 17, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT HAND CUSP WEB FS 245 AT RBL 44 CRACKED (.5 INCH) AND PUNCTURED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2, 51-10-3, AND 51-30-2.
- [SDR CALA0001446](https://openairdocs.org/sdr/CALA0001446.md): Web · cracked · Aug 17, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > RT SIDE CUSP WEB FS 245 APPROX RBL 44 CRACKED AND PUNCTURED. CUT OUT PUNCTURED PER SRM 53-01 FIG 2, FABBED REPAIR DOUBLER PER SRM 53-01 FIG 2, TREATED AND PRIMED PER SRM 51-10-3, INSTALLED PER SRM 51-30-2.
- [SDR CALA0001458](https://openairdocs.org/sdr/CALA0001458.md): Web · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073. TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.
- [SDR CALA0001457](https://openairdocs.org/sdr/CALA0001457.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 160 - 195 LBL 54 FLOOR SUPPORT IN FWD ENTRY IS CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT ON TRAVELLER T8983, FOUND CORROSION ON SUB FLOOR. REMOVED CORROSION IAW SRM 51-0-3, SUB FLOOR OUT OF LIMITS. SEE ATTACHED 44.0008 MAT ID 7075-T6.020/BATCH 00001
- [SDR CALA0001456](https://openairdocs.org/sdr/CALA0001456.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 148 - 200 RBL 54 FLOOR SUPPORT CORRODED BEYOND LIMITS (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW FLOOR SUPPORT TRAVELLER T9012, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, INSTALLED SUPPORT IAW SRM 51-3
- [SDR CALA0001455](https://openairdocs.org/sdr/CALA0001455.md): Web · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED, TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.
- [SDR CALA0001454](https://openairdocs.org/sdr/CALA0001454.md): Skin · gouged · Aug 15, 2000 · N13891 · Doug DC982 · Ailerons
  > RIGHT AILERON LOWER SURFACE SKIN IS GOUGED (.5 INCH) AT LEADING EDGE 18 INCHES OUTBOARD OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01, REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS
- [SDR CALA0001452](https://openairdocs.org/sdr/CALA0001452.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT STA 218 LBL 10 - RBL 10. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001451](https://openairdocs.org/sdr/CALA0001451.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED IN FORWARD ENTRY AREA STA 160 - 195 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-2, AND 51-10-03.
- [SDR CALA0001450](https://openairdocs.org/sdr/CALA0001450.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT FORWARD ENTRY STA 168 RBL 9 - RBL 43. REPLACED FLOORBEAM PER SRM 51-10-04, 51-30-03, 51-30-2, AND 51-30-5.
- [SDR CALA0001449](https://openairdocs.org/sdr/CALA0001449.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > FLOORBEAM ELONGATED HOLES AND CORROSION AT STA 160 LBL 5 - RBL 5. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED BEAM PER SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0001448](https://openairdocs.org/sdr/CALA0001448.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 148 - 200 RBL 7 FLOOR SUPPORT CORRODED OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW PART ON TRAVELLER T9013, LOCATE AND DRILL HOLES IAW SRM 51-10-4, INSTALLED FLOOR SUPPORT IAW SRM 51-30-1.
- [SDR CALA0001445](https://openairdocs.org/sdr/CALA0001445.md): Skin · gouged · Aug 15, 2000 · N13891 · Doug DC982 · Ailerons
  > RT AILERON LWR SURFACE SKIN IS GOUGED AT L/E APPROX 18 INCHES O/B OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01. REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS WITHIN LIMITS. INS
- [SDR CALA0001444](https://openairdocs.org/sdr/CALA0001444.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > STA 218 LBL 10 - RBL 10 FLOORBEAM OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-30-2, RECEIVED NEW FLOORBEAM ON T9010, LOCATED AND DRLLED IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED FLOORBEAM IAW SRM 51-30-5.
- [SDR CALA0001443](https://openairdocs.org/sdr/CALA0001443.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 195 - 200 LBL 17 FLOOR SUPPORT IS CORRODED OUT OF LIMIT (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-30-2, ROUTED TO FAB SHOP, RECEIVED NEW FLOOR SUPPORT ON TRAVELLER T8982, FINISHED FAB PER SAMPLE PER TRAVELLER T8982, INSTALLED IAW SRM 51-30-2.
- [SDR CALA0001442](https://openairdocs.org/sdr/CALA0001442.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > STA 200 LBL 5- FLOORBEAM IS CORRODED OUT OF LIMITS FWD ENTRY. REMOVED BEAM FOUND TO BE OUT OF LIMITS, FAB NEW BEAM ON T8981, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED AND INSTALLED IAW SRM 551-30-2.
- [SDR CALA0001441](https://openairdocs.org/sdr/CALA0001441.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 148 - 200 LBL 7 FLOOR SUPPORT IS CORRODED BEYOND LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT AND ROUTED TO FAB (REMOVAL PER SRM 51-30-2) RECEIVED FROM FAB-FABBED PER SAMPLE ON TRAVELLER T-8977, INSTALLED SUPPORT IAW SRM 51-30-2.
- [SDR CALA0001440](https://openairdocs.org/sdr/CALA0001440.md): Floorbeam · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor Beam
  > STA 168 LBL 16-BLL 38 FLOORBEAM HAS CORROSION FWD ENTRY. REMOVED FLOORBEAM IAW SRM 51-30-2, SENT TO FAB SHOP FOR NEW FLOORBEAM, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51
- [SDR CALA0001439](https://openairdocs.org/sdr/CALA0001439.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 160 - 195 LBL 44 FLOOR SUPPORT IS CORRODED AND HAS ELONGATED HOLES FWD ENTRY. REMOVED FLOOR IAW SRM 51-30-2, FLOOR SUPPORT, FABBED ON TRAVELLER T-8979, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED FLOOR SUPPORT IAW
- [SDR CALA0001438](https://openairdocs.org/sdr/CALA0001438.md): Floor Support · corroded · Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous Structure
  > STA 160 - 200 RBL 44 FLOOR SUPPORT OUT OF LIMITS FWD ENTRY. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-5, RECEIVED FLOOR SUPPORT FROM TRAVELER T9018, LOCATED AND DRILLED SUPPORT IAW SRM 51-10-04.
- [SDR CALA9900123](https://openairdocs.org/sdr/CALA9900123.md): Oil Syst · overserviced · Feb 14, 1999 · N13891 · Doug DC982 · APU Oil System
  > A MODERATE AMOUNT OF SMOKE APPEARED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM EWR WITH THE PNEUMATIC PRESSURE GAUGE READING 70 PSI. THE SMOKE SLOWLY DISSIPATED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOT

Next page: https://openairdocs.org/deregistered/N13891-2003-05-12/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 = 'N13891' AND deregistration_id = 'N13891-2003-05-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13891-2003-05-12/reports

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