# Service difficulty reports: N83870, cancelled May 15, 2006

A list on [N83870, cancelled May 15, 2006](https://openairdocs.org/deregistered/N83870-2006-05-15.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 · 72 reports

- [SDR CALA0500010](https://openairdocs.org/sdr/CALA0500010.md): Light · inoperative · Jan 14, 2005 · N83870 · Doug DC982 · Escape Slide
  > WHEN THE R-2 SERVICE DOOR SLIDE WAS DEPLOYED DURING TESTING, THE SLIDE LIGHTS FAILED TO ILLUMINATE. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED.
- [SDR CALA0400704](https://openairdocs.org/sdr/CALA0400704.md): Frame · corroded · Nov 8, 2004 · N83870 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELL FRAME CORRODED AT STA 1320 ABOVE LONGERON 30. REPAIRED BELL FRAME IAW SRM 53-03, PAGE 4A AND SRM 53-01, FIGURE 2, PAGE 3.
- [SDR CALA0400702](https://openairdocs.org/sdr/CALA0400702.md): Web · cracked · Nov 6, 2004 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 1212 ABOVE LONGERON 24R IN AFT BAGGAGE BIN, RBL 6 TO RBL 14. A PAN SECTION AND SPLICE DOUBLER WERE INSTALLED IAW ECRA 5311-01211.
- [SDR CALA0400024](https://openairdocs.org/sdr/CALA0400024.md): Frame · cracked · Jan 14, 2004 · N83870 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 5.
- [SDR CALA0400023](https://openairdocs.org/sdr/CALA0400023.md): Shear Tie · cracked · Jan 14, 2004 · N83870 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 7.
- [SDR CALA0300609](https://openairdocs.org/sdr/CALA0300609.md): Charger · inoperative · Oct 21, 2003 · N83870 · Doug DC982 · Emergency Lighting
  > EMERGENCY PATH LIGHTS INOPERATIVE FROM 6DEF THROUGH 14DEF. REMOVED AND REPLACED FORWARD BATTERY PACK CHARGER IAW MM 33-53-00.
- [SDR CALA0200314](https://openairdocs.org/sdr/CALA0200314.md): Frame · cracked · May 24, 2002 · N83870 · Doug DC982 · Fuselage Main, Frame
  > TAIL COMPARTMENT CANT CRACKED AT STATION 1416 AT L2. REPALCED CANT FRAME PER SRM 51-10-3.
- [SDR CALA0200307](https://openairdocs.org/sdr/CALA0200307.md): Frame · cracked · May 20, 2002 · N83870 · Doug DC982 · Fuselage Main, Frame
  > TAIL COMPARTMENT CANT 1474 RIGHT LOWER SIDE CRACKED AT ATTACH POINT. INSTALLED FRAME PER SRM 51-40-3 AND 51-10-3.
- [SDR CALA0200306](https://openairdocs.org/sdr/CALA0200306.md): Frame · cracked · May 20, 2002 · N83870 · Doug DC982 · Fuselage Main, Frame
  > OVERWING CABIN AREA RIGHT CENTER FUSELAGE FRAME AT STATION 905 CRACKED WHERE CABIN FLOOR BEAM ATTACHES TO FRAME. REMOVED AND REPLACED MAIN FRAME AT STATION 905 PER SRM 51-30-00.
- [SDR CALA0200300](https://openairdocs.org/sdr/CALA0200300.md): Channel · cracked · May 19, 2002 · N83870 · Doug DC982 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM CHANNEL CRACKED AT MAIN FRAM ATTACH POINT AT STATION 927 RIGHT. INSTALLED NEW FLOOR BEAM CHANNEL PER SRM 51-30-00.
- [SDR CALA0200301](https://openairdocs.org/sdr/CALA0200301.md): Pan · cracked · May 17, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD BAG BIN LOWER DOOR JAMB PAN CRACKED ON LOWER LEG STATION 393. REPAIRED LOWER DOOR JAMB PAN PER SRM 53-05 FIG 44.
- [SDR CALA0200297](https://openairdocs.org/sdr/CALA0200297.md): Angle · cracked · May 17, 2002 · N83870 · Doug DC982 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR SUPPORT AT STATION 1231 ABOVE STRINGER 26LT ABB. STOP DRILLED CRACK AND INSTALLED REPAIR PER EC/RA 5320-01263.
- [SDR CALA0200296](https://openairdocs.org/sdr/CALA0200296.md): Cargo Track · corroded · May 17, 2002 · N83870 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND NUT PLATE HOLES ON LEFT TIE DOWN RAIL AT STATION 1260 ABB. REMOVED AND REPLACED TIE DOWN RAIL PER SRM 51-10-2.
- [SDR CALA0200295](https://openairdocs.org/sdr/CALA0200295.md): Seat Track · corroded · May 16, 2002 · N83870 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD SEAT TRACK CORRODED FROM STATION 1094 THROUGHT 1215. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02.
- [SDR CALA2000287](https://openairdocs.org/sdr/CALA2000287.md): Floor Support · May 15, 2002 · N83870 · Doug DC982 · Fuselage Main, Structure
  > CORROSION ON FLOOR SUPPORT ON UNDESIDE AT STA 1211 BETWEEN STR 30 & 29R 1"X24". REPLACED FLOOR SUPPORT IAW SRM 51-30-5.
- [SDR CALA2000286](https://openairdocs.org/sdr/CALA2000286.md): Support · corroded · May 14, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR FWD GIRT LATCH SUPPORT AT STA 160 S18R, IS CORRODED. INSTALLED NEW SUPPORT IAW SRM 51-30-00.
- [SDR CALA2000285](https://openairdocs.org/sdr/CALA2000285.md): Support · corroded · May 14, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR AFT GIRT LATCH SUPPORT AT STA 190, S18R, IS CORRODED. INSTALLED NEW SUPPORT IAW SRM 51-30-00.
- [SDR CALA2000280](https://openairdocs.org/sdr/CALA2000280.md): Seat Track · corroded · May 12, 2002 · N83870 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT O/B SEAT TRACK PITTED UNDER G-2 GALLEY AT APPROXIMATELY STA 208. REPLACED O/B SECTION OF SEAT TRACK IAW SRM 53-05, FIG 4F.
- [SDR CALA2000277](https://openairdocs.org/sdr/CALA2000277.md): Floor Support · corroded · May 11, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD ENTRY CENTER FLOOR PANEL SCF01 H LT SIDE SUPPORT IS CORRODED FROM STA 160-200. REPLACED FLOOR SUPPORT IAW SRM 51-40-00.
- [SDR CALA2000276](https://openairdocs.org/sdr/CALA2000276.md): Floor Support · corroded · May 11, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD ENTRY CENTER FLOOR PANEL SCF01 H RT SIDE SUPPORT IS CORRODED 40 INCHES, STA 148-200. INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-40-00.
- [SDR CALA2000275](https://openairdocs.org/sdr/CALA2000275.md): Floor Support · corroded · May 11, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > CENTER FLOOR PANEL FWD EDGE SUPPORT AT STA 200, RBL 4 IS CORRODED. REPLACED SUPPORT IAW SRM 51-10-02.
- [SDR CALA2000274](https://openairdocs.org/sdr/CALA2000274.md): Floor Support · corroded · May 11, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > CENTER FLOOR PANEL SUPPORT AT STA 218, RBL 3 IS CORRODED. REPLACED SUPPORT IAW SRM 51-10-02.
- [SDR CALA2000273](https://openairdocs.org/sdr/CALA2000273.md): Plate · corroded · May 11, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR FLOOR SKIN BETWEEN GIRT LATCH SUPPORTS IS CORRODED. INSTALLED NEW PARTS PER SRM 51-30-00.
- [SDR CALA2000272](https://openairdocs.org/sdr/CALA2000272.md): Floor Support · May 9, 2002 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > FWD ENTRY THRESHOLD PLATE SUPPORT HAS CORROSION FROM STA 160-180 LBL-24L, 2"X24". REMOVED AND REPLACED THRESHOLD PLATE SUPPORT IAW SRM 51-10-03
- [SDR CALA0100641](https://openairdocs.org/sdr/CALA0100641.md): Battery · discharged · Jul 8, 2001 · N83870 · Doug DC982 · Emergency Lighting
  > THE OVERHEAD EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-14. THE BATTERIES IN ROW 10 OVERHEAD BIN BATTERY PACK WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA0000510](https://openairdocs.org/sdr/CALA0000510.md): Clip · out of adj · Apr 20, 2000 · N83870 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO PULL EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM THEIR RETAINING CLIPS EXCEEDED LIMITS. THE CLIPS WERE ADJUSTED AND TESTED IAW MM 53-53-00.
- [SDR CALA0000509](https://openairdocs.org/sdr/CALA0000509.md): Cable · frayed · Apr 19, 2000 · N83870 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO DROP TAIL CONE USING AFT PASSENGER ENTRANCE DOOR AND INTERIOR TAIL COMPARTMENT RELEASE HANDLE EXCEEDED LIMITS. MAINTENANCE FOUND TAIL CONE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLEY. THE CABLE ASSEMBLY WAS REPLACED IAW MM 5
- [SDR CALA0000508](https://openairdocs.org/sdr/CALA0000508.md): Door Frame · corroded · Apr 19, 2000 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON BOTTOM EDGE OF MID BAG BIN DOOR JAMB. A Z-BEAM REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA0000501](https://openairdocs.org/sdr/CALA0000501.md): Skin · worn · Apr 17, 2000 · N83870 · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND LT SIDE OF VERTICAL STABILIZER SKIN HAD A SMALL HOLE WORN INTO FORWARD LOWER EDGE OF OPENING FOR HORIZONTAL STABILIZER TRAVEL. THE WORN SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000493](https://openairdocs.org/sdr/CALA0000493.md): Skin · worn · Apr 14, 2000 · N83870 · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND RT SIDE OF VERTICAL STABILIZER SKIN WORN ALONG LOWER EDGE AT FORWARD END OF OPENING FOR HORIZONTAL STABILIZER TRAVEL. THE WORN SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801572](https://openairdocs.org/sdr/CALA9801572.md): Panel · mismanufactured · Aug 28, 1998 · N83870 · Doug DC982 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR HANDLE COULD NOT BE RAISED AFTER TAKEOFF. QRH CHECKLIST PROCEDURES WERE FOLLOWED TO NO AVAIL. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT A BURR ON CENTER INSTRUMENT PANEL CUTOUT WAS CAUSING THE
- [SDR CALA9800851](https://openairdocs.org/sdr/CALA9800851.md): Longeron · cracked · May 12, 1998 · N83870 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > TAIL COMPARTMENT STA 1418 LONG 2L AND 2R CRACKED (1). REPAIRED CRACKED LONGERON PER SRM 53-02 FIG 18.
- [SDR CALA9800850](https://openairdocs.org/sdr/CALA9800850.md): Beltframe · cracked · May 12, 1998 · N83870 · Doug DC982 · Fuselage Main, Frame
  > TAIL COMPARTMENT STA 1418 LONG 2L AND LONG 2R BELTFRAME CRACKED (3). REPAIRED BELTFRAME PER SRM 53-03 FIG 32 AND EC/RA 5310-03720.
- [SDR CALA9800848](https://openairdocs.org/sdr/CALA9800848.md): Skin · worn · May 12, 1998 · N83870 · Doug DC982 · Vertical Stabilizer
  > DORSAL FIN ATTACHMENT ANGLES FUSELAGE SKIN HAS SEVERAL OVERSIZED HOLES. REPAIRED PER EC/RA 5330-02660.
- [SDR CALA9800847](https://openairdocs.org/sdr/CALA9800847.md): Spar Cap · cracked · May 12, 1998 · N83870 · Doug DC982 · Wing Spar
  > LEFT WING LOWER SPAR CAP CRACKED 2.35 AT STA XRS 161.7. PERFORMED REPAIR PER TASK CARD 08-5700-1-0025 OP 12.
- [SDR CALA9800846](https://openairdocs.org/sdr/CALA9800846.md): Spar Cap · cracked · May 12, 1998 · N83870 · Doug DC982 · Wing Spar
  > A 1 INCH CRACK AROUND I/B HOLE ON RIGHT WING LOWER SPAR CAP. REPAIRED PER TASK CARD 08-5710-1-0020 OP 7.
- [SDR CALA9800816](https://openairdocs.org/sdr/CALA9800816.md): Support · corroded · May 7, 1998 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT SERVICE DOOR FWD ESCAPE SLIDE SUPPORT HAS CORROSION. REMOVED CORROSION. REINSTALLED SUPPORT. INSTALLED DOUBLER UNDER MOUNT PER SRM 51-30-3, 51-30-2, AND 53-01 FIG 4.
- [SDR CALA9800815](https://openairdocs.org/sdr/CALA9800815.md): Beam · cracked · May 6, 1998 · N83870 · Doug DC982 · Passenger/Crew Doors
  > MAIN CABIN DOOR NR 8 BEAM FWD END CRACKED (1). INSTALLED DOUBLER PER SRM 52-05 PG 177.
- [SDR CALA9800797](https://openairdocs.org/sdr/CALA9800797.md): Channel · corroded · May 6, 1998 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > CORRODED J-CHANNEL FORWARD ENTRY FLOOR STA 180 LBL 55. REPLACED CHANNEL PER SRM 51-30-0.
- [SDR CALA9800796](https://openairdocs.org/sdr/CALA9800796.md): Casting · corroded · May 6, 1998 · N83870 · Doug DC982 · Trailing Edge Flaps
  > LEFT WING NR 3 FLAP HINGE TOP I/B BOLT HOLE CORRODED. OPENED HOLE TO.596 TO CLEAN UP CORROSION PER OHM.
- [SDR CALA9800795](https://openairdocs.org/sdr/CALA9800795.md): Angle · corroded · May 6, 1998 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SUPPORT ANGLE ON LOWER RIGHT COCKPIT SIDEWALL AFT AT STA 146.5 RT. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-30-2.
- [SDR CALA9800794](https://openairdocs.org/sdr/CALA9800794.md): Angle · cracked · May 6, 1998 · N83870 · Doug DC982 · Passenger/Crew Doors
  > AFT ENTRY DOOR NR 3 BEAM 1.5 INCH CRACK IN RADIUS OF ATTACH ANGLE NEAR HINGE SIDE OF DOOR. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-30-2.
- [SDR CALA9800768](https://openairdocs.org/sdr/CALA9800768.md): Frame · corroded · Apr 30, 1998 · N83870 · Doug DC982 · Fuselage Main, Frame
  > AFT CARGO COMPT STA 1309 LONG 29R TO 29L HEAVY SURFACE CORROSION, BELTFRAME AND SKIN ATTACH CLIP. TRIMMED OUT CORRODED SECTION PER SRM 53-05 FIG 2A, FABRICATED AND SPLICED IN NEW BELTFRAME SECTION PER SRM 53-03 FIG 2A.
- [SDR CALA9800767](https://openairdocs.org/sdr/CALA9800767.md): Drain Pan · corroded · Apr 30, 1998 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > E AND E COMPARTMENT UPPER FLOOR STA 148 RBL 45, DRAIN LINE FITTING AREA SUB FLOOR CORROSION. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER EC/RA 5320-01210.
- [SDR CALA9800760](https://openairdocs.org/sdr/CALA9800760.md): Beam · cracked · Apr 30, 1998 · N83870 · Doug DC982 · Passenger/Crew Doors
  > MAIN CABIN DOOR NR 7 BEAM FWD END CRACKED (1). INSTALLED REPAIR ANGLE PER SRM 52-05 FIG 31.
- [SDR CALA9800766](https://openairdocs.org/sdr/CALA9800766.md): Sub Floor · corroded · Apr 29, 1998 · N83870 · Doug DC982 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION AT UNDER SIDE OF CABIN SUB FLOOR, E AND E COMPT AREA, STA 200 RBL 10, FWD SIDE OF FRAME. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLED PER SRM 53-01.
- [SDR CALA9800765](https://openairdocs.org/sdr/CALA9800765.md): Seat Track · corroded · Apr 29, 1998 · N83870 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION RIGHT OUTBOARD SEAT TRACK STA 208. FABRICATED NEW SEAT TRACK SPLICE AND INSTALLED PER SRM 53-05 FIG 4F.
- [SDR CALA9800764](https://openairdocs.org/sdr/CALA9800764.md): Pan · cracked · Apr 29, 1998 · N83870 · Doug DC982 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR PAN CRACKED (1.5) AT FWD LOWER STOP PAD. REPLACED FWD LOWER PAN ON FWD ENTRY DOOR PER SRM 51-30-2.
- [SDR CALA9800763](https://openairdocs.org/sdr/CALA9800763.md): Fitting · cracked · Apr 29, 1998 · N83870 · Doug DC982 · Passenger/Crew Doors
  > T-FITTING CRACKED (2) AT LEFT SIDE ON FORWARD SIDE IN LINE WITH LATCHING MECHANISM, AFT ENTRY DOOR. REMOVED AND REPLACED FITTING PER SRM 51-30-0.
- [SDR CALA9800762](https://openairdocs.org/sdr/CALA9800762.md): Frame · cracked · Apr 29, 1998 · N83870 · Doug DC982 · Fuselage Main, Frame
  > CANTED FRAME HAS IMPROPER STOP DRILL HOLES AT END OF CRACKS WITH CRACK GOING BEYOND DRILLED HOLES AT STA 1446 IN 8 PLACES (10 TOTAL FOR ALL CRACKS). REPLACD BELTFRAME AT STATION 1446 FROM LONG 10 LT TO 10 RT PER SRM 51-30-2.

Next page: https://openairdocs.org/deregistered/N83870-2006-05-15/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 = 'N83870' AND deregistration_id = 'N83870-2006-05-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N83870-2006-05-15/reports

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