# Service difficulty reports: N310NW, cancelled Sep 27, 2018

A list on [N310NW, cancelled Sep 27, 2018](https://openairdocs.org/deregistered/N310NW-2018-09-27.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 · 135 reports

- [SDR DALA2018080583210](https://openairdocs.org/sdr/DALA2018080583210.md): Door Frame · cracked · Jan 17, 2018 · N310NW · Airbus A320211 · Fuselage Main, Structure
  > FWD CARGO DOOR FRAME FORKS HAD OVERSIZED AND CRACKED HOLES AT FRAMES 54 - 54A. REPAIRED IAW ER/A 570292-14AD SECTION 1.
- [SDR DALA2017011100269](https://openairdocs.org/sdr/DALA2017011100269.md): Power Supply · inoperative · Jan 10, 2017 · N310NW · Airbus A320211 · Emergency Lighting
  > DURING EMERGENCY LIGHT SYSTEM TEST, FOUND RIGHT POWER SUPPLY UNIT INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY.
- [SDR DALA2016122610070](https://openairdocs.org/sdr/DALA2016122610070.md): Lamp · inoperative · Dec 24, 2016 · N310NW · Airbus A320211 · Emergency Lighting
  > RT AFT OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.
- [SDR DALA2016122610069](https://openairdocs.org/sdr/DALA2016122610069.md): Lamp · inoperative · Dec 24, 2016 · N310NW · Airbus A320211 · Emergency Lighting
  > RT FWD EMERGENCY OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.
- [SDR DALA2016121209829](https://openairdocs.org/sdr/DALA2016121209829.md): Skin · damaged · Dec 11, 2016 · N310NW · Airbus A320211 · Passenger/Crew Doors
  > EVIDENCE REWORK PASSENGER CREW DOOR 832 EXTERNAL SKIN LOCATED 15" FROM LOWER EDGE AND 30.5" FROM FWD EDGE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR 832 EXTERNAL SKIN LOCATED 15" FROM LOWER EDGE AND 30.5 FROM FWD EDGE AT AFT GALLEY A
- [SDR DALA2016120509633](https://openairdocs.org/sdr/DALA2016120509633.md): Access Panel · corroded · Dec 4, 2016 · N310NW · Airbus A320211 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANEL 640JB ON RT WING. REPLACED ACCESS PANEL 640JB ON RT WING
- [SDR DALA2016120509632](https://openairdocs.org/sdr/DALA2016120509632.md): Access Panel · corroded · Dec 4, 2016 · N310NW · Airbus A320211 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANEL 540PB FUEL TANK ON LT WING. REPLACED ACCESS PANEL 540PB ON LT WING.
- [SDR DALA2016120209623](https://openairdocs.org/sdr/DALA2016120209623.md): Skin · damaged · Dec 2, 2016 · N310NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > EXISTING REWORK ON EXTERNAL SKIN AT LOWER FUSELAGE TO FRAME 31+17" BETWEEN STRINGER 42R TO STRINGER 43R, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR31TO FR32 AND BTW STR41R TO STR 44 AT LOWER FUSELAGE AS PER SRM 53-00-11 PARAGRAPH 4 W AND FIG 238.
- [SDR DALA2016063005103](https://openairdocs.org/sdr/DALA2016063005103.md): Light · broken · Jun 28, 2016 · N310NW · Airbus A320211 · Emergency Lighting
  > ROW 7ABC EMERGENCY SEAT LIGHT INOPERATIVE, REPAIRED BROKEN.
- [SDR DALA2015050703116](https://openairdocs.org/sdr/DALA2015050703116.md): Wire · broken · May 5, 2015 · N310NW · Airbus A320211 · Light System Wiring
  > DURING NON-ROUTINE CHECK, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT SEAT ROW 7AB. T/S AND FOUND BROKEN WIRE AT CABIN SEAT ROW 7 A/B. SPLICED WIRE AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA14003343210](https://openairdocs.org/sdr/DALA14003343210.md): Wire · broken · Jan 15, 2014 · N310NW · Airbus A320211 · Light System Wiring
  > DURING CHECK, FOUND SEAT 7ABC EMERGENCY SEAT LIGHT INOPERATIVE. REPAIRED A BROKEN WIRE UNDER SEAT. FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13022183210](https://openairdocs.org/sdr/DALA13022183210.md): Wire · broken · May 11, 2013 · N310NW · Airbus A320211 · Light System Wiring
  > DURING IINSPECTION, FOUND EMERGENCY PATH LIGHT AT SEAT 6 WIRE BROKEN UNDER 6A. MX RECONNECTED WIRE AT 6A AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA12016903210](https://openairdocs.org/sdr/DALA12016903210.md): Sill · corroded · Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND FWD CARGO PIT DOOR SILL HAS CORROSION IN SEVERAL PLACES AS MARK NR 130/54. REMOVED CORROSION IAW SRM 51-74-00, NO ESTABLISH LIMITS. REMOVED DOOR SILL PLATE IAW SRM 51-42-11, FABRICATED SILL PLATE FROM MATERIAL 2024-T3.100' IAW SRM
- [SDR DALA12016693210](https://openairdocs.org/sdr/DALA12016693210.md): Floor Panel · damaged · Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DAMAGED AND DAMAGE DIM L=3" X W=2". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.
- [SDR DALA12016683210](https://openairdocs.org/sdr/DALA12016683210.md): Floor Panel · damaged · Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152QF DAMAGED WITH DIM OF DAMAGED L=2" X W=1.5". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.
- [SDR DALA12016423210](https://openairdocs.org/sdr/DALA12016423210.md): Beam · corroded · Dec 16, 2012 · N310NW · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND FWD LT OVERWING EMERGENCY EXIT DOOR CURVED BEAM HAS CORROSION. REMOVED CORROSION FROM CURVED BEAM IAW SRM 51-74-00 AND CHECK LIMITS ORIG THICK.039" AFTER REWORK.033" MAT. LOSS.006" NO ESTABLISH LIMITS IN SRM. BLENDED AREA L=5.5"
- [SDR DALA12016413210](https://openairdocs.org/sdr/DALA12016413210.md): Support Angle · corroded · Dec 16, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND LT FWD OVERWING EMERGENCY EXIT DOOR AFT VERTICAL FRAME ANGLE SUPPORT CORRODED. REMOVED VERTICAL FRAME ANGLE SUPPORT IAW SRM 51-42-11. RECEIVED NEW ANGLE SUPPORT, PN D5227905420400 BATCH NR: 0002049167. INSTALLED NEW VERTICAL FRAME AN
- [SDR DALA12016243210](https://openairdocs.org/sdr/DALA12016243210.md): Frame · corroded · Dec 13, 2012 · N310NW · Airbus A320211 · Fuselage Main, Frame
  > DURING INSPECTION, FOUND RT AFT PASSENGER DOOR SILL AFT FRAME 66, UPPER SURFACE AROUND NUT PLATE HOLES HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-74-00. DIM. L=2", W=1.3", D=.035". FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG1, SH2. ACCOMPLISHED ROTO
- [SDR DALA12016233210](https://openairdocs.org/sdr/DALA12016233210.md): Attach Fitting · chafed · Dec 13, 2012 · N310NW · Airbus A320211 · Fuselage Main, Attach Fittings
  > DURING INSPECTION, FOUND CHAFED MARK ON LT AFT PAX DOOR ASSIST CYLINDER ATTACHMENT FITTING. BLENDED OUT DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=.4", W=.2", D=.008", NO ALLOWABLE LIMITS PROVIDED. HFEC ACCOMPLISHED IAW NTM 51-10-08, NO CRACKS OR OTHER DISCRE
- [SDR DALA12016223210](https://openairdocs.org/sdr/DALA12016223210.md): Plate · damaged · Dec 13, 2012 · N310NW · Airbus A320211 · Leading Edge Devices
  > DURING INSPECTION, FOUND LT WING SLAT TRACK NR 6, CLOSING PLATE CHAFING WITH SLAT LOWER T/E. BLENDED OUT CHAFE DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=3.2", W=.25", D=.012". FOUND OUT OF LIMITS IAW SRM 57-40-00, FIG 106. ACCOMPLISHED DVI IAW NTM 51-90-00
- [SDR DALA12016283210](https://openairdocs.org/sdr/DALA12016283210.md): Rib · corroded · Dec 13, 2012 · N310NW · Airbus A320211 · Trailing Edge Flaps
  > DURING INSPECTION, FOUND LT OTBD FLAP, INBD RIB L/E HAS 2 AREAS OF PITTING AFTER RUB STRIP REMOVAL. BLENDED CORROSION IAW SRM 51-74-00, AREA L 1 =1.5" W=1.0 "D =0.028"AREA 55"W=0.070" D=0.030". ACCOMPLISHED ER/A 508976-14 REV ORIGINAL SECTION I PERMANENT REP
- [SDR DALA12016013210](https://openairdocs.org/sdr/DALA12016013210.md): Panel · cracked · Dec 12, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF CRACKED 6.0 INCHES LONG. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 L=6.0, W=.100 OUT OF LIMITS IAW 53-02-00.
- [SDR DALA12016003210](https://openairdocs.org/sdr/DALA12016003210.md): Panel · punctured · Dec 12, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162EF MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED IAW FIG 209, DIAMETER OF PUNCTURE.350 AREA (1).400 AREA (2) FOUND OUT OF LIMITS IAW SRM 53-02-00.
- [SDR DALA12015993210](https://openairdocs.org/sdr/DALA12015993210.md): Panel · damaged · Dec 12, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151HF HAS EDGE DAMAGE BEYOND ALLOWABLE LIMITS. SLOPE PANEL FABRICATED IAW 53-02-00. DAMAGE LOCATED AT EDGE OF CUTOUT 2.00" LONG W=2.0 OUT OF LIMITS IAW SRM 53-02-00.
- [SDR DALA12015983210](https://openairdocs.org/sdr/DALA12015983210.md): Floor Panel · damaged · Dec 12, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND FLOOR PANEL 241AF IS SOFT AND SPONGY. REMOVED CABIN FLOOR PANEL IAW MM 53-12-12-000-001-A. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & INSTALLED IAW AMM 53-12-12000-001-A.
- [SDR DALA12015913210](https://openairdocs.org/sdr/DALA12015913210.md): Floor Support · corroded · Dec 11, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO BAY AT FRAME 58, STR 44 BEAM HAS CORROSION. REMOVED CORROSION IAW 51-74-00. AREA MEASURES L=1.0"X W=.80"X D=.012" ORG MAT.079, NO LIMITS FOUND IN SRM. R & R BEAM AT STR 44 BETWEEN FR 58 AND 59 IAW SRM 51-42-11.
- [SDR DALA12015973210](https://openairdocs.org/sdr/DALA12015973210.md): Attach Bracket · corroded · Dec 11, 2012 · N310NW · Airbus A320211 · Fuselage Main, Attach Fittings
  > DURING INSPECTION, FOUND AFT CARGO COMPT FRAME 58, STR 36-38L, SEAL PLATE ATTACHMENT BRACKET HAS CORROSION. FOUND AFTER SEAL PLATE REMOVAL. REMOVED CORROSION IAW SRM 51-74-00 L=.600, W=.250, D=.100. ORIG MAT.120 NO LIMITS FOUND IAW SRM. REMOVED FITTING IA
- [SDR DALA12016293210](https://openairdocs.org/sdr/DALA12016293210.md): Carriage · gouged · Dec 10, 2012 · N310NW · Airbus A320211 · Trailing Edge Flaps
  > DURING INSPECTION, FOUND RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LOWER TRACK HAS GOUGE (2 EA). ACCOMPLISHED RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LWR TRACK REPAIR BY BLENDING AREA IAW SRM 51-73-00, OTBD L=1.400"W=.250"D =.003", INBD L=1.400"W=.250"D=
- [SDR DALA12015713210](https://openairdocs.org/sdr/DALA12015713210.md): Floor Panel · corroded · Dec 10, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221FF CORRODED ON LWR SURFACE 3.5" X 2.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA12015503210](https://openairdocs.org/sdr/DALA12015503210.md): Web · corroded · Dec 8, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND FORWARD CABIN RT SIDE AT FR 16 STRINGER 23 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1", W=1.3", D=.062. NO ESTABLISH LIMITS IN SRM. R & R WEB IAW SRM 51-42-11. PAINTED FASTENERS IAW SRM
- [SDR DALA12015493210](https://openairdocs.org/sdr/DALA12015493210.md): Skin · damaged · Dec 8, 2012 · N310NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND RT SIDE LOWER AFT FUSELAGE FR 69,S28-29R EXTERNAL SKIN SURFACE HAS PRE-EXISTING TOOL MARK (APPEARS TO BE FROM FASTENER REPLACEMENT). REMOVED TOOL MARKS IAW SRM 51-73-00. CHECKED DAMAGE L=.8", W=.7", D=.012". FOUND TO BE OUT OF LIMITS I
- [SDR DALA12015433210](https://openairdocs.org/sdr/DALA12015433210.md): Floor Panel · cracked · Dec 6, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221EF CRACKED 4.0" X 1.0". AND FWD UTILITY PANEL 221EF. REPLACED IAW SRM 51-72-00.
- [SDR DALA12015703210](https://openairdocs.org/sdr/DALA12015703210.md): Skin · damaged · Dec 4, 2012 · N310NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND LOWER FUSELAGE HAS LIGHTNING STRIKE ON THIRD FASTENER ON STRINGER 42R FWD OF FR 31. REMOVED FASTENER & REAMED HOLE IAW SRM 53-21-11, FIG 213. COLD WORK FASTENER HOLE IAW SRM 51-48-00. INSTALLED FASTENER IAW SRM 51-42-11. PERFORMED S
- [SDR DALA12015483210](https://openairdocs.org/sdr/DALA12015483210.md): Hinge Pin · corroded · Dec 4, 2012 · N310NW · Airbus A320211 · Spoilers
  > DURING INSPECTION, FOUND LT WING SPOILER NR 4 CENTER HINGE INBD PIN CORRODED. RECEIVED NEW CTR PIN TO BE INSTALLED ON JIC 5770-1010S-LT.
- [SDR DALA12015033210](https://openairdocs.org/sdr/DALA12015033210.md): Hinge Pin · corroded · Dec 4, 2012 · N310NW · Airbus A320211 · Spoilers
  > DURING INSPECTION, FOUND RT WING NR 5 SPOILER BOTH INBD AND OTBD CTR HINGE PIN HAS CORROSION AND THREAD DAMAGED. RECEIVED NEW CTR PINS INSTALLED ON JIC 5770-1010S-RT.
- [SDR DALA12015023210](https://openairdocs.org/sdr/DALA12015023210.md): Hinge Pin · corroded · Dec 4, 2012 · N310NW · Airbus A320211 · Spoilers
  > DURING INSPECTION, FOUND LT WING SPOILER NR 5 CENTER HINGE INBD PIN CORROD PIN INSTALLED ON JIC 5770-1010S-LT.
- [SDR DALA12015013210](https://openairdocs.org/sdr/DALA12015013210.md): Floor Panel · corroded · Dec 4, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF CORRODED 3.0" X 3.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA12015003210](https://openairdocs.org/sdr/DALA12015003210.md): Threshold · corroded · Dec 4, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND AFT CARGO THRESHOLD PANEL 152KF CORRODED.3.5 X 3.5. REPLACED AFT CARGO THRESHOLD PANEL IAW SRM 51-72-00.
- [SDR DALA12014993210](https://openairdocs.org/sdr/DALA12014993210.md): Floor Panel · corroded · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262EF WITH MULTIPLE CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014983210](https://openairdocs.org/sdr/DALA12014983210.md): Floor Panel · punctured · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL PUNCTURED 261DF 4.0" X 4.0". FABRICATED FLOOR PANEL IAW DWG.
- [SDR DALA12014973210](https://openairdocs.org/sdr/DALA12014973210.md): Floor Panel · punctured · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222CF PUNCTURED "2.5 X 3.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014963210](https://openairdocs.org/sdr/DALA12014963210.md): Floor Panel · cracked · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231YF CRACKED 7.0" LONG. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014943210](https://openairdocs.org/sdr/DALA12014943210.md): Floor Panel · corroded · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF WITH CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014773210](https://openairdocs.org/sdr/DALA12014773210.md): Floor Support · cracked · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND COCKPIT FLOOR SUPPORT BETWEEN FR 8-11 Y-765 WEB CRACKED. REMOVED WEB FROM FR8 TO FR11 Y-765 IAW SRM 51-42-11. RECEIVED NEW WEB PN D5311332220102 BATCH 2364974 AND INSTALLED NEW WEB FROM FR8 TO FR11 IAW SRM 51-42-11.
- [SDR DALA12014763210](https://openairdocs.org/sdr/DALA12014763210.md): Floor Panel · punctured · Dec 3, 2012 · N310NW · Airbus A320211 · Fuselage Floor Panel
  > DURING NON ROUTINE CHECK, FOUND AFT UTILITY FLOOR PANEL 262AB PUNCTURED 2.0" X 2.0". FABRICATED FLOOR PANEL IAW DWG.
- [SDR DALA12014433210](https://openairdocs.org/sdr/DALA12014433210.md): Panel · damaged · Dec 1, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151BF DAMAGED 4.0" X 4.0". FABRICATED SLOPE PANEL 151BF ON STAM TRAVELER T12/971271 IAW DWG 3D25-37705.
- [SDR DALA12014423210](https://openairdocs.org/sdr/DALA12014423210.md): Panel · damaged · Dec 1, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152BF DAMAGED 6.5" X 6.5". FABRICATED SLOPE PANEL 152BF ON STAM TRAVELER T12/971269 IAW DWG 3D25-37705.
- [SDR DALA12014413210](https://openairdocs.org/sdr/DALA12014413210.md): Panel · damaged · Dec 1, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152CF DAMAGED 4.0" X 5.0". FABRICATED SLOPE PANEL 152CF ON STAM TRAVELER T12/971268 IAW DWG 3D25-37705.
- [SDR DALA12014403210](https://openairdocs.org/sdr/DALA12014403210.md): Panel · damaged · Dec 1, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED 3.0" X 3.0". FABRICATED SLOPE PANEL 152EF ON STAM TRAVELER T12/971263 IAW DWG 3D25-37705.
- [SDR DALA12014393210](https://openairdocs.org/sdr/DALA12014393210.md): Panel · damaged · Dec 1, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152FF DAMAGED 5.0" X 5.0". FABRICATED SLOPE PANEL 152FF ON STAM TRAVELER T12/971261 IAW DWG 3D25-37705.

Next page: https://openairdocs.org/deregistered/N310NW-2018-09-27/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 = 'N310NW' AND deregistration_id = 'N310NW-2018-09-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N310NW-2018-09-27/reports

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