# Service difficulty reports: N963DN

A list on [N963DN](https://openairdocs.org/aircraft/N963DN.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 · 148 reports

- [SDR DALA2020080602719](https://openairdocs.org/sdr/DALA2020080602719.md): Attach Angle · cracked · Aug 5, 2020 · N963DN · Doug MD9030 · Empennage Structure
  > CRACK ON RH ATTACH ANGLE THROUGH ACCESS PANEL 370AL. NRC 00156: RH ATTACH ANGLE WAS REPLACED IAW DWG #5912188 REV BD AND MD-90 SRM 51-30-02 AND 51-30-05 VOL.II.
- [SDR DALA2020080542718](https://openairdocs.org/sdr/DALA2020080542718.md): Frame · cracked · Aug 4, 2020 · N963DN · Doug MD9030 · Fuselage Main, Frame
  > CRACK ON FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT (CAT). NRC 00251: FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER MD-90 SRM 53-10-02 FIG 1 VOL I. (LP #1589387)
- [SDR DALA2019101515905](https://openairdocs.org/sdr/DALA2019101515905.md): Pin · unsecure · Oct 11, 2019 · N963DN · Doug MD9030 · Escape Slide
  > FOUND L1 ENTRY DOOR SLIDE PACK HAD BOTH PINS FELL OUT OF SLIDE EYELETS. REMOVED AND REPLACED SLIDE PACK PER WC 2561-4641. SYS CKS OK. ACFT OK FOR SERVICE.
- [SDR DALA2019073004489](https://openairdocs.org/sdr/DALA2019073004489.md): Unknown · odor · Jul 29, 2019 · N963DN · Doug MD9030 · Air Distribution System
  > STRONG SMELL OF FUEL IN THE CABIN AFTER LANDING.THE SMELL IS STRONGER IN THE AFT CABIN, BUT IS STILL PRESENT UP TO THE FLAT DECK. INSPECTED A/C, APU, ENGINES, FUEL DRAINS. NO LEAKS FOUND. INOP APU. PERFORMED PNEU DUCT BURN OUT W/ENGINES PER AMM. 21-53-00 PG 20
- [SDR DALA2019073004487](https://openairdocs.org/sdr/DALA2019073004487.md): Attach Angle · cracked · Jul 27, 2019 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > FOUND 2" CRACK AT STRINGER 1307 JUST LEFT OF CENTER LINE. FOUND CRACK TO BE IN FLOOR PANEL TO FORMER ATTACH ANGLE SUBSTRUCTURE. FABRICATED & INSTALLED REPAIR ANGLE PER SRM 51-70-01 FIGURE 1 PAGE 2 AND 4. SECURED PANEL 181MF PER AMM 25-50. (LP# 5821591)
- [SDR DALA2019061873627](https://openairdocs.org/sdr/DALA2019061873627.md): Charger · inoperative · Jun 16, 2019 · N963DN · Doug MD9030 · Emergency Lighting
  > DURING SVC, FOUND EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT DOOR OUT. R/R BATTERY CHARGER PER MD90 AMM 33-51, OPS CHECK GOOD.
- [SDR DALA201811206695](https://openairdocs.org/sdr/DALA201811206695.md): Skin · debonded · Nov 17, 2018 · N963DN · Doug MD9030 · Vertical Stabilizer, Plate/Skin
  > FOUND VERTICAL STABILIZER PANEL 370TL LEADING EDGE DISBONDING. REMOVED PANEL 370TL AND ROUTED TO COMPOSITE SHOP. REMOVED DELAMINATED MESH AND DAMAGED PAINT IN PERPETRATION FOR REPAIR, MD90 SRM 55-41-01. REPAIRED COPPER LIGHTNING PROTECTION IAW MD90 SRM 55-41-0
- [SDR DALA201811206694](https://openairdocs.org/sdr/DALA201811206694.md): Tail Cone · lack of lube · Nov 17, 2018 · N963DN · Doug MD9030 · Aerodynamic Fairings
  > DURING OPS CHECK OF TAIL CONE DROP, AFT ENTRY DOOR DID NOT RELEASE TAIL CONE. LUBED TAIL CONE PER MD-90 AM 53-52. OPS WILL BE DONE ON AMDS 5352-7116. ALL RII COMPLIED WITH ON AMDS 5352-7116 QC2097. LUBED DOOR RELEASE CABLE PER PSM 900-8 #5. (LP# 5009704)
- [SDR DALA2018062904274](https://openairdocs.org/sdr/DALA2018062904274.md): Cable · binding · Jun 27, 2018 · N963DN · Doug MD9030 · Entrance Stairs
  > AFT VENTRAL STAIRS INOPERATIVE WILL NOT OPEN. DURING CHECKS, FOUND THE CONTROL CABLE ASSY FROM THE HANDLE BINDING IN THE OPEN DIRECTION. R & R BRACKET ASSEMBLY. REPLACED AFT VENTRAL STAIRS TELEFLEX CABLE.
- [SDR DALA2018031701777](https://openairdocs.org/sdr/DALA2018031701777.md): Bracket · cracked · Mar 16, 2018 · N963DN · Doug MD9030 · Engine Thrust Reverser
  > DURING INSPECTION, FOUND A CRACKED BRACKET ON FWD BULKHEAD AT THE RT UPPER ENGINE THRUST REVERSER. THE BRACKET WAS REPLACED.
- [SDR DALA2018031601727](https://openairdocs.org/sdr/DALA2018031601727.md): Rib · cracked · Mar 15, 2018 · N963DN · Doug MD9030 · Wing Spar
  > CRACK ON RIB OF FIXED LEADING EDGE INTERIOR SURFACE SATA XOS 530 APROX LT WING. RIB WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9919331-39 REV N.
- [SDR DALA2018031401679](https://openairdocs.org/sdr/DALA2018031401679.md): Beam · cracked · Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Main, Structure
  > CRACK RT/LT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y= 47 AT NLG. BEAM WAS REPAIRED PER SRM VOL I 53-90-01 PAR 8. (LENGHT CRACK WAS 0.500"), FOR BEAM RT WAS ISSUED A NRC SERIAL NUMBER 00982 TO SEPARATE TYPE REPAIR, REPAIRED UNDER LOG 0463002.
- [SDR DALA2018031401678](https://openairdocs.org/sdr/DALA2018031401678.md): Web · cracked · Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK ON WEB AT STA CANT Y=1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. WEB WAS REMOVED PER VOL II SRM 51-30-02 DAMAGE WAS REMOVED PER SRM 53-00-01 PAR 8 FIG 6. REPAIR PARTS WERE FABRICATED PER SRM VOL I 53-00-01 PAR 8 FIG 6. REPA
- [SDR DALA2018031401677](https://openairdocs.org/sdr/DALA2018031401677.md): Skin · cracked · Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Main, Frame
  > CRACK RT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y=47 AT NLG. REPAIRED PER REV ETI-90-18-013 REV 4 AND ER/A 566722-14 REV ORIGINAL.
- [SDR DALA2018031401676](https://openairdocs.org/sdr/DALA2018031401676.md): Intercostal · corroded · Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA Y= 163 PROTECTION LONG 28L AT INNER FUSELAGE STRUCTURE E&E COMPARTMENT AREA. REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9911549 REV D.
- [SDR DALA2018031301583](https://openairdocs.org/sdr/DALA2018031301583.md): Support · cracked · Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK ON INBD/OUTBD WEB SUPPORTS (2EAS) STA CANT 1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. ANGLES WERE REPLACE PER VOL II SRM 51-30-05 AND DWG 9923630-5 REV L AND 9911839-158 REV DP.
- [SDR DALA2018031301582](https://openairdocs.org/sdr/DALA2018031301582.md): Frame · corroded · Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME OF STA Y 1362 BTW LONGS 29R-26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 WAS REPAIRED PER SRM VOL I 53-10-02 FIG 2.
- [SDR DALA2018031301581](https://openairdocs.org/sdr/DALA2018031301581.md): Angle · cracked · Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK ON WEB ANGLE STA CANT 1542 AT 11 HRS POSITION AFT ACCESORY COMPARTMENT VENT BOX LOUVERS AREA. ANGLE WAS REPLACE PER VOL II SRM 51-30-05, SRM 51-30-01 AND 51-30-02.
- [SDR DALA2018031301580](https://openairdocs.org/sdr/DALA2018031301580.md): Angle · cracked · Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK ON AFT ACCESORY COMPARTMENT VENT BOX LOUVER UPPER ANGLE STA CANT 1520 AND 1HRS POSITION. ANGLE WAS REPLACE PER VOL II SRM 51-30-05 AND 51-30-02.
- [SDR DALA2018031201555](https://openairdocs.org/sdr/DALA2018031201555.md): Skin · cracked · Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL FUSELAGE. SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL WAS REPAIRED PER SRM VOL I 53-30-01 PAR 14, AND VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018031201554](https://openairdocs.org/sdr/DALA2018031201554.md): Longeron · cracked · Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONG 20 LT STA Y= 1050 AT LT MLG WHEEL WELL AREA. LONG 20 LT STA Y= 1050 WAS REPAIRED (CRACK 1") PER SRM VOL I 53-10-01 FIG 9.
- [SDR DALA2018031201553](https://openairdocs.org/sdr/DALA2018031201553.md): Fitting · corroded · Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON SEVERAL CLIPS FROM STA Y 1212-1269 LONG 19R AT AFT CARGO COMPARTMENT DOOR JAMB. CLIPS WERE REPLACED PER SRM VOL II 51-10-05.
- [SDR DALA2018031101551](https://openairdocs.org/sdr/DALA2018031101551.md): Longeron · corroded · Mar 10, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION LEVEL 2. CORROSION ON LONG 30 STA Y=218 AT INNER STRUCTURE E/E COMPARTMENT. LONGERON 30 BTW STA Y=160-229 WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018031001550](https://openairdocs.org/sdr/DALA2018031001550.md): Fitting · corroded · Mar 9, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON CLIP SUPPORT OF STA Y=1212 AT AFT CARGO COMPARTMENT. CLIP WAS REPLACED PER SRM VOL II 51-30-05 DWG 5936660 REV BZ.
- [SDR DALA2018031001549](https://openairdocs.org/sdr/DALA2018031001549.md): Fitting · corroded · Mar 9, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED FITTING SUPPORT STA Y=932, X=0 AT WING CENTER SECTION KEEL BEAM AREA. FITTING WAS REPLACED PER SRM VOL II 51-30-05.
- [SDR DALA2018031001548](https://openairdocs.org/sdr/DALA2018031001548.md): Doubler · cracked · Mar 9, 2018 · N963DN · Doug MD9030 · Landing Gear Doors
  > CRACKED REPAIR DOUBLER ON LOWER AFT CORNER INBD SECTION AT LH MLG INBD DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-80-02, FIG 8, SRM 51-30-01, AND 51-30-02.
- [SDR DALA2018030901511](https://openairdocs.org/sdr/DALA2018030901511.md): Angle · cracked · Mar 8, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING INSPECTION. A CRACKED ANGLE BS 1364, LONGERON 16R. REPLACED THE ANGLE IAW SRM 51-30-05.
- [SDR DALA2018030901510](https://openairdocs.org/sdr/DALA2018030901510.md): Longeron · cracked · Mar 8, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION. A CRACKED LONGERON 16L, BS 1364. THE AREA WAS REPAIRED IAW SRM 53-10-01, FIG 7.
- [SDR DALA2018030901508](https://openairdocs.org/sdr/DALA2018030901508.md): Angle · cracked · Mar 8, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING INSPECTION. FOUND A CRACKED ANGLE BS 1046, X=5 AT THE LT MLG WHEEL WELL KEEL BEAM AREA. REPAIRED IAW SRM 53-00-01, FIG 4, VOL I.
- [SDR DALA2018030801494](https://openairdocs.org/sdr/DALA2018030801494.md): Structure · damaged · Mar 7, 2018 · N963DN · Doug MD9030 · Passenger/Crew Doors
  > DURING INSPECTION, FOUND AN ELONGATED SCREW HOLE ON THE AFT UPPER CORNER OF THE L2 DOOR. REPAIRED IAW ETI-90-18-005, REV 1 AND ERA 566537-14, REV ORIGINAL.
- [SDR DALA2018030801493](https://openairdocs.org/sdr/DALA2018030801493.md): Pan · cracked · Mar 7, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND A CRACK ON THE UPPER AFT PAN BETWEEN BS 195 & 200 AT THE L1 DOOR. THE PAN WAS REPAIRED IAW ETI-90-18-007, REV. 3 AND ERA 566290-14, REV ORIGINAL.
- [SDR DALA2018030701464](https://openairdocs.org/sdr/DALA2018030701464.md): Door Frame · cracked · Mar 6, 2018 · N963DN · Doug MD9030 · Fuselage Main, Structure
  > DURING INSPECTION, A CRACK WAS FOUND BEYOND A STOP DRILL ON THE AFT MLG DOOR FRAME AT THE RT MLG WW. REPAIRED IAW SRM VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018030701463](https://openairdocs.org/sdr/DALA2018030701463.md): Web · corroded · Mar 6, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE WEB AT BS 884, BETWEEN LONGERONS 28L - 28R. THE WEB WAS REPAIRED IAW ER/A 566426-14, REV ORIG, AND ETI -90-18-003, REV 2.
- [SDR DALA2018030701462](https://openairdocs.org/sdr/DALA2018030701462.md): Angle · cracked · Mar 5, 2018 · N963DN · Doug MD9030 · Fuselage Main, Structure
  > DURING INSPECTION, FOUND A CRACKED ANGLE ON THE LT MLG DOOR FWD FRAME. THE ANGLE WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2018030701461](https://openairdocs.org/sdr/DALA2018030701461.md): Doubler · corroded · Mar 5, 2018 · N963DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND CORROSION ON THE INNER PRODUCTION DOUBLER, BS 1395 BETWEEN LONGERONS 29R - 29L IN THE AFT CARGO BAY. THE DOUBLER WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2018030701459](https://openairdocs.org/sdr/DALA2018030701459.md): Angle · cracked · Mar 5, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE IN FWD OUTBD CHANNEL ON FWD RT. THE ANGLE WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2018030701458](https://openairdocs.org/sdr/DALA2018030701458.md): Angle · cracked · Mar 5, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 110, IN THE NLG W/W. THE ANGLE WAS REPLACED IAW SRM 51-30-08.
- [SDR DALA2018030501363](https://openairdocs.org/sdr/DALA2018030501363.md): Floor Panel · delaminated · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Floor Panel
  > DELAMINATION ON FLOOR PANELS NBRS 222AF, 222HG, 222LG, 222AKG, 222MF, 222RF, AND 222VF AT PAX CAB. FLOOR PANELS NBRS 222AF, 222HG, 222LG, 222AKG, 222MF, 222RF, AND 222VF WERE REPLACED FABRICATE AND IDENTIFIED PER MD-90 VOL I S.R.M. 53-20-03. (LP0450439)
- [SDR DALA2018030501362](https://openairdocs.org/sdr/DALA2018030501362.md): Floor Panel · delaminated · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Floor Panel
  > DELAMINATION ON FLOOR PANELS NBRS 221LF, 221BF, AND 221JF AT PAX CAB. FLOOR PANELS NBRS 221LF, 221BF, AND 221JF WERE REPLACED, FABRICATE AND IDENTIFIED PER MD-90 VOL 1 S.R.M. 53-20-03. (LP0450402)
- [SDR DALA2018030501361](https://openairdocs.org/sdr/DALA2018030501361.md): Floor Panel · cracked · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Floor Panel
  > CRACKS ON FLOOR PANELS NBRS 221GF, 211FG, 221PF, 211AJF 221NF, 223EF, 221QF, 222CG, 222TF AND FLOOR PANEL P/N 9981474-41 AT PAX CAB (CPAX). FLOOR PANELS NBRS 221GF, 211FG, 221PF, 211AJF 221NF, 223EF, 221QF, 222CG, 222TF AND FLOOR PANEL P/N 9981474-41 WERE REP
- [SDR DALA2018030501360](https://openairdocs.org/sdr/DALA2018030501360.md): Bracket · cracked · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION. CRACKED HYD LINE BRACKET ON LT MLG WHEEL WELL FWD DOOR JAMB. BRACKET WAS REPLACED (CRACK 2") PER VOL II SRM 51-30-02.
- [SDR DALA2018030501359](https://openairdocs.org/sdr/DALA2018030501359.md): Stiffener · corroded · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON STIFFENER OF STA Y 1395 AND LONG 30 WAS FOUND DURING REMOVAL OF INNER PRODUCTION DOUBLER OF STA Y 1395 BTW LONGS 29R-29L. STIFFENER WAS REPLACED PER VOL II SRM 51-30-05.
- [SDR DALA2018030501358](https://openairdocs.org/sdr/DALA2018030501358.md): Floor Panel · corroded · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL 160G FROM STA Y 160-200 AND STA X -54 TO -60 AT PAX CABIN. LEVEL CORROSION 2 FLOOR PANEL 160G FROM STA Y 160-200 AND STA X -54 TO -60 WAS REPLACED PER DWG 9957828 REV AB.
- [SDR DALA2018030501357](https://openairdocs.org/sdr/DALA2018030501357.md): Channel · cracked · Mar 4, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK FWD INBD JAMB OF LT MLG DOOR WHEEL WELL. CHANNEL WAS REPLACED (CRACK 1") PER SRM VOL II 51-30-02 AND 51-30-05.
- [SDR DALA2018030301354](https://openairdocs.org/sdr/DALA2018030301354.md): Splice · cracked · Mar 2, 2018 · N963DN · Doug MD9030 · Wing Miscellaneous Structure
  > CRACKED SPLICE AND CLIP ANGLE ON LT WING INTERNAL FIXED LEADING EDGE STA XFS 194. SPLICE AND CLIP WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05 AND DWG9937517 REV J.
- [SDR DALA2018030301353](https://openairdocs.org/sdr/DALA2018030301353.md): Panel Support · cracked · Mar 2, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED PANEL SUPPORTS (2EAS) STA Y=1473 X=-10 AND X=10 AT AFT ACCESSORY COMPARTMENT. PANEL SUPPORTS (BRACKETS 2EAS) STA Y=1473 X=-10 AND X=10 WERE REPLACED PER DWG 5937954 REV R.
- [SDR DALA2018030301352](https://openairdocs.org/sdr/DALA2018030301352.md): Angle · cracked · Mar 2, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED ANGLES BETWEEN BS 883, LBL 43, RBL 43, Z=-6. THE ANGLES WERE REPAIRED IAW ER/A 498192-14MA, REV A.
- [SDR DALA2018030301351](https://openairdocs.org/sdr/DALA2018030301351.md): Skin · cracked · Mar 2, 2018 · N963DN · Doug MD9030 · Engine Thrust Reverser
  > CRACKED AND LOOSE FASTENERS ON AFT BIFURCATION TRACK FAIRING SKIN OUTBOARD SIDE AT RT LOWER ENGINE THRUST REVERSER C-DUCT. DAMAGE WAS REPAIRED IAW SRM 54-30-13, VOL IV.
- [SDR DALA2018030301350](https://openairdocs.org/sdr/DALA2018030301350.md): Web · corroded · Mar 2, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BETWEEN BS 131 TO 141, RBL 30 TO 52. REPAIRED IAW. SRM 51-10-01, FIG 10.
- [SDR DALA2018030301349](https://openairdocs.org/sdr/DALA2018030301349.md): Angle · cracked · Mar 2, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED ANGLES BETWEEN BS 962, LBL 44, RBL 44, Z=-7 LT & RT SIDE AT WING BOX AREA. THE ANGLES WERE REPLACED IAW SRM 51-30-05, AND DWG 9923417-17, REV B.

Next page: https://openairdocs.org/aircraft/N963DN/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 = 'N963DN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N963DN/reports

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