# Service difficulty reports: N960DN, cancelled Apr 25, 2022

A list on [N960DN, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N960DN-2022-04-25.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 · 126 reports

- [SDR DALA2019121807401](https://openairdocs.org/sdr/DALA2019121807401.md): O-Ring · failed · Dec 17, 2019 · N960DN · Doug MD9030 · APU Engine Fuel and Control
  > SHIP 9260 - TO IAH - DURING TAXI IN, JUST AS THE APU STARTED, GOT A STRONG FUEL ODOR IN THE CABIN TO THE COCKPIT NO FUMES SHUT DOWN THE APU ODOR DISSIPATED SLOWLY. FOUND FUEL LEAK BELOW APU AT GATE. / C/A FOUND APU FUEL CONTROL BOWL "O" RING EXPOSED & BOWL MOU
- [SDR DALA2019090905244](https://openairdocs.org/sdr/DALA2019090905244.md): Battery Pack · discharged · Sep 8, 2019 · N960DN · Doug MD9030 · Emergency Lighting
  > CABIN CEILING EMERGENCY LIGHTS AND OVERWING LIGHTS INOP. T/S PER MD 90 FIM 33-51-00-812-801 AND WDM 33-51-12. R/R BATTERY PACKS B5-228, B5-229, B5-230, AND B5-237. CK GOOD, NO FURTHER DEFECT AT THIS TIME. REF AMM 33-51. (LP# 3301082)
- [SDR DALA2019060433386](https://openairdocs.org/sdr/DALA2019060433386.md): Cable · damaged · Jun 1, 2019 · N960DN · Doug MD9030 · Aerodynamic Fairings
  > WHILE PERFORMING TAIL CONE EMERGENCY RELEASE FOUND PULL CABLE DAMAGE. R & R TAIL CONE NITROGEN EMERGENCY RELEASE PULL CABLE ON WORK CARD 5352-7116. (LP# 5618816)
- [SDR DALA2019050302785](https://openairdocs.org/sdr/DALA2019050302785.md): Bowl · unsecure · May 2, 2019 · N960DN · Doug MD9030 · APU Engine Fuel and Control
  > AT THE GATE THERE WAS A STRONG OILY/FUEL ODOR OF FUMES AFTER TURNING ON APU AIR. DEPLANED, ODOR DISSIPATED AFTER TURNING OFF APU AIR. ODOR STARTED IN THE AFT AND MOVED FORWARD. FOUND FUEL CONTROL FILTER BOWL NOT SECURED PROPERLY, INSTALLED PROPERLY WITH NO LEA
- [SDR DALA2019042402602](https://openairdocs.org/sdr/DALA2019042402602.md): Seal · leaking · Apr 24, 2019 · N960DN · Doug MD9030 · APU Engine Fuel and Control
  > AFTER LANDING IN SAT STARTED APU. AFTER STARTING APU VERY STRONG FUEL ODOR IN CABIN. UPON INSP FOUND APU HIGH PRESS FUEL FILTER BOWL SEAL LEAKING. REPLACED O RING AND PERFORMED A LEAK CHECK PER MD 90 AMM 49-32. DUCT BURNOUT TWICE. SYSTEM OPS CK GOOD AT THIS TI
- [SDR DALA2019031101611](https://openairdocs.org/sdr/DALA2019031101611.md): Unknown · odor · Mar 11, 2019 · N960DN · Doug MD9030 · Air Distribution System
  > FAINT SMELL OF ELECTRICAL SMOKE ON LANDING. INSPECTED OVERHEAD PANEL IN COCKPIT, INSPECTED TURTLE SHELL AREA, INSPECTED APU COMPARTMENT, INSPECTED 48 SECTION ACMS PACS, AND INSPECTED APU COMPARTMENT. NO OBVIOUS SIGNS OF LEAKS OR BURNED WIRES. T/S PER FIM 21-22
- [SDR DALA2018090705474](https://openairdocs.org/sdr/DALA2018090705474.md): Web · cracked · Sep 5, 2018 · N960DN · Doug MD9030 · Wing Miscellaneous Structure
  > DUE A CRACK ON WEB, REMOVE AND INSTALL JACKSCREW GIMBAL ASSEMBLY. JACKSCREW ASSY WAS REMOVED AND INSTALLED.
- [SDR DALA2018082805304](https://openairdocs.org/sdr/DALA2018082805304.md): Intercostal · corroded · Aug 27, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE INTERCOSTAL OVER LONGERON 29L, BETWEEN BS 1268 - 1288 IN THE AFT CARGO. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-05, VOL 2, AND DWG 9936632-9, REV S.
- [SDR DALA2018082865302](https://openairdocs.org/sdr/DALA2018082865302.md): Longeron · cracked · Aug 26, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 6R BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.
- [SDR DALA2018082865301](https://openairdocs.org/sdr/DALA2018082865301.md): Longeron · cracked · Aug 26, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 5R, AT BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.
- [SDR DALA2018082865300](https://openairdocs.org/sdr/DALA2018082865300.md): Intercostal · corroded · Aug 25, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE INTERCOSTAL, LONGERON 29L, BETWEEN BS 750 - 769. THE INTERCOSTAL WAS REPLACED IAW DWG 9936632, REV J, AND SRM 51-30-05, VOL II.
- [SDR DALA2018082865299](https://openairdocs.org/sdr/DALA2018082865299.md): Longeron · cracked · Aug 25, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 4R, BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.
- [SDR DALA2018082875303](https://openairdocs.org/sdr/DALA2018082875303.md): Skin · cracked · Aug 24, 2018 · N960DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > CRACK FOUND ON THE AFT ACCESSORY BAY INTERNAL SKIN AT BS 1475, BETWEEN LONGERONS 1L AND 2L. THE SKIN WAS REPAIRED IAW SRM 53-30-01, FIGURE 14, VOL I.
- [SDR DALA2018082855297](https://openairdocs.org/sdr/DALA2018082855297.md): Frame · cracked · Aug 24, 2018 · N960DN · Doug MD9030 · Fuselage Main, Frame
  > CRACKED FRAME CAP, BS 1364, LONGERONS 4R AND 8R. REPAIRED THE FRAME CAP IAW ER/A 570991-14, REV ORIGINAL, AND ETI-90-18-047, REV 1.
- [SDR DALA2018082855296](https://openairdocs.org/sdr/DALA2018082855296.md): Frame · cracked · Aug 24, 2018 · N960DN · Doug MD9030 · Fuselage Main, Frame
  > CRACKED FRAME WEB AT AFT ACCESSORY BAY, BS 1520, CANT BETWEEN 10 AND 11 HRS POSITION, WEB AND DOUBLER WERE REPLACED IAW SRM 53-10-04 FIG 12 VOL III, 51-30-2 AND 51-30-5 VOL II. (LP# 0711110)
- [SDR DALA2018082855295](https://openairdocs.org/sdr/DALA2018082855295.md): Web · cracked · Aug 24, 2018 · N960DN · Doug MD9030 · Vertical Stabilizer
  > CRACKED WEB SURROUNDING JACKSCREW ASSEMBLY, RT SIDE AT THE VERTICAL STABILIZER. THE WEB WAS REPAIRED IAW ER/A 570884-14, REV ORIGINAL, AND ETI-90-18-043, REV 1.
- [SDR DALA2018082405239](https://openairdocs.org/sdr/DALA2018082405239.md): Intercostal · corroded · Aug 23, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL LONG 28RH BTW STA 845 TO 826 AT CENTER CARGO COMPARTMENT AMDS 5330-2616 MRB 53-302-07. LEVEL COROSION 2. INTERCOSTAL LONG 28RH BTW STA 845 TO 826 AT CENTER CARGO COMPARTMENT WAS REPLACED PER MD90 SRM VOL. II 51-30-05, MD90 SRM VOL. III
- [SDR DALA2018082405238](https://openairdocs.org/sdr/DALA2018082405238.md): Frame Angle · cracked · Aug 23, 2018 · N960DN · Doug MD9030 · Fuselage Main, Frame
  > CRACKS ON AFT. ACC. COMP. FRAME CLIPS STA Y=1494 BTW LONGS. 2L AND 2R. AFT. ACC. COMP. FRAME CLIPS STA Y=1494 BTW LONGS. 2L AND 2R WERE REPLACED PER DWG 9953016 REV. AU AND MD90 VOL. II SRM 51-30-05 TOOL USED P/N: TEC6A S/N: 5233 D/D 26/OCT/18. (LP# 0709711)
- [SDR DALA2018082305218](https://openairdocs.org/sdr/DALA2018082305218.md): Access Panel · corroded · Aug 22, 2018 · N960DN · Doug MD9030 · Wing, Plate/Skin
  > CORROSION FOUND ON THE LT WING FUEL TANK ACCESS PANEL 520CT. UPPER WING ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801.
- [SDR DALA2018082305217](https://openairdocs.org/sdr/DALA2018082305217.md): Access Panel · corroded · Aug 22, 2018 · N960DN · Doug MD9030 · Wing, Plate/Skin
  > CORROSION FOUND ON THE RT WING FUEL TANK ACCESS PANEL 620CT UPPER WING ACCESS DOOR 520CT. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801, AND VERIFIED.
- [SDR DALA2018082325216](https://openairdocs.org/sdr/DALA2018082325216.md): Frame Angle · corroded · Aug 21, 2018 · N960DN · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE BS 1344 BETWEEN LONGERONS 28L AND 25R IN THE AFT CARGO. THE FRAME ANGLE WAS REPLACED IAW SRM 53-10-03, FIG 1, VOL 2, AND SRM 51-30-02, VOL 2.
- [SDR DALA2018082105169](https://openairdocs.org/sdr/DALA2018082105169.md): Rod End · corroded · Aug 20, 2018 · N960DN · Doug MD9030 · Elevator Structure
  > RUSTED ROD END, XE=82 ON THE LT ELEVATOR FRONT SPAR. THE ROD END WAS REPLACED IAW CMM 27-30-25.
- [SDR DALA2018082105168](https://openairdocs.org/sdr/DALA2018082105168.md): Skin · dented · Aug 20, 2018 · N960DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BETWEEN BS 1288 - 1307, LONGERON 29L - 29R.
- [SDR DALA2018082005150](https://openairdocs.org/sdr/DALA2018082005150.md): Cusp Web · corroded · Aug 19, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING REPAIR, FOUND CORROSION ON THE RT CUSP WEB BETWEEN BS 1155 - 1231. THE CUSP WEB WAS REPLACED IAW VOL.III SRM 53-10-03 FIG.11, VOL.I SRM 53-20-02 FIG 29, VOL.I SRM 53-20-02 FIG 12, VOL.II SRM 51-30-02, AND VOL.II SRM 51-30-05.
- [SDR DALA2018082005149](https://openairdocs.org/sdr/DALA2018082005149.md): Cusp Web · corroded · Aug 19, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > DURING REPAIR, FOUND CORROSION ON THE RT CUSP WEB BETWEEN BS 1231 - 1307. THE CUSP WEB WAS REPLACED IAW SRM 53-10-03, FIG 11, VOL III, SRM 53-20-02, FIG 29, VOL I, SRM 53-20-02, FIG 12, VOL I, SRM 51-30-02, VOL.II, SRM 51-30-05.
- [SDR DALA2018082005148](https://openairdocs.org/sdr/DALA2018082005148.md): Channel · cracked · Aug 19, 2018 · N960DN · Doug MD9030 · Wing Main, Frame Structure
  > CRACKED CHANNEL IN THE RT MLG WHEEL WELL, FWD DOOR FRAME. THE CHANNEL WAS REPLACED IAW SRM 51-30-02, VOL II, AND SRM 51-30-05, VOL II.
- [SDR DALA2018082095147](https://openairdocs.org/sdr/DALA2018082095147.md): Frame Angle · cracked · Aug 19, 2018 · N960DN · Doug MD9030 · Fuselage Main, Frame
  > CRACKED AFT ACCESSORY BAY FRAME ANGLES BS 1475, LONGERONS 16L&R AND 19 R. THE FRAME ANGLES WERE REPLACED IAW SRM 51-30-05, VOL II, AND DWG S1464575, REV A.
- [SDR DALA2018082095146](https://openairdocs.org/sdr/DALA2018082095146.md): Stiffener · cracked · Aug 19, 2018 · N960DN · Doug MD9030 · Fuselage Main, Bulkhead
  > CRACKED AFT PRESSURE BULKHEAD STIFFENER, LONGERON 1, BS 1395. THE AFT PRESSURE BULKHEAD STIFFENER WAS REPLACED IAW SRM 51-30-05, VOL.II, AND SRM 51-30-02, VOL II.
- [SDR DALA2018082085145](https://openairdocs.org/sdr/DALA2018082085145.md): Pan · cracked · Aug 17, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED INNER PAN BS 168, BEAM 4 AT FWD R1 SERVICE DOOR. THE INNER PAN WAS REPAIRED IAW SRM 52-01-01, PAR 8, FIG 9, VOL 1.
- [SDR DALA2018081705131](https://openairdocs.org/sdr/DALA2018081705131.md): Cusp Web · corroded · Aug 16, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE CUSP WEB, BS 1041 - 1063, BTW X 44 AND X 54. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 12, VOL I.
- [SDR DALA2018081705130](https://openairdocs.org/sdr/DALA2018081705130.md): Cusp Web · corroded · Aug 16, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE CUSP WEB, BS 924 - 943, X=44 AND X=54. FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, VOL 1.
- [SDR DALA2018081705129](https://openairdocs.org/sdr/DALA2018081705129.md): Cusp Web · corroded · Aug 16, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE LT CUSP WEB, BS 693 TO 703. LBL 54 AND 60. FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 11, VOL 1.
- [SDR DALA2018081705128](https://openairdocs.org/sdr/DALA2018081705128.md): Cusp Web · corroded · Aug 16, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE RT CUSP WEB, BS 712 TO 731, X=54 AND X=60. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 14, VOL I.
- [SDR DALA2018081705127](https://openairdocs.org/sdr/DALA2018081705127.md): Cusp Web · corroded · Aug 16, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORRODED CUSP WEB, BS 826 TO 864, LBL 44 AND 54, FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 11, VOL I.
- [SDR DALA2018081605104](https://openairdocs.org/sdr/DALA2018081605104.md): Intercostal · cracked · Aug 16, 2018 · N960DN · Doug MD9030 · Passenger/Crew Doors
  > CRACKED INTERCOSTAL BS 185 BETWEEN BEAMS 4-5, IN THE FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED SRM 51-30-02, AND 51-30-05, VOL II.
- [SDR DALA2018081505095](https://openairdocs.org/sdr/DALA2018081505095.md): Longeron · cracked · Aug 15, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 6L, BS 1364. THE LONGERON WAS REPAIRED SRM 53-10-01, FIG 7, VOL I.
- [SDR DALA2018081505094](https://openairdocs.org/sdr/DALA2018081505094.md): Longeron · cracked · Aug 15, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 5L, BS 1364. REPAIRED IAW SRM 53-10-01, FIG 7, VOL I.
- [SDR DALA2018081505093](https://openairdocs.org/sdr/DALA2018081505093.md): Web · cracked · Aug 15, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED INTERNAL WEB BS 171 IN BEAM 3 AT THE L1 DOOR. THE WEB WAS REPAIRED IAW SRM 52-00-01.
- [SDR DALA2018081505092](https://openairdocs.org/sdr/DALA2018081505092.md): Skin · dented · Aug 15, 2018 · N960DN · Doug MD9030 · Fuselage Main, Plate/Skin
  > DENT FOUND ON A PREVIOUS REPAIR, BS 236 BETWEEN LONGERONS 17L & 18L IN THE FUSELAGE SKIN. THE SKIN WAS REPLACED IAW SRM 53-30-01, FIG 8B, VOL I.
- [SDR DALA2018081505091](https://openairdocs.org/sdr/DALA2018081505091.md): Floor Support · cracked · Aug 15, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 1328 - 1344. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-05 VOL. II.
- [SDR DALA2018081405061](https://openairdocs.org/sdr/DALA2018081405061.md): Cusp Web · corroded · Aug 14, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE CUSP WEB, BS 864 TO 880, BETWEEN X=44 AND X=54. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 9, VOL II.
- [SDR DALA2018081405060](https://openairdocs.org/sdr/DALA2018081405060.md): Pan · cracked · Aug 13, 2018 · N960DN · Doug MD9030 · Cargo/Baggage Doors
  > AFTER REMOVAL OF STOP FITTING NR 4, ONE CRACK WAS FOUND ON THE PAN AT THE MID CARGO DOOR FWD EDGE. THE PAN WAS REPAIRED IAW SRM 52-30-02, FIG 2, VOL I.
- [SDR DALA2018081305046](https://openairdocs.org/sdr/DALA2018081305046.md): Floor Support · corroded · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE FLOOR SUPPORT RBL 54, BS 160 - 198. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-02, VOL II, AND SRM 51-30-05, VOL II.
- [SDR DALA2018081305045](https://openairdocs.org/sdr/DALA2018081305045.md): Pan · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Main, Structure
  > CRACKED RT RING PAN, BS 845. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.
- [SDR DALA2018081305044](https://openairdocs.org/sdr/DALA2018081305044.md): Pan · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Main, Structure
  > CRACKED LT RING PAN, BS 1079, 1098, 1117, AND 1136. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.
- [SDR DALA2018081305043](https://openairdocs.org/sdr/DALA2018081305043.md): Pan · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Main, Structure
  > CRACKED RT RING PAN AT BS 1155, 1174, 1231, 1250, AND 1288. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.
- [SDR DALA2018081305042](https://openairdocs.org/sdr/DALA2018081305042.md): Floor Support · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BL 0, BTW BS 1344 & 1364. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-03, VOL III.
- [SDR DALA2018081305041](https://openairdocs.org/sdr/DALA2018081305041.md): Support · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ON THE LT TUNNEL BETWEEN BS 76 AND 69 WITHIN THE NLG WHEEL WELL. THE SUPPORT WAS REPLACED IAW SRM 51-30-05, VOL.
- [SDR DALA2018081305040](https://openairdocs.org/sdr/DALA2018081305040.md): Longeron · cracked · Aug 12, 2018 · N960DN · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 2R, BS 575. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, VOL I.
- [SDR DALA201808135038](https://openairdocs.org/sdr/DALA201808135038.md): Cusp Web · corroded · Aug 11, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE RT CUSP WEB, BS 756, RBL 54 - 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 18, VOL. I.

Next page: https://openairdocs.org/deregistered/N960DN-2022-04-25/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 = 'N960DN' AND deregistration_id = 'N960DN-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N960DN-2022-04-25/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.