# Service difficulty reports: N911DA, cancelled Apr 25, 2022

A list on [N911DA, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N911DA-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 · 149 reports

- [SDR DALA2019071604253](https://openairdocs.org/sdr/DALA2019071604253.md): Warning System · activated · Jul 16, 2019 · N911DA · Doug MD9030 · Landing Gear Position and Warning
  > ON APPROACH AT APPOX 2000 FT AGL FOR 27L AT ATL OVER THE MARKER SELECTED GEAR HANDLE DOWN. GEAR DOOR LIGHT ILLUMINATED BUT NO GEAR EXTENSION, ALL RED. NO PIV. CYCLED THE GEAR HANDLE PRIOR TO 1000 AGL AND THE GEAR EXTENTED NORMALLY THE SECOND TIME. CONTINUED AP
- [SDR DALA2018120306998](https://openairdocs.org/sdr/DALA2018120306998.md): Detector · missing · Dec 1, 2018 · N911DA · Doug MD9030 · Landing Gear Position and Warning
  > BOTH NOSE LANDING GEAR DEBRIS DEFLECTORS ARE MISSING. BOTH NOSE GEAR DERIS DEFLECTOR CARRIED OVER TO CDL 32-37-01. REMOVED AND REPLACED RH NLG DEBRIS DEFLECTOR PER MD90 AMM32-37. LH DEBRIS DEFLECTOR DID NOT MAKE FLIGHT TO PHL. REF LOG # 4865714 FOR NEW CDL OF
- [SDR DALA2018110606477](https://openairdocs.org/sdr/DALA2018110606477.md): Floor Support · corroded · Nov 5, 2018 · N911DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > STA 190 L/H SIDE JUST INSIDE L1 DOOR FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT ANGLE. REFERENCE MD90 SRM 53-10-01 VOLUME III. (LP# 0813773)
- [SDR DALA2018031301584](https://openairdocs.org/sdr/DALA2018031301584.md): Web · damaged · Mar 12, 2018 · N911DA · Doug MD9030 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB WEB AT STA YV 157.7 LEFT SIDE NEAR STAB SCREWJACK HAS DAMAGE. REPAIR PER ERA 566268-14 REV ORG.
- [SDR DALA2018031001547](https://openairdocs.org/sdr/DALA2018031001547.md): Channel · cracked · Mar 9, 2018 · N911DA · Doug MD9030 · Vertical Stabilizer
  > CHANNEL CRACKED AROUND JACKSCREW.
- [SDR DALA2018030301348](https://openairdocs.org/sdr/DALA2018030301348.md): Floorboard · delaminated · Feb 8, 2018 · N911DA · Doug MD9030 · Fuselage Floor Panel
  > DELAMINATED FLOORBOARD IN THE FORWARD GALLEY. A NEW FLOORBOARD WAS INSTALLED DURING C-CHECK ON N/R 302.
- [SDR DALA2017070205199](https://openairdocs.org/sdr/DALA2017070205199.md): Sign · missing · Jun 29, 2017 · N911DA · Doug MD9030 · Emergency Lighting
  > EXIT SIGN MISSING ABOVE L2 DOOR. FOUND WIRE L982214 OFF T-STRIP. INSTALLED EXIT SIGN IAW DWG 5963985-1. OPERATION CHECKS GOOD.
- [SDR DALA2017050503670](https://openairdocs.org/sdr/DALA2017050503670.md): Fuse · inoperative · May 4, 2017 · N911DA · Doug MD9030 · Emergency Lighting
  > L1 AND R1 DOOR EMERGENCY EXIT ARROW LIGHTS INOPERATIVE. REMOVED AND REPLACED FUSES. OPERATION CHECKED GOOD.
- [SDR DALA2017062204922](https://openairdocs.org/sdr/DALA2017062204922.md): Access Panel · cracked · Apr 18, 2017 · N911DA · Doug MD9030 · Wing, Plate/Skin
  > CRACK ON OUTBOARD FORWARD CORNER OF FUELING PANEL. REPAIRED IAW PRI/ERA 559426-14.
- [SDR DALA2017020100922](https://openairdocs.org/sdr/DALA2017020100922.md): Skin · damaged · Jan 31, 2017 · N911DA · Doug MD9030 · Vertical Stabilizer, Plate/Skin
  > LEFT VERTICAL STABILIZER FOUND SECOND HOLE FROM BOTTOM DAMAGED. REPAIRED IAW ERA 554885-14D.
- [SDR DALA2017013100921](https://openairdocs.org/sdr/DALA2017013100921.md): Spring · out of position · Jan 30, 2017 · N911DA · Doug MD9030 · Aerodynamic Fairings
  > TAIL CONE LEFT UPPER LOCKING SPADE HAS SPRING OUR OF POSITION. REPOSITIONED SPRING IAW MM.
- [SDR DALA2017013100852](https://openairdocs.org/sdr/DALA2017013100852.md): Cable · out of position · Jan 30, 2017 · N911DA · Doug MD9030 · Aerodynamic Fairings
  > TAIL CONE CABLE TOO CLOSE TO CONDUIT. ADJUSTED CONDUIT IAW MM.
- [SDR DALA2016030101593](https://openairdocs.org/sdr/DALA2016030101593.md): Structure · cracked · Feb 28, 2016 · N911DA · Doug MD9030 · Vertical Stabilizer
  > VERTICAL STABILIZER L/E FORWARD TIP HAS CRACK THRU FASTENER HOLE APPROXIMATELY, BS 1460. REPAIRED IAW SRM 55-30-05, FIG 19.
- [SDR DALA2016022401386](https://openairdocs.org/sdr/DALA2016022401386.md): Oil System · leaking · Feb 21, 2016 · N911DA · Doug MD9030 · Turbine Engine Oil System
  > UPON ENGINE SHUTDOWN, GROUND CREW REPORTED EXCESSIVE SMOKE COMING FROM NR 1 ENGINE TAIL PIPE. MAINTENANCE TROUBLESHOT. FOUND TURBINE EXHAUST BLADES WET WITH OIL. OIL BEGINNING TO POOL. IAW PROPULSION ENGINEERING CHANGE NR 1 OIL QUANTITY TRANSMITTER AND NR
- [SDR DALA2016030401662](https://openairdocs.org/sdr/DALA2016030401662.md): Frame · corroded · Feb 19, 2016 · N911DA · Doug MD9030 · Fuselage Main, Frame
  > FRAME CORRODED AT BS 1344, LONGERON 28R. REPAIRED IAW SRM 53-10-02, FIG 2.
- [SDR DALA2016022101279](https://openairdocs.org/sdr/DALA2016022101279.md): Spar · cracked · Feb 18, 2016 · N911DA · Doug MD9030 · Wing Spar
  > UPPER DIAMOND DOUBLER CRACKED ON OTBD EDGE AT REAR SPAR, LT WING. REPAIRED CRACK IAW SRM 51-10-03, FIG 3 AND PRI 543919-14, REV O.
- [SDR DALA2016022101389](https://openairdocs.org/sdr/DALA2016022101389.md): Bottle · low · Feb 17, 2016 · N911DA · Doug MD9030 · Escape Slide
  > L1 DOOR SLIDE PRESSURE LOW. R & R SLIDE.
- [SDR DALA2016021701170](https://openairdocs.org/sdr/DALA2016021701170.md): Skin · cracked · Feb 14, 2016 · N911DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > AIRCRAFT SKIN HAS 2.75" LONG CRACKS AT ADJACENT RIVETS IN CANTED FRAME AT BS 1531, OTBD OF AIRSTAIR CUTOUT, LT EDGE.
- [SDR DALA2016021401169](https://openairdocs.org/sdr/DALA2016021401169.md): Bulkhead · damaged · Feb 13, 2016 · N911DA · Doug MD9030 · Fuselage Main, Bulkhead
  > APB 2 FASTENERS FOUND ON APB SPLICE LOWER SIDE BETWEEN L26R AND L27R. REPAIRED IAW ERA 543286-14, REV O.
- [SDR DALA2016021401168](https://openairdocs.org/sdr/DALA2016021401168.md): Bulkhead · damaged · Feb 13, 2016 · N911DA · Doug MD9030 · Fuselage Main, Bulkhead
  > APB, 2 FASTENERS FOUND ON APB SPLICE LOWER SIDE BETWEEN L26L AND L27L. REPAIRED IAW ERA 543286-14, REV O.
- [SDR DALA2016021001245](https://openairdocs.org/sdr/DALA2016021001245.md): Longeron · corroded · Feb 10, 2016 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > LONGERON, BS 1344-1366, L28R CORRODED. REPAIRED IAW SRM 53-10-01, PARA 6.
- [SDR DALA2016021001188](https://openairdocs.org/sdr/DALA2016021001188.md): Longeron Splice · corroded · Feb 10, 2016 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > BS 1328-1344, LONGERON SPLICE AT 29R CORRODED. FABRICATED SPLICE IAW SRM 53-10-01, FIG 7.
- [SDR DALA2016021001187](https://openairdocs.org/sdr/DALA2016021001187.md): Longeron · corroded · Feb 10, 2016 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > BS 1355-1366, LONGERON 27R CORRODED. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2016021001186](https://openairdocs.org/sdr/DALA2016021001186.md): Skin · corroded · Feb 10, 2016 · N911DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN PILLOWED AT BS 1328-1344, LONGERON 29R. REPAIRED IAW SRM 53-31-04, FIG 4.
- [SDR DALA2016011100228](https://openairdocs.org/sdr/DALA2016011100228.md): Door Frame · cracked · Jan 6, 2016 · N911DA · Doug MD9030 · Fuselage Main, Structure
  > CRACK FOUND AT RT MLG WHEEL WELL OPENING FORWARD JAMB. INSTALLED NEW DOOR JAMB IAW ERA 542843-14, REV 1. CHECKS OK.
- [SDR DALA2015030902005](https://openairdocs.org/sdr/DALA2015030902005.md): Slide · no test · Mar 9, 2015 · N911DA · Doug MD9030 · Escape Slide
  > L1 DOOR FAILED DOOR SLIDE DEPLOYMENT, SYSTEM OPS CHECK FORECAST 92-0525-8-0006. LP 1853787.
- [SDR DALA2014091405035](https://openairdocs.org/sdr/DALA2014091405035.md): Light · sparks · Sep 10, 2014 · N911DA · Doug MD9030 · Passenger Compartment Lighting
  > FLIGHT CREW REPORTED THAT SIDEWALL LIGHTS AT ROW 32A WERE SPARKING. MAINTENANCE R & R LIGHT ASSEMBLY IAW AMM.
- [SDR DALA14014309211](https://openairdocs.org/sdr/DALA14014309211.md): Skin · corroded · Feb 28, 2014 · N911DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN BETWEEN FS 826-845, LONGERON 28-29R HAS CORROSION UNDER RUBSTRIP. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW ERA 520314-14, REV O.
- [SDR DALA14013869211](https://openairdocs.org/sdr/DALA14013869211.md): Pan · corroded · Feb 26, 2014 · N911DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > FORWARD CABIN FLOOR FOUND CORROSION ON FLOOR PAN, BS 200-215, RBL 15-25. CUTOUT DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 51-10-03, 51-30-05, AND 51-30-02.
- [SDR DALA14013929211](https://openairdocs.org/sdr/DALA14013929211.md): Frame · corroded · Feb 24, 2014 · N911DA · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME DOUBLER, BS 1364, L29L, CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-05, 51-10-03, 53-10-02.
- [SDR DALA14013449211](https://openairdocs.org/sdr/DALA14013449211.md): Frame · corroded · Feb 24, 2014 · N911DA · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME DOUBLER BS 1364, L29L. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-02, 51-30-02, AND 51-3-10-05.
- [SDR DALA14012059211](https://openairdocs.org/sdr/DALA14012059211.md): Beam · corroded · Feb 21, 2014 · N911DA · Doug MD9030 · Fuselage Main, Structure
  > AFT CARGO DOOR FRAME BEAM CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED DOOR FRAME BEAM IAW SRM 51-30-05, 51-30-02 AND DWG 5936038.
- [SDR DALA14012049211](https://openairdocs.org/sdr/DALA14012049211.md): Skin · corroded · Feb 20, 2014 · N911DA · Doug MD9030 · Fuselage Main, Plate/Skin
  > CENTER WING UPPER EXTERNAL SKIN, BS 953 XCW 58.6 RIGHT HAS CORROSION. REMOVED CORROSION. ALODINED, FLAP PEENED REWORKED AREA IAW ERA 520317-14, REV 1.
- [SDR DALA14010989211](https://openairdocs.org/sdr/DALA14010989211.md): Beam · corroded · Feb 17, 2014 · N911DA · Doug MD9030 · Fuselage Main, Structure
  > MID CARGO DOOR FRAME BEAM CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER AND SPACER IAW SRM 53-60-02.
- [SDR DALA14010199211](https://openairdocs.org/sdr/DALA14010199211.md): Stiffener · debonded · Feb 16, 2014 · N911DA · Doug MD9030 · Fuselage Floor Panel
  > MAIN CABIN LEFT FORWARD OTBD FLOOR PANEL HAS A DEBONDED STIFFNER. REPAIRED STIFFNER IAW ERA 417243-14MA.
- [SDR DALA14013879211](https://openairdocs.org/sdr/DALA14013879211.md): Web · corroded · Feb 15, 2014 · N911DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN, BS 180-200, RBL 10-43 WEB CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 51-10-01, 51-10-05, & 51-30-02.
- [SDR DALA14010979211](https://openairdocs.org/sdr/DALA14010979211.md): Longeron · corroded · Feb 15, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 28R JUST FORWARD OF TIE. CUT OUT DAMAGE. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-01, 51-10-03 AND 53-10-01.
- [SDR DALA14010969211](https://openairdocs.org/sdr/DALA14010969211.md): Longeron · corroded · Feb 15, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 27R BETWEEN BS 1379-1395. CUT OUT DAMAGED SECTION. FABRICATED NEW LONGERON SECTION IAW SRM 53-10-01, 41-30-05, AND 51-30-02.
- [SDR DALA14010239211](https://openairdocs.org/sdr/DALA14010239211.md): Longeron · corroded · Feb 13, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29R, BETWEEN BS 1379-1395, REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-30-02, 51-10-05 AND 53-10-01, PARA 4, FIG 7.
- [SDR DALA14014349211](https://openairdocs.org/sdr/DALA14014349211.md): Longeron Splice · corroded · Feb 11, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON SPLICE 29R BETWEEN BS 1328 AND 1344. REMOVED LONGERON SPLICE. FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 53-10-01, 51-10-03 AND 51-01-00.
- [SDR DALA14010109211](https://openairdocs.org/sdr/DALA14010109211.md): Longeron · corroded · Feb 11, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 28R, BS 1393. R & R LONGERON IAW SRM 51-30-05 AND DWG 5936667.
- [SDR DALA14010099211](https://openairdocs.org/sdr/DALA14010099211.md): Longeron Clip · corroded · Feb 11, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON TIE, L27R, BS 1395. R & R LONGERON TIE IAW SRM 51-30-05 AND DWG 5936667.
- [SDR DALA14010089211](https://openairdocs.org/sdr/DALA14010089211.md): Longeron Clip · corroded · Feb 11, 2014 · N911DA · Doug MD9030 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON TIE, BS 1393, L29R. R & R LONGERON TIE IAW SRM 51-30-05 AND DWG 5936667, REV WB.
- [SDR DALA14014359211](https://openairdocs.org/sdr/DALA14014359211.md): Frame · corroded · Feb 10, 2014 · N911DA · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1345 BETWEEN L26-27R BOTH SIDES, TASK 53-100-16. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME IAW SRM 53-10-02.
- [SDR DALA14010269211](https://openairdocs.org/sdr/DALA14010269211.md): Doubler · corroded · Feb 9, 2014 · N911DA · Doug MD9030 · Fuselage Main, Bulkhead
  > CORROSION ON AFT SIDE OF BULKHEAD ON THE STRAP, JUST FORWARD OF APB, BL 11L - 11R. R & R DOUBLER IAW SRM 51-10-05, RIG 1 AND DWG 9915561.
- [SDR DALA14009499211](https://openairdocs.org/sdr/DALA14009499211.md): Frame · corroded · Feb 9, 2014 · N911DA · Doug MD9030 · Fuselage Main, Frame
  > CORROSION ON FRAME, BS 1344, L29L-29R. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED AND INSTALLED ANGLE IAW SRM 53-10-02, 51-10-03 AND 51-30-05.
- [SDR DALA14008429211](https://openairdocs.org/sdr/DALA14008429211.md): Seat Track · damaged · Feb 9, 2014 · N911DA · Doug MD9030 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK GOUGED AND SCRATCHED AT BS 579-646, RBL 22. BLENDED OUT GOUGES. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.
- [SDR DALA14009529211](https://openairdocs.org/sdr/DALA14009529211.md): Former · corroded · Feb 8, 2014 · N911DA · Doug MD9030 · Fuselage Main, Structure
  > CORROSION ON FORMER, BS 1307, BETWEEN L28-29R. CUT OUT DAMAGE. FABRICATED AND INSTALLED FORMER SECTION IAW SRM 53-10-02, FIG 3.
- [SDR DALA14009489211](https://openairdocs.org/sdr/DALA14009489211.md): Seat Track · corroded · Feb 8, 2014 · N911DA · Doug MD9030 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN FS 864-1079+10 CORRODED AND GOUGED AT MULTIPLE LOCATIONS, RBL 54. R & R SEAT TRACK FROM BS 856-1144, IAW SRM 53-40-01, FIG 6 AND 51-30-01.
- [SDR DALA14008469211](https://openairdocs.org/sdr/DALA14008469211.md): Support · corroded · Feb 5, 2014 · N911DA · Doug MD9030 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT BS 1269-1276 BETWEEN L29-30R,. R & R SUPPORT IAW DWG 5936071.

Next page: https://openairdocs.org/deregistered/N911DA-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 = 'N911DA' AND deregistration_id = 'N911DA-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N911DA-2022-04-25/reports

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