# Service difficulty reports: N955DL, cancelled Apr 25, 2022

A list on [N955DL, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N955DL-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 · 102 reports

- [SDR DALA2019080604590](https://openairdocs.org/sdr/DALA2019080604590.md): Turbine · damaged · Aug 5, 2019 · N955DL · Doug MD88 · Turbine Section
  > RETURNED TO DEPARTURE FOR ENGINE FAILURE. CREW REPORTED AT 3800' HEARD A COMPRESSOR STALL AND RIGHT ENGINE PARAMETERS ROLLED BACK AND EGT CLIMBED. FOLLOWED THE QRH AND SHUT DOWN THE RIGHT ENGINE. EMERGENCY DECLARED. MAINTENANCE FOUND TURBINE DAMAGE AND THE RIG
- [SDR DALA2019070303994](https://openairdocs.org/sdr/DALA2019070303994.md): Door · damaged · Jul 3, 2019 · N955DL · Doug MD88 · Electrical/Electronic Compartment Doors
  > E/E DOOR HAS 9 1/2" CREASE IN IT. RT EDGE OFF DOOR IS CATCHING AIRCRAFT SKIN WHEN OPENING AND CLOSING. R/R E/E DOOR PER AMM 52-43. NO DAMAGE ON AIRCRAFT SKIN. (LP5926825)
- [SDR DALA2019040302117](https://openairdocs.org/sdr/DALA2019040302117.md): Battery Pack · inoperative · Apr 3, 2019 · N955DL · Doug MD88 · Emergency Lighting
  > FWD OVERWING EXIT LIGHT ABOVE LT TRT OVERWING EXITS INOP. REPLACED BATTERIES FOR THE FWD OVER EXIT SIGNS PER MD88 AMM 35-53. CKS GOOD. (LP5797649)
- [SDR DALA2019030601487](https://openairdocs.org/sdr/DALA2019030601487.md): Connector · defective · Mar 6, 2019 · N955DL · Doug MD88 · Light System Wiring
  > 16D EMERGENCY LIGHT INOP. R/R LIGHT CONNECTOR AT 16D PER SWPM 20-31. OPS CHECK GOOD OK FOR SVC. R/R LIGHT CONNECTOR AT 16D PER SWPM 20-31. OPS CHECK GOOD OK FOR SVC. (LP5741945)
- [SDR DALA2019010700054](https://openairdocs.org/sdr/DALA2019010700054.md): Fitting · cracked · Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, Frame
  > LWR LEFT FRAME CLIP CRACKED 7:00 POSITION CANTED FRAME 1510. R/R DAMAGE CLIP. (LP0892190)
- [SDR DALA2019010700053](https://openairdocs.org/sdr/DALA2019010700053.md): Frame · cracked · Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, Frame
  > AFT FRAME 1510 NALIGHMENT PIN HOLES CRACKED/MISSING MATERIAL LWR RIGHT FRAME 4 PLACES 5:30, 5:00, 3:30, 2:30. REMOVED BOTTOM LOWER RIGHT FRAME, DRILLED AND BEGAN INSTALLATION OF NEW FRAME PER BAC DWG 5966769 FINISHED INSTALL OF FRAME PER BAC DWG 5966769. (LP08
- [SDR DALA2019010700052](https://openairdocs.org/sdr/DALA2019010700052.md): Frame · cracked · Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, Frame
  > UPPER FRAME POWERPACK MOUNT CANTED FRAME CRACKED LWR I/B BOLT 2 OCLOCK POSITION FRAME 1510. REMOVED DAMAGE UPPER CANTED FRAME AT STA 1510. DRILLED UP NEW CANTED FRAME PER BAC DWG 5966768 INSTALLED CANTED FRAME PER BAC DWG 5966768. (LP0892161)
- [SDR DALA2019010300017](https://openairdocs.org/sdr/DALA2019010300017.md): Battery · discharged · Jan 3, 2019 · N955DL · Doug MD88 · Emergency Lighting
  > AFT OVER WING EXIT SIGN LIGHTS ON BOTH LEFT AND RIGHT SIDE ARE INOP. FOUND NO VOLTAGE AT BATTERY PACK IN OVERHEAD BIN 25E,D. REPLACED BATTERY IN BATTERY PACK. PER AMM 33-53. BOTH LEFT AND RIGHT EXIT SIGNS WORK GOOD. LP5057498)
- [SDR DALA2018110106378](https://openairdocs.org/sdr/DALA2018110106378.md): Skin · corroded · Oct 30, 2018 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN/STA 464 / BETWEEN L-29L AND L-30 / CORROSION. ER/A 561921-14 REV B - PERMANENT REPAIR RESTRICTION = REPAIR MUST BE REACCOMPLISHED PER SECTION II. INSTRUCTIONS NOT MORE THAN 24 MONTHS OF SERVICE AFTER SECTION I REPAIR. APPROVAL IS LIMITED TO 24 MO
- [SDR DALA2018082205194](https://openairdocs.org/sdr/DALA2018082205194.md): Slide · low pressure · Aug 21, 2018 · N955DL · Doug MD88 · Escape Slide
  > FOUND L2 DOOR SLIDE PRESSURE WAS BELOW LIMITS. REMOVED AND REPLACED THE SLIDE IAW WORK CARD 2561-4002, AND AMDS 2561-4002 440684.
- [SDR DALA2018031701738](https://openairdocs.org/sdr/DALA2018031701738.md): Channel · cracked · Mar 17, 2018 · N955DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RT FWD MLG WELL CHANNEL CRACKED FOUND ON SVC CHECK. FND CRACKS IN RT WHEEL WELL 1", 3.5" &3" CORNER CHANNEL BY SERVICING DOOR. REF TOP PARA XB2- ENGINEERING HAS EVALUATED & FINDS ACCEPTABLE FOR FERRY FLIGHT, PER ENGINEERING STOPPED DRILLED CRACKED. A/C TO FER
- [SDR DALA2018021600964](https://openairdocs.org/sdr/DALA2018021600964.md): Battery Pack · inoperative · Feb 16, 2018 · N955DL · Doug MD88 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS ROWS 22 TO 26 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK B5104 IAW AMM 33-53.
- [SDR DALA2017092307055](https://openairdocs.org/sdr/DALA2017092307055.md): Skin · damaged · Sep 22, 2017 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PER MAINTENANCE REQUEST FOUND SKIN DAMAGE AT LONGERON 30 AND STATION 465 IN FRONT OF THE VHF ANTENNA. SEVERAL RIVET HEADS ARE MISSING. AREA LOOKS LIKE LIGHTNING STRIKE. C/W PRI 561921-14 REV O MATCHES ERA 561921-14.
- [SDR DALA2018110106376](https://openairdocs.org/sdr/DALA2018110106376.md): Skin · not reported · Sep 20, 2017 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PER ERA 561921-14 DTE IS REQUIRED ON THE FUSELAGE SKIN AT FS 464 BETWEEN L-30 AND L29L DUE TO A SKIN REPAIR. REF LOG PAGE 0807279 FOR ERA561921-14 REV B TRACKING. LOGPAGE TERMINATED, PERMANENT REPAIR REQUIRED ON DIFFERENT LOGPAGE PER ER/A 561921-14 REV B. (LP0
- [SDR DALA2017021701325](https://openairdocs.org/sdr/DALA2017021701325.md): Coffeemaker · smoke · Feb 16, 2017 · N955DL · Doug MD88 · Buffet/Galleys
  > NR 2 COFFEEMAKER SMOKING WHEN ON, BUT NOT BREWING; TURNED OFF, SMOKE STOPPED. REPLACED THE COFFEEMAKER.
- [SDR DALA2017013100763](https://openairdocs.org/sdr/DALA2017013100763.md): Actuator · failed · Jan 30, 2017 · N955DL · Doug MD88 · Landing Gear Actuator
  > ON APPROACH INTO BHM WHEN GEAR SELECTED DOWN, THE NLG FAILED TO EXTEND. CREW ACCOMPLISHED QRH PROCEDURE AND PERFORMED AN ALTERNATE GEAR EXTENSION. NLG EXTENDED NORMALLY WITH GREEN DOWN/LOCKED INDICATION, CREW STOWED ALTERNATE EXTENSION LEVEL AND LANDED NORMALL
- [SDR DALA2016071805385](https://openairdocs.org/sdr/DALA2016071805385.md): Intercostal · cracked · Jul 17, 2016 · N955DL · Doug MD88 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FOUND CRACKED 2 OCLOCK POSITION. REMOVED INTERCOSTAL AND ATTATCHING PARTS. DRILLED UP NEW INTERCOSTAL IAW DWG 9911875. INSTALLED IAW DWG 9911875.
- [SDR DALA2015110306654](https://openairdocs.org/sdr/DALA2015110306654.md): Light · inoperative · Nov 3, 2015 · N955DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 19D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.
- [SDR DALA2015091605669](https://openairdocs.org/sdr/DALA2015091605669.md): Skin · cracked · Sep 15, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ACFT HAS SKIN PROTRUDING AND CRACKED AT BS 241, STRINGER 29L. REPAIRED IAW PRI 539193-14, REV 7.
- [SDR DALA2015091605668](https://openairdocs.org/sdr/DALA2015091605668.md): Structure · cracked · Sep 15, 2015 · N955DL · Doug MD88 · Empennage Structure
  > AFT LT EMPENNAGE, JUST ABOVE NR 1 PYLON. PACK EXIT FLANGE IS CRACKED. REPAIRED IAW ERA 539229-14, REV ORIGINAL.
- [SDR DALA2015091405613](https://openairdocs.org/sdr/DALA2015091405613.md): Skin · corroded · Sep 13, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN HAS AN AREA OF CORROSION, BS 578, STRINGER 29L. REPAIRED IAW SRM 53-04, FIG 12C, VIEW H.
- [SDR DALA2016091209445](https://openairdocs.org/sdr/DALA2016091209445.md): Skin · damaged · Sep 12, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > MTC REPORTED CORROSION, CRACKED SKIN, AND THREE PLUGS UNDER THE TCAS ANTENNA DOUBLER LOCATED BETWEEN FS 229-255 AND L-28L TO L-29R. ER/A 539193-14 WAS ISSUED TO REPAIR THE DAMAGE.
- [SDR DALA2015091405616](https://openairdocs.org/sdr/DALA2015091405616.md): Skin · corroded · Sep 12, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > BELLY SKIN BULGED, FASTENERS PULLED THROUGH BS 555 STRINGER 29R. REPAIRED IAW SRM 53-04, FIG 12C.
- [SDR DALA13055560955](https://openairdocs.org/sdr/DALA13055560955.md): Door Frame · corroded · Oct 27, 2013 · N955DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON FWD & AFT CARGO BAY DOOR FRAME BEAM. CORROSION REMOVED IAW SRM 51-10-3, PAR 26A. FOUND OUT OF LIMITS IAW SRM 53-05, FIG 123A. REPAIRED IAW ER/A 519124-14, REV ORIGINAL. REPAIR INSPECTED IAW ER/A 5109124-14 RE, ORIG AND SRM 53-05, FIG 123A.
- [SDR DALA13055540955](https://openairdocs.org/sdr/DALA13055540955.md): Tee Fitting · damaged · Oct 24, 2013 · N955DL · Doug MD88 · Fuselage Main, Bulkhead
  > SCRATCHES ON TEE ANGLE OF PRESSURE DOME LOWER AREA Y=1338 X=25 TO 23, X=6 TO 4, X=-35 TO 33. DAMAGED TEE SECTION AND STRUCTURE PARTS WERE REMOVED IAW SRM 53-03, FIG 37. NEW TEE SECTION FABRICATED AND INSTALLED IAW SRM 53-03, FIG 37, 51-30-2 AND 51-30-5.
- [SDR DALA13053890955](https://openairdocs.org/sdr/DALA13053890955.md): Finger Doubler · damaged · Oct 20, 2013 · N955DL · Doug MD88 · Wing, Plate/Skin
  > DAMAGE ON FINGER DOUBLER FASTENER PROTUDING LOWER AFT CORNER, BS 617, S20-21R. DOUBLER WAS REPLACED IAW ER/A 239715-14, REV D.
- [SDR DALA13053450955](https://openairdocs.org/sdr/DALA13053450955.md): Skin · damaged · Oct 18, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN BELOW FILLET PANEL RUBSTRIP AREA ON BS 807 BETWEEN LONGERONS 28-29R. SKIN REPAIRED IAW SRM 53-04, FIG 57, 51-30-5, 51-30-1.
- [SDR DALA13053310955](https://openairdocs.org/sdr/DALA13053310955.md): Tab · damaged · Oct 17, 2013 · N955DL · Doug MD88 · Elevator Structure
  > LIGHTING STRIKE ON T/E CONTROL TAB. REPAIRED IAW SRM 55-04 PH3.
- [SDR DALA13053330955](https://openairdocs.org/sdr/DALA13053330955.md): Skin · damaged · Oct 16, 2013 · N955DL · Doug MD88 · Rudder, Plate/Skin
  > DAMAGED METALLIZED SURFACE ON RUDDER. REPAIRED IAW SRM 51-70-IA.
- [SDR DALA13053320955](https://openairdocs.org/sdr/DALA13053320955.md): Longeron · corroded · Oct 16, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 26L BETWEEN, BS 1287 AND 1309, AFT CARGO BAY. CORROSION REMOVED, OUT OF LIMITS. LONGERON REMOVED AND NEW LONGERON SECTION INSTALLED IAW SRM 51-10-3 PAR. 26-21-14 53-02 FIG. 18.
- [SDR DALA13052650955](https://openairdocs.org/sdr/DALA13052650955.md): Structure · corroded · Oct 14, 2013 · N955DL · Doug MD88 · Fuselage Main, Structure
  > DURING SCHEDULED CHECK, CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLERS BETWEEN BS 731 & 750 IN THE CABIN FLOOR STRUCTURE. DOUBLERS WERE REMOVED AND NEW REPAIR DOUBLERS INSTALLED IAW SRM 53-05, FIGURE 131A.
- [SDR DALA13052660955](https://openairdocs.org/sdr/DALA13052660955.md): Doubler · corroded · Oct 13, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED HEAVY CHECK, CORROSION WAS NOTED AT ALL 4 RADIO ALTIMETER TO SKIN FAYING SURFACES. CORROSION WAS REMOVED AND NEW DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-3.
- [SDR DALA13052430955](https://openairdocs.org/sdr/DALA13052430955.md): Seat Track · corroded · Oct 11, 2013 · N955DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SEAT TRACK, X=-54, STA Y=480-482 AT CABIN FLOOR STRUCTURE. REPAIRED PLUG, INSTALLED PLUG IAW SRM 53-05, FIG 4A.
- [SDR DALA13052440955](https://openairdocs.org/sdr/DALA13052440955.md): Seat Track · corroded · Oct 10, 2013 · N955DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SEAT TRACK X=54 BETWEEN STA Y=423-425 AT CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED AND REPAIR PLUG WAS INSTALLED IAW SRM 53-05, FIG 4A.
- [SDR DALA13051820955](https://openairdocs.org/sdr/DALA13051820955.md): Frame · corroded · Oct 10, 2013 · N955DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME AT STA Y=127 AND BETWEEN LONGERONS 17 AND 18R COCKPIT STRUCTURE. FRAME WAS REPLACED IAW SRM 51-30-5, 51-30-2 AND DWG 9911511, REV "B".
- [SDR DALA13051800955](https://openairdocs.org/sdr/DALA13051800955.md): Access Panel · corroded · Oct 10, 2013 · N955DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON ACCESS PLATE NR 1464C AND SCREW HOLES OF RT MAIN FUEL TANK. REPLACED PLATE 1464C IAW SRM 51-22-2A.
- [SDR DALA13051790955](https://openairdocs.org/sdr/DALA13051790955.md): Access Panel · corroded · Oct 10, 2013 · N955DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON ACCESS PLATE NR 1462C AND SCREW HOLES OF RT MAIN FUEL TANK. ACCESS PLATE NR 1462C. REPLACED IAW SRM 51-22-2A.
- [SDR DALA13051740955](https://openairdocs.org/sdr/DALA13051740955.md): Longeron · cracked · Oct 10, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 12L AT BS 1437. REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA13053920955](https://openairdocs.org/sdr/DALA13053920955.md): Skin · corroded · Oct 9, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN BENEATH RUBSTRIP FROM BS 769 TO 771 AND BETWEEN LONGERONS 27-28R. REPAIR DOUBLER WAS FABRICATED AND REPAIR WASHERS, AND REPAIR DOUBLER WERE INSTALLED IAW SRM 53-0 4 FIG. 57.
- [SDR DALA13051430955](https://openairdocs.org/sdr/DALA13051430955.md): Door Frame · cracked · Oct 9, 2013 · N955DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON INTERNAL DOUBLER AT THE LOWER AFT DOOR FRAME CORNER, BS 423.5 BETWEEN LONGERONS 27-28R AT THE FWD CARGO BAY. FASTENERS WERE REMOVED AND DAMAGE REMOVED IAW SRM 51-30-2 AND 51-30-5 AND 53-05, FIG 105. DOUBLERS AND FILLERS WERE FABRICATED IAW SRM 53-05
- [SDR DALA13051410955](https://openairdocs.org/sdr/DALA13051410955.md): Bushing · damaged · Oct 8, 2013 · N955DL · Doug MD88 · Wing Miscellaneous Structure
  > ELONGATED BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING. BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING WERE R & R IAW EA 09-070683-03, AD REV L AND SRM 51-30-10; RII COMPLETED.
- [SDR DALA13050170955](https://openairdocs.org/sdr/DALA13050170955.md): Frame · corroded · Oct 6, 2013 · N955DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1380 FROM X=-25 TO X=25. FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5, DWG 9912246, REV CE.
- [SDR DALA13050140955](https://openairdocs.org/sdr/DALA13050140955.md): Longeron · cracked · Oct 6, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK LONGERON 10R, BS 1431, SECTION OF LONGERON DAMAGE WAS REMOVED. NEW SECTION AND SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-20-0.
- [SDR DALA13049500955](https://openairdocs.org/sdr/DALA13049500955.md): Skin · worn · Oct 3, 2013 · N955DL · Doug MD88 · Wing, Plate/Skin
  > WORN PREVIOUS REPAIR DOUBLER ON L/E STA XFS=110 RT WING. PREVIOUS REPAIR REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, INSTALLED AND IDENTIFIED IAW ER/A N 378819-14, REV A.
- [SDR DALA13049080955](https://openairdocs.org/sdr/DALA13049080955.md): Cusp Web · corroded · Oct 2, 2013 · N955DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1003 TO Y=1022 AND BETWEEN X=54 TO X=60 AT PAX CABIN. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, INSTALLED, IDENTIFIED, AND CIC WAS APLICATED IAW SRM 53-05 FIG 131A, 51-10
- [SDR DALA13049070955](https://openairdocs.org/sdr/DALA13049070955.md): Cusp Web · corroded · Oct 2, 2013 · N955DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1022 TO 1041 AND BETWEEN X=54 TO X=60 AT PAX CABIN REF NRC (T0 294284) OR NC 193 ZONE 58, REF (T0 295304). DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG
- [SDR DALA13048820955](https://openairdocs.org/sdr/DALA13048820955.md): Longeron · cracked · Oct 1, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 2LT AT BS 160. SECTION OF LONGERON WAS REMOVED AND NEW SECTION LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18.
- [SDR DALA13055550955](https://openairdocs.org/sdr/DALA13055550955.md): Longeron · corroded · Sep 26, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 23LT FROM BS 1271 - 1322 IN AFT CARGO BAY LT TUNNEL. CORROSION REMOVED. REWORKED AREA FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1., DAMAGE LONGERON SECTION REMOVED, AND A NEW SECTION LONGERON INSTALLED.
- [SDR DALA13053860955](https://openairdocs.org/sdr/DALA13053860955.md): Longeron · worn · Sep 24, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > WORN LONGERON 19 LEFT BS 1375. DAMAGE BLENDED AND LONGERON SECTION REMOVED. NEW SECTION INSTALLED IAW SRM 53-01, FIG 1, 51-30-2, 51-30-5,53-02, FIG 18, 51-10-3 PAR 21 AND 14, AND PS 900-5-1.
- [SDR DALA13057730955](https://openairdocs.org/sdr/DALA13057730955.md): Skin · cracked · Sep 17, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKS FOUND ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 519129-14AD REV. ORIG.

Next page: https://openairdocs.org/deregistered/N955DL-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 = 'N955DL' AND deregistration_id = 'N955DL-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N955DL-2022-04-25/reports

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