# Service difficulty reports: N913DL, cancelled Dec 3, 2022

A list on [N913DL, cancelled Dec 3, 2022](https://openairdocs.org/deregistered/N913DL-2022-12-03.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 4 · 155 reports

- [SDR DALA2020032602044](https://openairdocs.org/sdr/DALA2020032602044.md): Structure · damaged · Mar 17, 2020 · N913DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO BIN, AT APPROXIMATELY 4FT AFT OF THE DOOR, THERE IS A HOLE IN THE CENTER OF THE FLOOR (ABOUT 2X2 INCHES). REMOVED DAMAGED AREA. CLEANED UP AREA AND INSTALLED A DOUBLER OVER AREA PER MD-88 SRM 53-05 FIG 7A. (LP #1533051)
- [SDR DALA2020030201504](https://openairdocs.org/sdr/DALA2020030201504.md): Hose · leaking · Feb 29, 2020 · N913DL · Doug MD88 · Crew Oxygen System
  > CAPTAIN'S OXYGEN PANEL HOSE DEVELOPED A LEAK IN FLIGH, TURNED OFF OXYGEN BOTTLE TO STOP LEAKAGE. REPL OBSERVERS O2 BOX AND MASK PER MD88 AMM 35-10 AND RI 585835- 14 REV ORIG SECTION II TIME LIMITED REPAIR II. LEAK CHECK AND OPS CHECK OK. MASK, OX, CREW; OFF 55
- [SDR DALA2020012700598](https://openairdocs.org/sdr/DALA2020012700598.md): Battery Pack · inoperative · Jan 26, 2020 · N913DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT ROWS 16-20 INOP. REPLACED BATTERIES IN BATTERY PACK - TESTS AND OPS CHECKS GOOD. (LP6484606)
- [SDR DALA2019120437037](https://openairdocs.org/sdr/DALA2019120437037.md): Terminal · burned · Dec 2, 2019 · N913DL · Doug MD88 · Electrical Power System Wiring
  > SDR REPORTED DUE TO EMERGENCY DECLARED PER MCC NOTIFICATION - ON DESCENT / APPROACH A/P AND A/T DISCONNECTED WITH MULTIPLE OAP LIGHTS AND LOTS OF CA / FO FLT / NAV INSTRUMENTATION - LT GEN OFF AND LT AC BUS MULTIPLE ASSOCIATED LIGHTS - RAN QRH GEN OFF PROCEDUR
- [SDR DALA2019120307007](https://openairdocs.org/sdr/DALA2019120307007.md): Gcu · failed · Dec 1, 2019 · N913DL · Doug MD88 · AC Generator-Alternator
  > DURING DESCENT PASSING 9000 FT, LOST THE LEFT GENERATOR, NO FURTHER ACTION TAKEN. REMOVED AND REPLACED THE LT GEN CONTROL IAW AMM 24-20. OPS CHECKS GOOD.
- [SDR DALA2019091305296](https://openairdocs.org/sdr/DALA2019091305296.md): Battery Pack · discharged · Sep 12, 2019 · N913DL · Doug MD88 · Emergency Lighting
  > ROW 25 OVERWING EMERGENCY EXIT SIGNS INOP. REPL BATTERY PACK PER AMM 33-53. OPS CHECK GOOD. (LP5597571)
- [SDR DALA2019081904845](https://openairdocs.org/sdr/DALA2019081904845.md): Gauge · failed · Aug 19, 2019 · N913DL · Doug MD88 · AC Generator-Alternator
  > CREW LOST THE LT GENERATOR WHILE THE RT GENERATOR WAS ALREADY ON MEL. REPLACED LT ENG. GENERATOR, CSD, AND OIL COOLER. FLUSHED OIL LINES AND SERVICED CSD. FOUND # 1 PMG C/B POPPED ON # 1 GCU. REPLACED GCU. OPN CKS AND LEAK CKS OK. (LP5595378)
- [SDR DALA2019032101834](https://openairdocs.org/sdr/DALA2019032101834.md): Terminal Block · burned · Mar 21, 2019 · N913DL · Doug MD88 · AC Power Distribution System
  > BEFORE PUSHBACK EXT. PWR WAS PULLED. ALL ELECT POWER REMOVED FROM JET. RESTORED EXT PER. AFTER PUSH, BEGINNING TAXI, GALLEY PER SHREDDED. STRONG ELECTRICAL SMELL OBSERVED FROM CB PANEL BEHIND CAPTAINS SEAT. NO SMOKE OBSERVED. FOUND TERMINAL BLOCK S3-263 BURNED
- [SDR DALA2019120907158](https://openairdocs.org/sdr/DALA2019120907158.md): Skin · torn · Mar 14, 2019 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE/ SKIN/ C-3 DOOR CUTOUT/ AFT EDGE: REPAIR OF EDGE TEAR - PERMANENT REPAIR ACCOMPLISHMENT. ACCOMPLISHED SECTION III OF ERA 271005-14 REV E NO FURTHER DAMAGE NOTED. REF LOG PG 1386582 AS TRACKING SECTION IV PERMANENT REPAIR REQ PER ERA 2710050-14 REV E.
- [SDR DALA2019030801551](https://openairdocs.org/sdr/DALA2019030801551.md): Wire · shorted · Mar 8, 2019 · N913DL · Doug MD88 · Light System Wiring
  > SUSPECTED SHORT IN CAPT'S OVERHEAD MAP LT. POPPED CB AFTER RESETTING. ELECTRICAL SMELL. TURNED OFF, SMELL GONE. INSP. OVHD MAP LIGHT ASSY. FOUND EVIDENCE OF SHORTED WIRE AT POS TERM. R/R LIGHT ASSY PER AMM CH 33-10. OPS CK GOOD. OK FOR SVC. (LP5759160)
- [SDR DALA2019030101329](https://openairdocs.org/sdr/DALA2019030101329.md): Doubler · cracked · Feb 28, 2019 · N913DL · Doug MD88 · Fuselage Miscellaneous Structure
  > TWO CRACKS WERE FOUND ON INTERNAL DOUBLER AT LOWER AFT CORNER OF FORWARD CARGO DOOR JAMB. PERMANENT REPAIR SECTION I WAS PERFORMED AT LOWER AFT CORNER OF FORWARD CARGO DOOR JAMB PER ER/A 575828-14AD REV. ORIGINAL AND ETI-88-19-016 REV.4. REPAIR APPROVAL IS LIM
- [SDR DALA2019030101331](https://openairdocs.org/sdr/DALA2019030101331.md): Skin · dented · Feb 27, 2019 · N913DL · Doug MD88 · Trailing Edge Flaps
  > DENTS ON LOWER SKIN ON MID AND INBD FLAPS VANES OF OUTBD FLAP AT RT WING (AD). DUE TO DELAMINATION ON DENT AT MID VANE PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-03D-PAR. 11B. PERFORM A DETAIL VISUAL INSPECTION EVERY C CHECK ON DENTED AREA, LOWER SKIN OF INB
- [SDR DALA2019022801283](https://openairdocs.org/sdr/DALA2019022801283.md): Skin · delaminated · Feb 27, 2019 · N913DL · Doug MD88 · Trailing Edge Flaps
  > DENTS ON LOWER SKIN ON MID AND INBD FLAPS VANES OF OUTBD FLAP AT RT WING (AD). DUE TO DELAMINATION ON DENT AT MID VANE PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-03D-PAR. 11B PERFORM A TAP TEST INSPECTION FOR POSSIBLE DISBOND EVERY C CHECK ON DENTED AREA, LO
- [SDR DALA2019022801282](https://openairdocs.org/sdr/DALA2019022801282.md): Frame · cracked · Feb 27, 2019 · N913DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON AFT. ACC. COMP. WEB FRAME FWD FACE STA Y=1463 CANT PROYECTION LONG 9R. WEB FRAME FWD FACE STA Y=1463 CANT PROYECTION LONG 9R.ON AFT. ACC. COMP. WAS REPLACED PER DWG 9953015 REV AH AND SRM 51-30-2 AND SRM 51-30-5. (LP0962285)
- [SDR DALA2019022601210](https://openairdocs.org/sdr/DALA2019022601210.md): Release Mech · sheared · Feb 25, 2019 · N913DL · Doug MD88 · Aerodynamic Fairings
  > AWR. MTC REQUEST. DURING TORQUE TEST VERIFICATION IN REF AMDS 5350-4287 STEP 1, SHAFT OF TAILCONE RELEASE MECHANISM CAM WAS SHEARED. CAM ASSY P/N: 5961568-501 WAS REMOVED PER MD-88 AMM 53-53-02-201 1 STEP 3(A) AND SERVICIABLE CAM ASSY P/N: 5961568-501 WAS INST
- [SDR DALA2019022501155](https://openairdocs.org/sdr/DALA2019022501155.md): Access Panel · worn · Feb 24, 2019 · N913DL · Doug MD88 · Wing, Plate/Skin
  > AFTER REMOTION OF FUEL ACCES PANEL NBR: 1361C WAS FOUND WEAR ON CONTERSINK IN REF NRC 006. FUEL ACCESS PANEL NBR: 1361C WAS REPLACED FOR A SERVICEABLE ACCESS PANEL P/N: NARB0975-519 PER MD-88 AMM 28-00-00-201. (LP0958359)
- [SDR DALA2019021100878](https://openairdocs.org/sdr/DALA2019021100878.md): Battery Pack · inoperative · Feb 9, 2019 · N913DL · Doug MD88 · Emergency Lighting
  > 2ND ROW OVERWING EXIT EMERGENCY LIGHTS INOP. R/R BATTERY PACK FOR 2ND ROW OVERWING EXIT SIGNS. PER MD88 AMM 33-53. OK FOR SVC. (LP3759170)
- [SDR DALA2019020400699](https://openairdocs.org/sdr/DALA2019020400699.md): Skin · delaminated · Jan 30, 2019 · N913DL · Doug MD88 · Rudder, Plate/Skin
  > DURING PAINT VISIT FOUND RUDDER DELAMINATED. REPLACED RUDDER WITH SERVICEABLE RUDDER PER WORKCARD 2720-4421 RUDDER, MAIN TA OFF 00000 ON 88-5554-9-0001 00550. (LP3759132)
- [SDR DALA2019020400700](https://openairdocs.org/sdr/DALA2019020400700.md): Tab · damaged · Jan 28, 2019 · N913DL · Doug MD88 · Rudder, Tab Structure
  > REMOVE RUDDER TAB DUE TO MISSING AND DAMAGED FLAME SPRAY. REMOVE ON NRC 20 IAC/AMA PER AMM 27-20-02. REPLACED RUDDER TAB WITH SERVICEABLE RUDDER TAB PER WORKCARD 2720-4921 TAB, RUDDER W/C OFF 00000 ON 88-5554-9-0003 00350. (LP3759131)
- [SDR DALA2019012100378](https://openairdocs.org/sdr/DALA2019012100378.md): Relay · stuck · Jan 21, 2019 · N913DL · Doug MD88 · AC Power Distribution System
  > AFTER LNDG WITH APU GEN ON - WITH RIGHT ENGINE SHUTDOWN, R BUS FAILED. ELEC SMELL STARTED. C/W NO GO ODI 21-72 AND W/C 2120-2367. FOUND RT AUX POWER RELAY STUCK. R/R RT AUX POWER RELAY PER WDM 24-21-03. OPS CK GOOD. A/C OK FOR SVC. (LP3759108)
- [SDR DALA2018100505897](https://openairdocs.org/sdr/DALA2018100505897.md): Wire Harness · inoperative · Oct 5, 2018 · N913DL · Doug MD88 · Light System Wiring
  > EMRG EXIT ROW LIGHTS INOP AT 19/20. REPLACED EMRG LIGHT WIRE HARNESS PER MD88 AMM 32-51 OK FOR SVC. (LP4359437)
- [SDR DALA2018092655761](https://openairdocs.org/sdr/DALA2018092655761.md): Frame · cracked · Sep 24, 2018 · N913DL · Doug MD88 · Fuselage Main, Frame
  > THE LEFT WHEEL WELL FORWARD FRAME HAS A CRACK. REPLACED LEFT FORWARD WHEEL WELL FRAME PER BAC DWG #5930584. (LP #4765882)
- [SDR DALA2018080304840](https://openairdocs.org/sdr/DALA2018080304840.md): Door · corroded · Jul 22, 2018 · N913DL · Doug MD88 · Service Doors
  > WASTE WATER SERVICE DOOR AFT. AFT LAV SVC DOOR CORRODED. RMVD DOOR AND PLACED IN FWD CARGO MCO POUCH. INSTALLED NEW AFT LAV SERVICE DOOR OPS CHECK GOOD REF AMM 52-40 P/N ON 5914792-61.
- [SDR DALA2018053103718](https://openairdocs.org/sdr/DALA2018053103718.md): Cable · deteriorated · May 30, 2018 · N913DL · Doug MD88 · Standard Practices/Structures
  > KEVLAR CABLE FOUND DETERIORATED BE LT GROMMET. R/I KEVLAR CABLE PER MD88 AMM 53-53 & WORKCARD 5350-01077-0101 STEP 14. (LP4247373)
- [SDR DALA2018052703604](https://openairdocs.org/sdr/DALA2018052703604.md): Fuse · blown · May 26, 2018 · N913DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS FROM SEAT 31 AFT INOPERATIVE. REPLACED FUSES IN CHARGER PER CMM 25-60-03. OPS CHECK GOOD PER MD88 AMM 33-53.
- [SDR DALA2018061504018](https://openairdocs.org/sdr/DALA2018061504018.md): Apu · shutdown · May 18, 2018 · N913DL · Doug MD88 · APU Core Engine
  > ON APU START, APU STARTED AND THEN SHUT DOWN. NO FAULT LIGHT RPM DROPPED IMMEDIATELY TO ZERO. GRN CREW REPORTED FLAME OUT THE EXHAUST. COMPARTMENT NO EXTERNAL DAMAGE FOUND. FWD APU TO MCO AND PLACARD PER MEL 49-00-01A M PROC C/W. R&R APU ASSY OPS + LK CK GOOD
- [SDR DALA2017121808663](https://openairdocs.org/sdr/DALA2017121808663.md): Longeron · cracked · Dec 17, 2017 · N913DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > FUSELAGE CRACK AT FASTEN HOLE STA 294 L24L. REMOVED DAMAGE SECTION 54 3/4 OF LONGERON 24 LEFT @ STA 294 AND REPAIRED LONGERON IAW MD88 SRM 53-02 FIG 18. (LP0342699)
- [SDR DALA2017121408598](https://openairdocs.org/sdr/DALA2017121408598.md): Skin · dented · Dec 13, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS STA 291 - 307 / LONG. 23L - 25L / DENT REPAIR - DTA-INFORM ENGINEERING. ERA273604-14 REV B FS STA 291-307/LONG, 23L-25L/DENT REPAIR TIME LIMITED. THIS LP IS TO BE TERMINATED. THE DTA HAS BEEN ACCOMPLISHED AND REQUIRES REPAIR REPLACEMENT PR
- [SDR DALA2017111308061](https://openairdocs.org/sdr/DALA2017111308061.md): Fire Loop · false indication · Nov 11, 2017 · N913DL · Doug MD88 · Fire Detection
  > FIRE LOOP A, ON THE RIGHT ENGINE ILLUMINATED WITH NO FIRE WARNING. LOOP B OPS CHECKED GOOD. INSPECTED THE FIRE LOOP ELEMENTS AND CONNECTIONS. NO PROBLEMS NOTED. OPS CHECKED THE RT ENGINE FIRE LOOP A, CHECKED NORMAL IAW AMM 26-10-00. NO 30 DAY HISTORY. O
- [SDR DALA2017102607791](https://openairdocs.org/sdr/DALA2017102607791.md): Smoke Detector · false activation · Oct 26, 2017 · N913DL · Doug MD88 · Smoke Detection
  > LEFT AFT LAVATORY SMOKE DETECTOR SOUNDED IN FLIGHT. NO SMOKE OR FIRE PRESENT. NO TROUBLE FOUND. SMOKE DETECTOR TESTS OK.
- [SDR DALA2017062604967](https://openairdocs.org/sdr/DALA2017062604967.md): Wire · disconnected · Jun 25, 2017 · N913DL · Doug MD88 · Light System Wiring
  > DUAL RED EMERGENCY LIGHTS AT ROW 24 INOPERATIVE. CONNECTED WIRES TO CONNECTOR. LIGHTS OPERATED NORMALLY IAW AMM 33-53.
- [SDR DALA2017062604966](https://openairdocs.org/sdr/DALA2017062604966.md): Wire · disconnected · Jun 25, 2017 · N913DL · Doug MD88 · Light System Wiring
  > AISLE EMERGENCY LIGHT AT ROW 26 INOPERATIVE. RECONNECTED WIRES TO CONNECTOR. LIGHT OPERATES NORMALLY IAW AMM 33-53.
- [SDR DALA2017040402721](https://openairdocs.org/sdr/DALA2017040402721.md): Feeder Cable · burned · Mar 31, 2017 · N913DL · Doug MD88 · Electrical Power System Wiring
  > WHILE PERFORMING DUAL PACK CONFIDENCE CHECK FOUND APU GENERATOR FEEDER CABLES SCOTCHED AND BLACKENED. PULLED AND COLLARD APU CNTR/APU DOOR CNTL/AND APU GEN CNTL C/BS. RMVD L/H AFT STAIR SIDEWALL FOR ACCESS. RMVD APU INLET SCREEN FOR ACCESS. RMVD JUMPER BETWEE
- [SDR DALA2017031702180](https://openairdocs.org/sdr/DALA2017031702180.md): Indicator · missing · Mar 16, 2017 · N913DL · Doug MD88 · Hydraulic Filter, Main
  > RIGHT HYDRAULIC SYSTEM PRESSURE/QUANTITY LOSS REQUIRED USE OF ALTERNATE GEAR EXTEND PER QRH. MAINTENANCE FOUND THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SIDE FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR (DPI) MISSING. RETAINING SCREWS SHEARED FROM MODUL
- [SDR DALA2017021501236](https://openairdocs.org/sdr/DALA2017021501236.md): Skin · cracked · Feb 14, 2017 · N913DL · Doug MD88 · Elevator, Plate/Skin
  > CRACKED INNER SKIN ON RT ELEVATOR. REPAIRED IAW ET/I-88-17-044 REV 4 AND ER/A 554132-14 SECCION 1 REV ORIGINAL.
- [SDR DALA2017021501235](https://openairdocs.org/sdr/DALA2017021501235.md): Vane · delaminated · Feb 14, 2017 · N913DL · Doug MD88 · Trailing Edge Flaps
  > DELAMINATION ON LOWER SURFACE OF CENTER GUIDE VANE, LT OTBD FLAP. THE GUIDE VANE WAS REMOVED AND REPLACED IAW AMM 27-51-03.
- [SDR DALA2017021401194](https://openairdocs.org/sdr/DALA2017021401194.md): Doubler · dented · Feb 13, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT FOUND ON FUSELAGE SKIN REPAIR DOUBLER BS 227, LONGERON 16 - 18L. REPAIRED IAW ETI-88-17-042 REVISION 4, AND ER/A 554130-14 REVISION ORIGINAL.
- [SDR DALA2017020801045](https://openairdocs.org/sdr/DALA2017020801045.md): Skin · cracked · Feb 7, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN AT BS 1406 NEAR LONGERON 2R BESIDE DORSAL FIN ATTACH ANGLE. REPAIRED IAW ETI-88-17-016 REVISION 3 AND ER/A 541702-14AD SECTION II.
- [SDR DALA2017020600998](https://openairdocs.org/sdr/DALA2017020600998.md): Skin · corroded · Feb 5, 2017 · N913DL · Doug MD88 · Ailerons
  > CORROSION ON UPPER SKIN BELOW STATIC DISCHARGE BASE AT LT AILERON. THE SKIN WAS REPAIRED IAW SRM 51-70-1A, PAR. 12.
- [SDR DALA2017020300899](https://openairdocs.org/sdr/DALA2017020300899.md): Skin · nicked · Feb 2, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > NICK ON FWD LWR EDGE LT WINDOW BELT. THE NICKS BS 658 - 714 WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21 AND ERA 554135-14 REV. ORIGINAL.
- [SDR DALA2017020300898](https://openairdocs.org/sdr/DALA2017020300898.md): Skin · nicked · Feb 2, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > NICK ON FWD LOWER EDGE LT WINDOW BELT IAW ER/A 554127-14 REV,ORIG. THE NICKS WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21, AND ER/A. 554136-14 REV. ORIGINAL,
- [SDR DALA2017020200877](https://openairdocs.org/sdr/DALA2017020200877.md): Cargo Track · corroded · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, CORROSION ON RT TIE TRACK FROM Y=1003 TO Y=1155, Y=1212 TO Y=1322. DUE TO EXCESIVE CORROSION WERE REPLACE TIE TRACKS. NEWS TIE TRACKS WERE DRILLED PER SRM. 51-10-4. NEWS TIE TRACK RT Y=1212 TO Y=1322 AND TIE TRACK RT Y=1103 TO Y=1155 WER
- [SDR DALA2017020200875](https://openairdocs.org/sdr/DALA2017020200875.md): Floor Support · damaged · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, ELONGATED HOLE ON FLOOR SUPPORT ABOVE LONG 28R BTW STA Y = 1117 TO 1155. SUPPORT "Z" WAS REMOVED AND INSTALLED PER SRM 51-30-1 AND 51-30-2 NEW SUPPORT "Z" WAS DRILLED PER SRM 51-10-4. NEW SUPPORT "Z" WAS TREATED AND PAINTED PER SRM 51-1
- [SDR DALA2017020200870](https://openairdocs.org/sdr/DALA2017020200870.md): Skin · nicked · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE, NICKS ON AFT LWR EDGE LT WINDOW BELT STA Y=748. REF ERA 554116-14 REV ORIG SEC II.
- [SDR DALA2017020200869](https://openairdocs.org/sdr/DALA2017020200869.md): Intercostal · cracked · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED 2 INTERCOSTALS AND PLATE AT KEEL BEAM STA 937 BETWEEN X=7 AND X=-7. INTERCOSTALS (2 E/A) AND PLATE WAS REMOVED, FABRICATED AND INSTALLED PER DWG 9936368 REV AW SRM 51-30-5 AND 53-14-3.
- [SDR DALA2017020200868](https://openairdocs.org/sdr/DALA2017020200868.md): Insert · missing · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage Floor Panel
  > MISSING INSERTS AND CRACK ON AFT CARGO COMPARTMENT CENTER FLOOR PANEL 181DF. FLOOR PANEL WAS REPLACED PER AMM 25-52-01-801.
- [SDR DALA2017020200867](https://openairdocs.org/sdr/DALA2017020200867.md): Cargo Track · corroded · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, CORROSION ON LT TIE TRACK FROM Y=1003 TO Y=1322. NEWS TIE TRACK LT Y=1003 TO Y=1220 AND TIE TRACK LT Y=1220 TO Y=1322 WERE INSTALLED PER SRM 51-30-1 AND 51-30-2 HOLES WERE TREATED AND PAINTED PER SRM 51-10-3 PAR 14 AND 21.
- [SDR DALA2017020200863](https://openairdocs.org/sdr/DALA2017020200863.md): Intercostal · cracked · Feb 1, 2017 · N913DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE ON FLOOR SUPPORT AT STA Y=1361 X=-22 Z=0. INTERCOSTAL WAS REPAIRED PER SRM, 53-01 FIG 1 51-10-2, 51-30-5.
- [SDR DALA2017021001124](https://openairdocs.org/sdr/DALA2017021001124.md): Relief Valve · corroded · Jan 31, 2017 · N913DL · Doug MD88 · Pressure Regulator/Outflow Valve
  > FWD CARGO BAY CORRODED ON AFT POSITIVE PRESSURE RELIEF VALVE AT FWD CARGO BAY. REPLACED FOR A NEW VALVE IAW AMM 21-32-07-201.
- [SDR DALA2017020100828](https://openairdocs.org/sdr/DALA2017020100828.md): Structure · corroded · Jan 31, 2017 · N913DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION ON BUSHING BORE OF LT MLG. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW DWG SR 09570087 REV. BB.

Next page: https://openairdocs.org/deregistered/N913DL-2022-12-03/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 = 'N913DL' AND deregistration_id = 'N913DL-2022-12-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N913DL-2022-12-03/reports

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