# Service difficulty reports: N934DL, cancelled Aug 22, 2019

A list on [N934DL, cancelled Aug 22, 2019](https://openairdocs.org/deregistered/N934DL-2019-08-22.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 2 · 91 reports

- [SDR DALA2018032801979](https://openairdocs.org/sdr/DALA2018032801979.md): Skin · corroded · Mar 27, 2018 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION AT THE AFT LAVATORY SERVICE PANEL CUTOUT. REPAIRED IAW ERA 567095-14, REV O.
- [SDR DALA2018032801980](https://openairdocs.org/sdr/DALA2018032801980.md): Skin · damaged · Mar 22, 2018 · N934DL · Doug MD88 · Rudder, Plate/Skin
  > PAINT ON LEFT AND RIGHT SIDE OF RUDDER MISSING DOWN TO COMPOSITE LEVEL. RUDDER WAS REPLACED.
- [SDR DALA2017073005784](https://openairdocs.org/sdr/DALA2017073005784.md): Transformer · damaged · Jul 29, 2017 · N934DL · Doug MD88 · Passenger Compartment Lighting
  > FUME EVENT AT CRUISE. SMELLED ELECTRICAL BUT COULD NOT ISOLATE. WENT AWAY AFTER 5 MIN APPROX. MAYBE ASSOCIATED WITH ENG ANTI ICE. ON DESCENT RETURNED COMPLIED WITH QRH. SEEMED TO DISSIPATE AFTER RIGHT PACK/ AND RECIRC FAN/ GND SVC BUS C/B'S PULLED. ON GND FUME
- [SDR DALA2017071905536](https://openairdocs.org/sdr/DALA2017071905536.md): Sensor · failed · Jul 18, 2017 · N934DL · Doug MD88 · Leading Edge Slat Position Indicating System
  > SLAT DISAGREE WARNING LIGHT ILLUMINATED. COMPLIED WITH TAKEOFF WARNING TEST, NO FAULTS, CHECKED PSEU AND SIF COMPUTERS, ALL CHECK GOOD. DFDR REMOVED. LT WING SLAT C SENSOR FOUND FAILED. REPLACED SENSOR AND ADJUSTED OTHER SENSORS. REPLACED NR 2 STALL WARNING
- [SDR DALA2016033102472](https://openairdocs.org/sdr/DALA2016033102472.md): Battery Pack · inoperative · Mar 30, 2016 · N934DL · Doug MD88 · Emergency Lighting
  > THE FLIGHT CREW FOUND THAT THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED EMERGENCY LIGHT BATTEY PACKS AND THE LIGHTS CHECKED OK.
- [SDR DALA2016032702358](https://openairdocs.org/sdr/DALA2016032702358.md): Skin · damaged · Mar 26, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON WINDOW FRAME BETWEEN BS 750 TO 769 AND LONGERONS 12RT TO 13RT. REWORKED AREAS WERE MEASURED, UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUTS ON ZONE CRITICAL, THE ORIGINAL THICKNESS ON BLEND OUT 1 IS.086"
- [SDR DALA2016032702357](https://openairdocs.org/sdr/DALA2016032702357.md): Skin · damaged · Mar 25, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTING STRINKE ON LOWER WINDOW FRAME, BS 1100 RT SIDE. REWORKED AREAS WERE MEASURED, UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL, 1 THE ORIGINAL THICKNESS IS.084" AND REMAINING THICKNESS.080", THE ORI
- [SDR DALA2016032702353](https://openairdocs.org/sdr/DALA2016032702353.md): Skin · damaged · Mar 25, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON WINDOW FRAME BETWEEN BS 731 TO BS 750 AND LONGERONS 12 RT TO 13 RT. REWORKED AREAS WERE MEASURED (UT) WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PARAGRAPH 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL, 1 IS.090" AND REMAINING THICKNES
- [SDR DALA2016032702352](https://openairdocs.org/sdr/DALA2016032702352.md): Skin · damaged · Mar 25, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES, FOUR ON WINDOW FRAME BETWEEN BS 674 TO 693 AND LONGERONS 14TO 15R. MEASURE REWORKED AREAS, UT) WAS ACCOMPLISHED IAW DC/MD NDT SPM 04-00-07 PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL BLEND OUT, 2 THE ORIGINAL THICKNESS ES.120
- [SDR DALA2016032602309](https://openairdocs.org/sdr/DALA2016032602309.md): Skin · dented · Mar 25, 2016 · N934DL · Doug MD88 · Trailing Edge Flaps
  > SEVERAL DENTS ON LOWER SKIN, BELOW OF REPAIR DOUBLER OF LT WING OTBD FLAP INBD GUIDE VANE. LOWER SKIN OF LT WING OTBD FLAP INBD GUIDE VANE WAS REPAITED IAW SRM 57-03D, PAR II.
- [SDR DALA2016111608866](https://openairdocs.org/sdr/DALA2016111608866.md): Skin · corroded · Mar 24, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION BTW FUSELAGE SKIN AND DOUBLER ON LOWER CORNER AT AFT LAVATORIES SERVICE PANEL CUT OUT. REMOVED CORROSION AREAS, MEASURE: ORIG, MATERIAL THICKNESS IS 0.063" REMAINING THICKNESS IS 0.055". REPAIRED PER ER/A.
- [SDR DALA2016032502294](https://openairdocs.org/sdr/DALA2016032502294.md): Door · cracked · Mar 24, 2016 · N934DL · Doug MD88 · Engine Thrust Reverser
  > SEVERAL CRACK ON HOLES OF OUTER SKIN AT LT ENGINE THRUST REVERSE UPPER DOOR. SKIN AT LT ENGINE TRUST REVERSE UPPER DOOR WERE REPAIRED IAW AMM 78-30-07-801.
- [SDR DALA2016032502293](https://openairdocs.org/sdr/DALA2016032502293.md): Strap · corroded · Mar 24, 2016 · N934DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON REPAIR STRAP ON LOWER AT AFT CARGO COMPARTMENT DOOR JAMB BETWEEN BS 1155 TO BS 1212. STRAP WAS REPLACED IAW ER/A 457309-14, REV A AND SRM 53-05, FIG 123A.
- [SDR DALA2016032402283](https://openairdocs.org/sdr/DALA2016032402283.md): Skin · deformed · Mar 23, 2016 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DEFORMED FUSELAGE SKIN AND DOUBLERS ON LOWER AND FWD, AFT CORNERS AT AFT LAVATORY SERVICE PANEL CUTOUT. REPAIRED LOWER FWD CORNER IAW ERA 397822-14 MA, REV B.
- [SDR DALA2016032302240](https://openairdocs.org/sdr/DALA2016032302240.md): Cargo Track · corroded · Mar 22, 2016 · N934DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT CARGO TRACK BETWEEN BS 1220 - 1320. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4 AND 51-30-01 AND 51-30-5.
- [SDR DALA2016032302235](https://openairdocs.org/sdr/DALA2016032302235.md): Access Panel · corroded · Mar 22, 2016 · N934DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON SEATING AREA AND COUNTERSINK ON FUEL ACCESS PLATE 1409C AT RT WING. ACCESS PLATE REPLACED.
- [SDR DALA2016032302236](https://openairdocs.org/sdr/DALA2016032302236.md): Floor Panel · cracked · Mar 20, 2016 · N934DL · Doug MD88 · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL BETWEEN CAPTAIN SEAT AND COLUMN AT LT COCKPIT. FLOOR PANEL WAS REPLACED IAW SRM 51-10-03, 51-10-04 ON 51-30-01.
- [SDR DALA2016032102137](https://openairdocs.org/sdr/DALA2016032102137.md): Door Frame · corroded · Mar 20, 2016 · N934DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB BEAM AT MID CARGO COMPARTMENT. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A AND ERA 504344-14, REV ORIGINAL.
- [SDR DALA2016032102125](https://openairdocs.org/sdr/DALA2016032102125.md): Door Frame · cracked · Mar 20, 2016 · N934DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON UPPER CENTER DOOR JAMB AT LT FWD EMERGENCY EXIT. CRACK ON UPPER DOOR JAMB LT WAS REPAIRED IAW SRM 53-05, FIG 32.
- [SDR DALA2016031802075](https://openairdocs.org/sdr/DALA2016031802075.md): Longeron · corroded · Mar 17, 2016 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 28LT BETWEEN BS 1231 TO BS 1240 AT AFT CARGO COMPARTMENT. FASTENERS AND CORROSION WERE REMOVED, REWORKED AREA WITHIN LIMITS WAS TREATED AND PAINTED, FASTENERS WERE INSTALLED IAW SRM 51-10-3 PAR 26, 21/14, 51-30-2, 53-02 PAR 13, 51-10-1.
- [SDR DALA2015041002735](https://openairdocs.org/sdr/DALA2015041002735.md): Wire Harness · damaged · Apr 10, 2015 · N934DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 20D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND THE SEAT HARNESS DAMAGED. THE WIRE HARNESS WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2015040602629](https://openairdocs.org/sdr/DALA2015040602629.md): Wire · broken · Apr 4, 2015 · N934DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE CONNECTOR. THE CONNECTOR WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION. LP 6466124
- [SDR DALA2014122406711](https://openairdocs.org/sdr/DALA2014122406711.md): Connector · damaged · Dec 24, 2014 · N934DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 34DE WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE CONNECTOR PIN. THE CONNECTOR WAS PINNED AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA14033830934](https://openairdocs.org/sdr/DALA14033830934.md): Latch · loose · Jun 4, 2014 · N934DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE UPPER RT RELEASE LATCH WAS VERY LOOSE. THE TAILCONE RELEASE LATCH ASSY AND CLAMP WERE BOTH REPLACED AND THEN RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA14033820934](https://openairdocs.org/sdr/DALA14033820934.md): Latch · out of limits · Jun 4, 2014 · N934DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE UPPER LEFT RELEASE LATCH WAS OUT OF ALLOWABLE RIG LIMITS. THE TAILCONE RELEASE LATCH ASSY WAS REPLACED AND THEN RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA14033800934](https://openairdocs.org/sdr/DALA14033800934.md): Door Frame · cracked · Jun 3, 2014 · N934DL · Doug MD88 · Fuselage Main, Structure
  > RIGHT OVERWING FRAME INSPECTION, BS 886, FOUND CRACKED. REPAIRED IAW AMDS 5310-01415-0202.
- [SDR DALA13071740934](https://openairdocs.org/sdr/DALA13071740934.md): Lanyard · unsecure · Dec 24, 2013 · N934DL · Doug MD88 · Emergency Equipment
  > CREW REPORTED THE R1 DOOR GIRT BAR LANYARD WAS NOT CONNECTED PROPERLY. REINSTALLED & SECURED R1 DOOR GIRT BAR LANYARD LATCH AS REQUIRED. OPS CHECKED GOOD IAW AMM 25-62.
- [SDR DALA13068280934](https://openairdocs.org/sdr/DALA13068280934.md): Wire · chafed · Dec 9, 2013 · N934DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN AFT CABIN WERE INOPERATIVE. MAINTENANCE FOUND A WIRE CHAFING, REPAIRED WIRE INSULATION, AND REPLACED THE BATTERY PACKS. OPS CHECKED NORMAL.
- [SDR DALA13052480934](https://openairdocs.org/sdr/DALA13052480934.md): Battery Pack · inoperative · Oct 13, 2013 · N934DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, THE AFT OVERWING EMERGENCY EXIT OVERHEAD LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD.
- [SDR DALA13052530934](https://openairdocs.org/sdr/DALA13052530934.md): Battery Pack · inoperative · Oct 12, 2013 · N934DL · Doug MD88 · Emergency Lighting
  > DURING ROUTINE LINE CHECK, THE CEILING EMERGENCY LIGHTS FROM ROW 22-36 WERE FOUND TO BE INOPERATIVE. REPLACED THE CABIN EMERGENCY LIGHT BATTERIES AMM 33-53 AND OPS CHECKED GOOD.
- [SDR DALA13052490934](https://openairdocs.org/sdr/DALA13052490934.md): Battery Pack · inoperative · Oct 11, 2013 · N934DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND LIGHTS INOPERATIVE AT ROW 25 AT BOTH AFT EMERGENCY EXIT DOORS. REPLACED BATTERY PACK ABOVE ROW 25 D/E IAW AMM 33-53-00. OPS CHECKS GOOD.
- [SDR DALA13050060934](https://openairdocs.org/sdr/DALA13050060934.md): Battery Pack · inoperative · Oct 3, 2013 · N934DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND IN THE GALLEY WERE INOPERATIVE. MX REPLACED BATTERY PACKS. OPS CHECKED GOOD.
- [SDR DALA13007550934](https://openairdocs.org/sdr/DALA13007550934.md): Latch · worn · Feb 12, 2013 · N934DL · Doug MD88 · Aerodynamic Fairings
  > UPPER LT AND RT TAILCONE RETENTION LATCHES WORN. REPLACED UPPER LT TAILCONE LATCH ASSY WITH PN 3913351 IAW AMM 53-53. BLENDED WORN PARTS W/IN LIMITS IAW DWG 4920459-3. INSTALLED LATCH RIGGING ACCOMPLISHED ON CARD 53-50-01077-0101. INSTALLATION IAW IPC 53-50-
- [SDR DALA13007480934](https://openairdocs.org/sdr/DALA13007480934.md): Skin · cracked · Feb 12, 2013 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED IN 5 EA AREAS 12" ABOVE PYLON STA 1380- CRACKED EMPENNAGE(HFEC -M-). REPAIRED IAW ER/A 511418-14, REV ORIGINAL. WORK ACCOMPLISHED ON PRI 511418-14 REV O AND REV 1.
- [SDR DALA13007470934](https://openairdocs.org/sdr/DALA13007470934.md): Frame · cracked · Feb 12, 2013 · N934DL · Doug MD88 · Fuselage Main, Frame
  > BS 1510 FRAME IS CRACKED AT 4:30 POS AT TAIL CONE ALINGMENT PIN--CRACKED EMPENNAGE (HFEC-M-). NR 128: REPAIRED IAW ERA 511420-14, REV ORIGINAL BY FRAME SECTION REPLACEMENT. WORK ACCOMPLISHED ON PRI 511420-14 REV O COINCIDES WITH FINAL ER/A 511420-14, REV ORIGI
- [SDR DALA13007030934](https://openairdocs.org/sdr/DALA13007030934.md): Skin · damaged · Feb 12, 2013 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON EXTERIOR SKIN 5:00 AND 5:30 POSITION AT BS 1510 JUST FWD OF TAIL CONE. REMOVED FASTENERS AND REMOVED PAINT AROUND DAMAGED AREA. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-04-1. TRIMMED OUT DAMAGE MAINTAINING ED AND.50" RADIUS IAW SRM 53
- [SDR DALA13006990934](https://openairdocs.org/sdr/DALA13006990934.md): Skin · cracked · Feb 7, 2013 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CROWN SKIN CRACKED AT BS 1447 BETWEEN S2-3L. CUT OUT CRACK WITH ONE INCH HOLE SAW. PERFORMED HFEC OF CUT OUT IAW NDT SPM 06-10-001. NO DEFECTS NOTED.
- [SDR DALA12015530934](https://openairdocs.org/sdr/DALA12015530934.md): Battery Pack · inoperative · Dec 8, 2012 · N934DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE LT OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE BATTERY PACK IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA1240280934](https://openairdocs.org/sdr/DALA1240280934.md): Longeron · cracked · Jul 4, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, A CRACK WAS FOUND ON LONGERON 8 RT ON STA Y=1307 AT PAX CABIN. DAMAGE AREA WAS CUT OUT AND NEW SECTION SPLICED IN IAW SRM 53-02 FIG 18.
- [SDR DALA1240260934](https://openairdocs.org/sdr/DALA1240260934.md): Beam · corroded · Jul 4, 2012 · N934DL · Doug MD88 · Fuselage Main, Structure
  > DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT LOWER BEAM STA Y=636-693. BLENDED AREA AND INSTALLED DOUBLER IAW SRM 53-05 FIG 123.
- [SDR DALA1240250934](https://openairdocs.org/sdr/DALA1240250934.md): Beam · corroded · Jul 4, 2012 · N934DL · Doug MD88 · Fuselage Main, Structure
  > DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT LOWER DOOR FRAME BEAM, BS Y=655 AND Y=674, AROUND SETSCREW HOLES. DAMAGE AREA WAS CUT OUT AND PLUGS INSTALLED IAW ER/A 504344-14 REV ORIG.
- [SDR DALA1240230934](https://openairdocs.org/sdr/DALA1240230934.md): Skin · corroded · Jul 4, 2012 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER FILLET PANEL FAIRING RUBSTRIPS BETWEEN STA Y=763-826 AND LONGERON 25 RT-30. FUSELAGE SKIN BLENDED OUT. INSTALLED DOUBLER REPAIR IAW SRM 53-04 PARA 57.
- [SDR DALA1238860934](https://openairdocs.org/sdr/DALA1238860934.md): Frame · cracked · Jun 25, 2012 · N934DL · Doug MD88 · Fuselage Main, Frame
  > DURING HMV, A CRACK WAS FOUND ON FUSELAGE FRAME OVERWING OF THE STA Y=864 AND X=55 AT THE CABIN FLOOR STRUCTURE. FRAME WAS REPLACED IAW DWG SR09530282 REV C.
- [SDR DALA1238670934](https://openairdocs.org/sdr/DALA1238670934.md): Skin · cracked · Jun 24, 2012 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CRACKS WERE FOUND LENGTH OF 0.109 INCH AND 0.125 INCH IN FUSELAGE SKIN FWD CARGO COMPARTMENT DOOR FWD UPPER CORNER AT BS 374 CLOSE TO DOOR FRAME EDGE. DAMAGE AREA WAS CUT OUT AND DOUBLERS FILLER INSTALLED IAW ERA 504233-14AD REV ORIG.
- [SDR DALA1238660934](https://openairdocs.org/sdr/DALA1238660934.md): Skin · cracked · Jun 24, 2012 · N934DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, A CRACK WAS FOUND IN FWD SERVICE DOOR CUTOUT FUSELAGE SKIN FWD UPPER CORNER AT BS 175.75, CLOSE TO DOOR JAMB EDGE WITH THE LENGTH OF 0.055 INCH. DAMAGE AREA WAS CUT OUT AND REPAIRED DOUBLERS FILLER. INSTALLED IAW SRM 53-05 FIG 112.
- [SDR DALA1238640934](https://openairdocs.org/sdr/DALA1238640934.md): Longeron · cracked · Jun 24, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, A CRACKED LONGERON WAS FOUND LONGERON 12 LT AT INTERSECTION WITH FRAME 1437. LONGERON WAS REMOVED FROM BS 1437 TO 1448 AND SPLICED IN NEW LONGERON IAW SRM 53-02 FIG 18.
- [SDR DALA1238630934](https://openairdocs.org/sdr/DALA1238630934.md): Longeron · cracked · Jun 24, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, A CRACK WAS FOUND ON LONGERON 4 LT AT INTERSECTION WITH FRAME BS 1437. REMOVED LONGERON FROM BS 1432 TO 1448 AND SLICED IN NEW LONGERON IAW SRM 53-02 FIG 18.
- [SDR DALA1236460934](https://openairdocs.org/sdr/DALA1236460934.md): Longeron · cracked · Jun 11, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, A CRACK WAS FOUND ON LONGERON 4 RT BS 541 OF INTERNAL FUSELAGE STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.
- [SDR DALA1236330934](https://openairdocs.org/sdr/DALA1236330934.md): Longeron · cracked · Jun 9, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV A CRACK WAS FOUND ON LONGERON 17 LT ON STA Y=275 AT PAX CABIN. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.
- [SDR DALA1236320934](https://openairdocs.org/sdr/DALA1236320934.md): Longeron · cracked · Jun 9, 2012 · N934DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV A CRACKED LONGERON 17 RT ON FRAME STA Y=389 AT PAX CABIN. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.

Next page: https://openairdocs.org/deregistered/N934DL-2019-08-22/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 = 'N934DL' AND deregistration_id = 'N934DL-2019-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N934DL-2019-08-22/reports

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