# Service difficulty reports: N912DL, cancelled Jun 27, 2024

A list on [N912DL, cancelled Jun 27, 2024](https://openairdocs.org/deregistered/N912DL-2024-06-27.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 · 185 reports

- [SDR DALA2020021701176](https://openairdocs.org/sdr/DALA2020021701176.md): Support Angle · cracked · Feb 16, 2020 · N912DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE LATCH SUPPORT ANGLES CRACKED @ 2:00, 8:00 & 10:00 3EA. RMVD & REPLACED CRACKED ANGLE @ 10:00 POSITION. INSTALLED LTCH SUPPORT ANGLES PER MD88 SRM 51-30-01 LOCATION @ 2:00 & 8:00 POSITION. (LP1492273)
- [SDR DALA2020021501170](https://openairdocs.org/sdr/DALA2020021501170.md): Frame · cracked · Feb 15, 2020 · N912DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE SUPPORT CANTED FRAME CRACKED AT 3:30, 8:00, 2:00. REMOVED FRAME AND BEGAN INSTALLING NEW FRAME PER DWG 5966769. COMPLETED INSTALL OF NEW FRAME PER DWG 5966769. (LP1490877)
- [SDR DALA2020021501169](https://openairdocs.org/sdr/DALA2020021501169.md): Frame · cracked · Feb 15, 2020 · N912DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE SUPPORT CANTED FRAMECRACKED AT (1) 3:30 (2) 8:00 (3) 2:00. REMOVED FRAME & BEGAN INSTALLING NEW FRAME PER DWG#5966769. COMPLETED INSTALL OF NEW FRAME PER DWG# 5966769. (LP1490796)
- [SDR DALA2020010650057](https://openairdocs.org/sdr/DALA2020010650057.md): Slide · dislodged · Jan 4, 2020 · N912DL · Doug MD88 · Escape Slide
  > DOOR 1L ENTIRE SLIDE PACK CAME OUT OF IT'S HOUSING WHEN DOOR WAS CLOSED FOR PUSHBACK. SLIDE DID NOT DEPLOY. REINSTALLED DOOR 1L SLIDE PACK IAW MD88 AMM 25-62 OK FOR SERVICE.(LP6657585)
- [SDR DALA2019052903280](https://openairdocs.org/sdr/DALA2019052903280.md): Control Cable · broken · May 28, 2019 · N912DL · Doug MD88 · Drag Control System
  > AIRPLANE ROLLED LEFT WITH SPOILER DEPLOYMENT WITH AUTOPILOT ON OR OFF ALL SPEEDS. ALSO FELT IT WHEN ACTUATING AILERONS WHILE FLYING MANUALLY (SOME LEFT ROLL PRESSURE WHEN AILERONS NEUTRAL). GND SPOILER F/D CHECK IS OK. DID FLIGHT AND GROUND SPOILER VISUAL CHEC
- [SDR DALA2019032701929](https://openairdocs.org/sdr/DALA2019032701929.md): Spar · cracked · Mar 27, 2019 · N912DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LT SIDE LEADING EDGE SPAR CHORD CRACK REPAIR / AMOC 17-088ER/A 557950-14AD REV A SUPPLEMENTAL INSPECTION RESTRICTION: ACCOMPLISH SECTION II: SUPPLEMENTAL INSPECTIONS, AT ACCRUEMENT OF 63,615 TOTAL AIRCRAFT FLIGHT CYCLES, AND EVERY 4,500 FLI
- [SDR DALA2018122437361](https://openairdocs.org/sdr/DALA2018122437361.md): Tab · damaged · Dec 21, 2018 · N912DL · Doug MD88 · Ailerons
  > RT WING AILERON CONTROL TAB TRAILING EDGE EXPOSED COMPOSITE. PAINTED RIGHT WING AILERON CONTROL TAB PER MD-88 SRM-51-10-3B. PERFORMED RIGHT WING AILERON CONTROL TAB SATISFACTORY WEIGHT AND BALANCE PER MD-88 SRM 57-50-1. REMOVAL AND INSTALLATION OF RIGHT WING
- [SDR DALA2018122437360](https://openairdocs.org/sdr/DALA2018122437360.md): Tab · damaged · Dec 21, 2018 · N912DL · Doug MD88 · Ailerons
  > LT WING AILERON CONTROL TAB TRAILING EDGE EXPOSED COMPOSITE. PAINTED LEFT WING AILERON CONTROL TAB PER MD-88 SRM 51-10-3B. PERFORMED LEFT WING AILERON CONTROL TAB SATISFACTORY WEIGHT AND BALANCE PER MD-88 SRM 57-50-1. REMOVAL AND INSTALLATION OF LEFT WING AIL
- [SDR DALA2018122107324](https://openairdocs.org/sdr/DALA2018122107324.md): Skin · delaminated · Dec 21, 2018 · N912DL · Doug MD88 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE INLET COWL INTERIOR HAS DELAMINATED AREA AT AFT END OF COWL, 7 OCLOCK POSITION. REPLACED #2 ENG INLET COWL IAW MD-88-AMM-71-10-01 LEAK CHECKED SATISFACTORY ANTI-ICE CONNECTION ON #2 ENG INLET COWL IAW MD-88-AMM-71-10-01. (LP0872635)
- [SDR DALA2018122107323](https://openairdocs.org/sdr/DALA2018122107323.md): Skin · cracked · Dec 20, 2018 · N912DL · Doug MD88 · Passenger/Crew Doors
  > TASKCARD 5211-2537 - L1 DOOR FUSELAGE SKIN AFT #5 DOORSTOP ADJUST HOLE, STA Y=200, CRACKED APROX 0.125" LONG 37-001. REPAIRED FUSELAGE SKIN AT L1 DOOR JAMB AFT #15 DOOR STOP HOLE. CUT OUT DIM 1.7"X3.7" IAW MD88 SRM 53-05 FIG 114 PAR 131. THIS IS A CATEGORY B R
- [SDR DALA2018122007299](https://openairdocs.org/sdr/DALA2018122007299.md): Tab · debonded · Dec 19, 2018 · N912DL · Doug MD88 · Elevator, Tab Structure
  > RT HORIZ STAB CENTER GEARED TAB HAS DISBANDED COMPOSITE REPAIR ON TE DOT 003/96. REMOVED & INSTALLED OF RIGHT HORIZ. STAB GEAR TAB IAW DELTA 2730-4130-RH REPAIRED RIGHT HORIZ. STAB GEAR TAB IAW -MD-88-SRM- 51-70-02D PARA E(7,8,13,15) WEIGHED RIGHT HORIZ. STAB
- [SDR DALA2018072304601](https://openairdocs.org/sdr/DALA2018072304601.md): Battery · discharged · Jul 20, 2018 · N912DL · Doug MD88 · Emergency Lighting
  > EMERERGENCY CELLING LIGHTS ARE INOPERATIVE ROW 31 TO THE TAIL. B5-107 BATTERIES DEAD. THE BATTERIES WERE REPLACED PER AMM 33-53. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA2018062304164](https://openairdocs.org/sdr/DALA2018062304164.md): Lanyard · broken · Jun 23, 2018 · N912DL · Doug MD88 · Emergency Equipment
  > FOUND 1L DOOR SLIDE GIRT BAR LANYARD BROKEN. REPLACED 1L DOOR LANYARD.
- [SDR DALA2018052403538](https://openairdocs.org/sdr/DALA2018052403538.md): Light · inoperative · May 23, 2018 · N912DL · Doug MD88 · Emergency Lighting
  > DOOR R1 EMERGENCY LIGHT INOP. RELAMPED OPS CHECK GOOD IAW AMM 33-51.
- [SDR DALA2018050403059](https://openairdocs.org/sdr/DALA2018050403059.md): Engine · failed · May 3, 2018 · N912DL · Doug MD88 · Engine (Turbine/Turboprop)
  > ATB/IFSD TO RIC DUE TO A RIGHT ENGINE FAILURE. CREW REPORTED AT 900 FT HEARD A BANG ENGINE ROLLED BACK AND EGT SPIKED. PER QRH SHUT DOWN ENGINE AND RETURNED. FIREBALL REPORTED BY WITNESS ON GROUND. SUBSEQUENT FIRE IN FIELD OFF OF DEPARTURE END OF RUNWAY. MTC F
- [SDR DALA2018041802593](https://openairdocs.org/sdr/DALA2018041802593.md): Unknown · odor · Apr 17, 2018 · N912DL · Doug MD88 · Air Distribution System
  > CLIMBING THROUGH FL90, FLIGHT ATTENDANT REPORTED STRONG SMOKEY ODOR IN THE MID CABIN. CREW RAN QRH AND ODOR DISSIPATED. ON RESUMPTION OF CLIMB POWER ODOR RETURNED. RETURNED TO DEPARTURE. MAINTENANCE PERFORMED THE NO GO ODI PREVENTION WORK CARDS 2120-2367 A
- [SDR DALA2017110708007](https://openairdocs.org/sdr/DALA2017110708007.md): B-Nut · leaking · Nov 6, 2017 · N912DL · Doug MD88 · Hydraulic System, Main
  > FLIGHT ATTENDANTS REPORTED FUMES IN CABIN AFTER TAKEOFF. FOUND THE LT A/C COMPARTMENT B-NUT ON A HYD FUSE LEAKING NEAR FILTER PACK. TIGHTENED THE B-NUT.
- [SDR DALA2017102807845](https://openairdocs.org/sdr/DALA2017102807845.md): Skin · cracked · Oct 27, 2017 · N912DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN, ONE INCH FWD OF THE LT CANT BS 1474 AT VENTRAL STAIR CUTOUT. COMPLIED WITH ERA 562986-14, REV ORIG.
- [SDR DALA2017102407753](https://openairdocs.org/sdr/DALA2017102407753.md): Battery Pack · inoperative · Oct 23, 2017 · N912DL · Doug MD88 · Emergency Lighting
  > FWD UPPER EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES IAW AMM 33-53-00. CHECKED GOOD.
- [SDR DALA2017072405644](https://openairdocs.org/sdr/DALA2017072405644.md): Battery Pack · inoperative · Jul 21, 2017 · N912DL · Doug MD88 · Emergency Lighting
  > DURING A SERVICE CHECK, FOUND SEAT ROWS 1-3, 10-12 AND FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK.
- [SDR DALA2017072005590](https://openairdocs.org/sdr/DALA2017072005590.md): Sign · inoperative · Jul 19, 2017 · N912DL · Doug MD88 · Emergency Lighting
  > EMERGENCY EXIT SIGNS INOPERATIVE. SECURED EMER EXIT SIGN. OPN CKS NORM.
- [SDR DALA2017062104857](https://openairdocs.org/sdr/DALA2017062104857.md): Light · illuminated · Jun 20, 2017 · N912DL · Doug MD88 · Landing Gear Position and Warning
  > GEAR DOOR OPEN LIGHT ILLUMINATED IN CRUISE. PER QRH, ALTERNATE GEAR EXTEND USED FOR LANDING. REPLACED L1-122 MAIN GEAR OPEN LIGHT ASSEMBLY. JACKED A/C AND COMPLETED MULTIPLE GEAR SWINGS WHILE COMPLYING WITH POSITION AND WARNING INDICATION TEST. POSITIVE RESULT
- [SDR DALA2017061604756](https://openairdocs.org/sdr/DALA2017061604756.md): Battery Pack · inoperative · Jun 16, 2017 · N912DL · Doug MD88 · Emergency Lighting
  > LEFT & RIGHT AFT OVERWING EXIT IDENTIFIER LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM IAW 33-53. OPS CHECKED GOOD.
- [SDR DALA2017052404146](https://openairdocs.org/sdr/DALA2017052404146.md): Unknown · odor · May 23, 2017 · N912DL · Doug MD88 · Air Distribution System
  > DURING CLIMB AT FL 260, THE AUTOTHROTTLES DISCONNECTED WITH ERRONEOUS EPR READINGS ON THE RIGHT ENGINE. FLIGHT ATTENDANTS ADVISED ELECTRICAL, PLASTIC BURNING ODOR IN THE FORWARD GALLEY AND FAINT ODOR NOTICED IN COCKPIT. COMPLIED WITH WORK CARD 2120-2367. CO
- [SDR DALA2019032901992](https://openairdocs.org/sdr/DALA2019032901992.md): Spar · cracked · Apr 24, 2017 · N912DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LT SIDE LEADING EDGE SPAR CHORD CRACK REPAIR AMOC 17-088. ER/A 557950-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, LOGPAGE TERMINATED. (LP2989956)
- [SDR DALA2017042303313](https://openairdocs.org/sdr/DALA2017042303313.md): Structure · cracked · Apr 22, 2017 · N912DL · Doug MD88 · Vertical Stabilizer
  > CRACK INDICATION ON BOLT HOLE FOR THE LT SIDE OF THE VERTICAL STAB L/E ZFS 52.267. REPAIRED IAW DWG SG 09550005-7001.
- [SDR DALA2017011600384](https://openairdocs.org/sdr/DALA2017011600384.md): Heater · failed · Jan 14, 2017 · N912DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > WITH ANTI FOG SWITCH ON, CAPTAINS SLIDING WINDOW GOT EXCESSIVELY HOT. WINDOW STARTED WARPING, AND BECAME SOFT. ALSO HAD A SMALL BURNING ODOR. WITH ANTI FOG OFF, THE BURNING ODOR WENT AWAY. R & R CAPTAINS SLIDING WINDOW IAW AMM 56-10. OPS CHECKED GOOD, NO BUR
- [SDR DALA2016122009972](https://openairdocs.org/sdr/DALA2016122009972.md): Support · corroded · Dec 19, 2016 · N912DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > MAIN LANDING GEAR/WHEEL WELL, CORROSION AND SCRATCHES ON BEARING OF RT MLG RETRACT ACTUATOR UPPER SUPPORT. BEARING WAS REPLACED PER CMM 20-10-17 AND ER/A 552856-14 AD REV ORIGINAL.
- [SDR DALA2016121809935](https://openairdocs.org/sdr/DALA2016121809935.md): Skin · damaged · Dec 17, 2016 · N912DL · Doug MD88 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN: WAVY PREVIOUS REPAIR FROM STA Y=181 TO Y=228 BTW LONG 22R TO 26R. DAMAGE PREVIOUS REPAIR WAS REMOVED AND REPLACED FOR NEW ONE CORRECT REPAIR PER SRM 53-04 FIGURE 12C. PERFORM EXTERNAL VISUAL INSPECTION THRESHOLD 8000 LANDINGS AND REPETI
- [SDR DALA2016121709930](https://openairdocs.org/sdr/DALA2016121709930.md): Release Mech · defective · Dec 16, 2016 · N912DL · Doug MD88 · Aerodynamic Fairings
  > DURING "OK TO INSTALL EVACUATION SLIDE" WERE FOUND SEVERAL DISCREPANCIES: ACTIVATED POSITION OF TAIL CONE RELEASE CAM, OVER TENSIONED TAIL CONE RELEASE MECHANISM CONTROL CABLES AND MISSING LUBE SAME CONTROL CABLES/PADS GUIDE PIN. TAILCONE WAS REMOVED PER AMM 5
- [SDR DALA2016121510193](https://openairdocs.org/sdr/DALA2016121510193.md): Skin · damaged · Dec 14, 2016 · N912DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN DAMAGED AROUND AFT LH LAV SERVICE. REPAIRED IAW ERA 551757-14.
- [SDR DALA2016121509883](https://openairdocs.org/sdr/DALA2016121509883.md): Access Panel · corroded · Dec 14, 2016 · N912DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RT WING HEATER BLANKET CUT OUT OF ACCESS PANEL. REPLACED IAW AMM 30-80-02, PAGE 401, PAR 2.A.
- [SDR DALA2016121409848](https://openairdocs.org/sdr/DALA2016121409848.md): Skin · corroded · Dec 13, 2016 · N912DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN BS 1170, LONGERON 18 - 19L. REPAIRED IAW ETI-88-16-453 REV. 2 AND ER/A 552819-14 REV. ORIG.
- [SDR DALA2016121309795](https://openairdocs.org/sdr/DALA2016121309795.md): Frame · cracked · Dec 12, 2016 · N912DL · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORY COMPARTMENT, HAS A CRACK ON FRAME BS 1510. REPLACED IAW SRM 51-30-2 AND DWG 9911843-5 REV AC.
- [SDR DALA2016121209784](https://openairdocs.org/sdr/DALA2016121209784.md): Latch · corroded · Dec 11, 2016 · N912DL · Doug MD88 · Service Doors
  > CORROSION AROUND OF INTERNAL SIDE ON LATCHES AND CLIP AT AFT SERVICE PANEL DOOR AMDS 5300-2960. SERVICE PANEL DOOR WAS REPLACED PER SRM 51-30-5.
- [SDR DALA2016121209782](https://openairdocs.org/sdr/DALA2016121209782.md): Support Fitting · corroded · Dec 11, 2016 · N912DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > HIDDEN DAMAGE. AFTER NUT REMOVAL ON RT MLG SUPPORT FITTING INBD LOWER STUD CORROSION WAS FOUND. LOWER STUD ON RT MLG SUPPORT FITTING WAS REMOVED AND INSTALLED PER AMM 20-30-01 AND 20-10-14, AFTER STUD REMOVAL CORROSION WAS FOUND ON FITTING BORE AND WAS ATTENDE
- [SDR DALA2016121009778](https://openairdocs.org/sdr/DALA2016121009778.md): Beam · corroded · Dec 9, 2016 · N912DL · Doug MD88 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT, CORROSION ON DOOR JAMB BEAM BTW STA Y=1155 TO 1212 LONG 27R TO 28R. DOOR JAMB BEAM BTW STA Y=1155 TO 1212 LONG 27R TO 28R WAS REPAIRED PER SRM 51-30-5 AND SRM 53-05 FIG 123.
- [SDR DALA2016121009776](https://openairdocs.org/sdr/DALA2016121009776.md): Cusp Web · corroded · Dec 9, 2016 · N912DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER AND LOWER CUSP WEBS FROM STA Y=1150 TO Y=1174 BTW X= 60 TO X=44. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A-21.
- [SDR DALA2016120909711](https://openairdocs.org/sdr/DALA2016120909711.md): Door Frame · corroded · Dec 9, 2016 · N912DL · Doug MD88 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT, CORROSION ON DOOR JAMB WEB BTW STA Y=1150 TO Y=1270 BTW LONG 30 TO 24R. FITTINGS STA-Y: 1255, Y: 1212, STRAPS STA Y: 1220, Y: 1245 AND WEB WERE REMOVED AND INSTALL NEW WEB PER SRM 51-30-2, 51-30-5 AND DWG 5936442 REV A.
- [SDR DALA2016120909709](https://openairdocs.org/sdr/DALA2016120909709.md): Frame · cracked · Dec 8, 2016 · N912DL · Doug MD88 · Fuselage Main, Frame
  > CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB AT RT OVERWING FRAME STA Y=864 STA: 00441. FRAME WAS REPLACED PER SRM 51-10-4, SRM 51-30-5, SRM 51-30-2 AND CARD REPLACE SECTION OVERWING FRAME 5310-01415-0302.
- [SDR DALA2016120809686](https://openairdocs.org/sdr/DALA2016120809686.md): Skin · corroded · Dec 7, 2016 · N912DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON THE RT HORIZONTAL STABILIZER SKIN BARREL NUT HOLE 14 AND 16. REPAIRED IAW ETI-88-16-438 REV. 1 AND ER/A 551763-14 REV ORIG.
- [SDR DALA2016120809684](https://openairdocs.org/sdr/DALA2016120809684.md): Longeron · cracked · Dec 7, 2016 · N912DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 3L, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.
- [SDR DALA2016120809679](https://openairdocs.org/sdr/DALA2016120809679.md): Longeron · cracked · Dec 7, 2016 · N912DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT ACCESORY BAY HAS A CRACKED LONGERON 5R BS 1437. THE LONGERON WAS REPAIRD IAW SRM 53-02 FIG 18.
- [SDR DALA2016120709673](https://openairdocs.org/sdr/DALA2016120709673.md): Skin · delaminated · Dec 6, 2016 · N912DL · Doug MD88 · Wing, Plate/Skin
  > RIGHT WING HAD A DELAMINATED OTBD TE PANEL XA=429-434. REPAIRED IAW ERA 551768-14 REV ORIGINAL.
- [SDR DALA2016120709647](https://openairdocs.org/sdr/DALA2016120709647.md): Skin · corroded · Dec 6, 2016 · N912DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON THE LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 15,14, AND 13. REPAIRED IAW ETI 88-16-437 REV 1 AND ER/A 551718-14 REV ORIG.
- [SDR DALA2016120709646](https://openairdocs.org/sdr/DALA2016120709646.md): Longeron · corroded · Dec 6, 2016 · N912DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 22L, BS 1319 AT AFT CARGO BAY. THE LONGERON WAS REPLACED IAW SRM 53-02 FIGURE 18.
- [SDR DALA2016120609604](https://openairdocs.org/sdr/DALA2016120609604.md): Intercostal · corroded · Dec 5, 2016 · N912DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BS 1308 - 1361 BETWEEN RBL 17 AND LBL 17. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1 AND DWG 9936656 REV. AM.
- [SDR DALA2016120609602](https://openairdocs.org/sdr/DALA2016120609602.md): Floorbeam · corroded · Dec 5, 2016 · N912DL · Doug MD88 · Fuselage Main, Floor Beam
  > AFT WET AREA HAD CORROSION ON THE FLOORBEAM BS 1338 BETWEEN RBL 60 TO LBL 60. THE FLOORBEAM WAS REPLACED IAW SRM 51-70-5 FIG 1 (SHEET 2).
- [SDR DALA2016120509535](https://openairdocs.org/sdr/DALA2016120509535.md): Door Frame · cracked · Dec 4, 2016 · N912DL · Doug MD88 · Fuselage Main, Structure
  > DURING NDT INSPECTION WAS FOUND WITH DISCREPANT AREA AT FWD SERVICE DOOR FRAME UPPER FWD CORNER. REPAIRED IAW ERA 551775-14AD REV. ORIGINAL SECTION II.
- [SDR DALA2016120509596](https://openairdocs.org/sdr/DALA2016120509596.md): Frame · cracked · Dec 2, 2016 · N912DL · Doug MD88 · Fuselage Main, Frame
  > AFT WET AREA HAS A CRACKED FRAME BS 1322 AND LONGERON 17L. REPAIRED THE FRAME IAW ER/A 493697-14MA REV.B.

Next page: https://openairdocs.org/deregistered/N912DL-2024-06-27/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 = 'N912DL' AND deregistration_id = 'N912DL-2024-06-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N912DL-2024-06-27/reports

---
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