# Service difficulty reports: N992DL, cancelled Dec 30, 2022

A list on [N992DL, cancelled Dec 30, 2022](https://openairdocs.org/deregistered/N992DL-2022-12-30.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 5 · 202 reports

- [SDR DALA2019040802290](https://openairdocs.org/sdr/DALA2019040802290.md): Frame · cracked · Apr 8, 2019 · N992DL · Doug MD88 · Aerodynamic Fairings
  > AFT TAIL CONE CTR FRAME CRACKED AT GUIDE PIN 4:00. REMOVED R/H LWR CANTED FRAME. DRILLED NEW CANTED FRAME. INSTALLED R/H LWR TAIL CONE CANTED FRAME PER DWG 9911843.
- [SDR DALA2018091005506](https://openairdocs.org/sdr/DALA2018091005506.md): Battery · discharged · Sep 10, 2018 · N992DL · Doug MD88 · Emergency Lighting
  > TAIL COMPARTMENT WALKWAY CENTER EMERGENCY LIGHT OUT. REFERENCED WDM 33-51-13. FOUND NO POWER AT LAMP. REPLACED BATTERIES IN POWER SUPPLY B5-28 (LOCATED IN AFT RIGHT LAVATORY CEILING). OPS CHECK OK. PN'S OFF AND ON TWO 41B004AD07G3 BATTERIES.
- [SDR DALA2018082705251](https://openairdocs.org/sdr/DALA2018082705251.md): Slat · damaged · Aug 27, 2018 · N992DL · Doug MD88 · Leading Edge Devices
  > NR 1 LEFT SLAT WAS DAMAGED. REPLACED THE SLAT IAW W/C 2700-4224-LH-01.
- [SDR DALA2018082805309](https://openairdocs.org/sdr/DALA2018082805309.md): Structure · damaged · Aug 20, 2018 · N992DL · Doug MD88 · Wing Main, Frame Structure
  > DURING A WALK AROUND, FOUND THE GAUGE ON THE LT WING L/E UNDER SLAT NR 1, XFS 136. COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER IAW SRM 57-06B, FIG 13. COMPLETED INSTALLATION OF REPAIR IAW SRM 57-06B, FIG 31
- [SDR DALA2018061604037](https://openairdocs.org/sdr/DALA2018061604037.md): Control Cable · severed · Jun 15, 2018 · N992DL · Doug MD88 · Landing Gear Steering System
  > TAKING THE RUNWAY LOST ALL STEERING TO THE RIGHT VIA THE TILLER. FOUND NOSE WHEEL STEERING CONTROL CABLE 123A SEVERED. REMOVED AND REPLACED 123A REF AMM 32-51. PERFORMED STEERING TEST REF AMM 32-52. CKS NML.
- [SDR DALA2018011200223](https://openairdocs.org/sdr/DALA2018011200223.md): Door Frame · cracked · Jan 11, 2018 · N992DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL LT. DOOR JAMB FWD WHEEL WELL LT ( PAN) WAS REPLACED PER DC9/MD80 SRM 51-30-2 AND 51-30-5.
- [SDR DALA2018011100192](https://openairdocs.org/sdr/DALA2018011100192.md): Door Frame · cracked · Jan 10, 2018 · N992DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL RT. DOOR JAMB FWD WHEEL WELL RT ( PAN) WAS REPLACED PER SRM 51-30-02 AND 51-30-05.
- [SDR DALA2017112008216](https://openairdocs.org/sdr/DALA2017112008216.md): Power Supply · inoperative · Nov 18, 2017 · N992DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS FOR SEATS ROWS 31 AFT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERIES IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017111508158](https://openairdocs.org/sdr/DALA2017111508158.md): Wire · shorted · Nov 14, 2017 · N992DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHTS FOR SEATS 31-36 WILL NOT WORK IN TEST MODE. REPLACED AFT EMERGENCY LIGHTS BATTERY AND CHARGER, B5-212, IAW AMM 33-53. REPAIRED A SHORTED WIRE L902T14 IAW WDM 33-51-14. THE SYSTEM CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017030801876](https://openairdocs.org/sdr/DALA2017030801876.md): Support Fitting · worn · Mar 7, 2017 · N992DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE CAM MECHANISM SUPPORT FITTING WORN, AND FAILED TORQUE CHECK. REMOVED THE TAIL CONE SUPPORT FITTING AND REPLACED THE SHAFT AND SUPPORT FITTING IAW AMM 53-53-02 AND AMDS 5350-010770101.
- [SDR DALA2016091906708](https://openairdocs.org/sdr/DALA2016091906708.md): Skin · deteriorated · Sep 8, 2016 · N992DL · Doug MD88 · Rudder, Plate/Skin
  > FLAME SPRAY DETERIORATED ON RUDDER WITHIN 7" OF FORWARD SPAR ON BOTH SIDES. R & R RUDDER.
- [SDR DALA2016032902418](https://openairdocs.org/sdr/DALA2016032902418.md): Light · damaged · Mar 28, 2016 · N992DL · Doug MD88 · Emergency Lighting
  > THE FLIGHT CREW FOUND EMERGENCY LIGHTS DAMAGED. MAINTENANCE RESECURED THE EMERGENCY EXIT LIGHT AT DOOR R1 AND THE FORWARD EMERGENCY EXIT FLOOR LIGHT IN THE G2 GALLEY.
- [SDR DALA2016021201015](https://openairdocs.org/sdr/DALA2016021201015.md): Fan · failed · Feb 11, 2016 · N992DL · Doug MD88 · Air Distribution Fan
  > F/A NOTICED AN ACRID ODOR AT 1300 FT ON ARRIVAL. TURNED OFF ALL CABIN LIGHTS, ODOR DISSAPATED YET NEVER WENT AWAY. W/C 2120-2367, FOUND RECIRCULATION FAN WITH SMOKE ODOR AND EXCESSIVE VIBRATION. R & R RECIRCULATION FAN IAW AMM 21-20, CONTACTED OK FOR SERVIC
- [SDR DALA2015122007681](https://openairdocs.org/sdr/DALA2015122007681.md): Spar Cap · damaged · Dec 19, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > PREVIOUS TOOL DAMAGE ON NEW RT HORIZONTAL STABILIZER REAR SPAR UPPER CAP XHS=115. REAR SPAR UPPER CAP WAS REPAIRED IAW ER/A 541579-14AD, REV ORIGINAL ETI-88-15-435, REV 2.
- [SDR DALA2015122107683](https://openairdocs.org/sdr/DALA2015122107683.md): Pan · cracked · Dec 18, 2015 · N992DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR. OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR, C3 WAS REPAIRED IAW ERA 541561-14, REV ORIG PERMANENT REPAIR.
- [SDR DALA2017121208526](https://openairdocs.org/sdr/DALA2017121208526.md): Spar Cap · damaged · Dec 16, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > MD88 - STABILIZERS / H.S. / RH REAR SPAR UPPER CAP, XHS 115 / TOOLING DAMAGE. DTA MONITOR INSPECTION LOG REFERENCE ER/A 541579-14AD SECTION II REQUIRES DTA APPROVAL WITHIN 24 MONTHS AFTER SECTION I. ER/A 541579-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED,
- [SDR DALA2015121707657](https://openairdocs.org/sdr/DALA2015121707657.md): Pan · cracked · Dec 16, 2015 · N992DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INNER PAN BS 370. INNER PAN WAS REPAIRED IAW ER/A 541559-14, REV ORIG.
- [SDR DALA2015121707656](https://openairdocs.org/sdr/DALA2015121707656.md): Hinge · damaged · Dec 16, 2015 · N992DL · Doug MD88 · Fuselage, Door Hinge
  > ELONGATED HOLES ON FWD/AFT HINGE AT MID CARGO COMPARTMENT DOOR. FWD/AFT HINGES AT MID CARGO COMPARTMENT DOOR WERE REPLACED THEREFORE HINGES ARE OUT OF LIMITS IAW MD-88 52-31- 02 AND ER/A 497387-14MA, REV B. ADJUST AND TEST WILL BE ACCOMPLISHED WITH CARD 5200
- [SDR DALA2015121707653](https://openairdocs.org/sdr/DALA2015121707653.md): Floor Panel · delaminated · Dec 16, 2015 · N992DL · Doug MD88 · Fuselage Floor Panel
  > DELAMINATED AND DAMAGED FLOOR PANEL BS 1231 - 1338. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.
- [SDR DALA2015121707652](https://openairdocs.org/sdr/DALA2015121707652.md): Support Fitting · corroded · Dec 16, 2015 · N992DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON LT RETRACT ACTUATOR SUPPORT FITTING BORE. REPAIRED IAW DWG SR09570087, REV B.
- [SDR DALA2015121707651](https://openairdocs.org/sdr/DALA2015121707651.md): Support Fitting · corroded · Dec 16, 2015 · N992DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON RT MLG RETRACT ACTUATOR SUPPORT FITTING BUSHING VERTICAL FACE AND BORE. REPAIRED IAW DWG SR09570087, REV B.
- [SDR DALA2015121407583](https://openairdocs.org/sdr/DALA2015121407583.md): Access Panel · corroded · Dec 13, 2015 · N992DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION AT SETTLEMENT AND COUNTER SKIN AREAS OF FUEL ACCESS PANEL 1466C. FUEL ACCESS 1466C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00-05B AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.
- [SDR DALA2015121407588](https://openairdocs.org/sdr/DALA2015121407588.md): Rib · damaged · Dec 12, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > ELONGATED HOLE ON RIB AT RT HORIZONTAL STABILIZER OUTER CONSTANT SECTION REAR SPAR BS XH=27.234 ELONGATED HOLE WAS REPAIR IAW ETI-88-15-418 AND ER/A 541547-14, REV ORIGINAL.
- [SDR DALA2015121307579](https://openairdocs.org/sdr/DALA2015121307579.md): Structure · corroded · Dec 12, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer Structure
  > CORROSION ON BARREL NUT HOLE NR 13, BS XM=27.234 AT LT HORIZONTAL STABILIZER. BARREL NUT NR 13 AT LT HORIZONTAL STABILIZER WAS REMOVED IAW AMM 20-10-14 CORROSION WAS REMOVED IAW ER/A 541539-14, REV ORIGINAL. BUSHING WAS FABRICATED AND INSTALLED IAW ER/A REV
- [SDR DALA2015121307578](https://openairdocs.org/sdr/DALA2015121307578.md): Cusp Web · corroded · Dec 12, 2015 · N992DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB LOWER SURFACE BETWEEN X= 54-X=60 AND BETWEEN BS 627-632, 636-641 AND 648-653. CUSP WEB X 54, 522 TO 788 WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9930538, REV CF.
- [SDR DALA2015121207576](https://openairdocs.org/sdr/DALA2015121207576.md): Spar Cap · cracked · Dec 11, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON HORIZONTAL STABILIZER RT REAR SPAR CAP AT CRITICAL HOLE CARD. REAR CAP WAS REPLACED IAW DWG 09550030, REV C AND SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR DALA2015121207574](https://openairdocs.org/sdr/DALA2015121207574.md): Access Panel · corroded · Dec 11, 2015 · N992DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1335C. FUEL ACCESS 1335C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0120, JOB 001-0445.
- [SDR DALA2015121207573](https://openairdocs.org/sdr/DALA2015121207573.md): Tripler · punctured · Dec 11, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PUNCTURED PREVIOUS REPAIR TRIPLER ON AFT LAVATORY SERVICE PANEL CUTOUT. REPLACE REPAIR TRIPLER IAW ER/A 529789-14, REV A AND SRM 51-30-2 AND 51-30-5.
- [SDR DALA2015121207572](https://openairdocs.org/sdr/DALA2015121207572.md): Hinge · cracked · Dec 11, 2015 · N992DL · Doug MD88 · Spoilers
  > CRACK INBD HINGE FITTING AT LT GROUND SPOILER BS XW=47.450, REAR SPAR WING RIB. REAR SPAR WING RIB WAS REPLACED IAW SRM 51-30-2, 51-30-1 AND DWG 5936830-501.
- [SDR DALA2015121207571](https://openairdocs.org/sdr/DALA2015121207571.md): Structure · damaged · Dec 11, 2015 · N992DL · Doug MD88 · Horizontal Stabilizer Structure
  > TOOL DAMAGE ON BARREL NUT HOLE NR 8 AT RT HORIZONTAL STABILIZER BS XH=27.234. BARREL NUT WAS REMOVED IAW AMM 20-10-14. NEW BUSHING WAS FABRICATED IAW ER/A 541558-14, REV ORIGINAL AND NEW BUSHING WAS INSTALLED IAW 541558-14, REV ORIGINAL AND NEW BARREL NUT WA
- [SDR DALA2015121107538](https://openairdocs.org/sdr/DALA2015121107538.md): Access Panel · corroded · Dec 10, 2015 · N992DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1472C. FUEL PANEL WAS REPLACED.
- [SDR DALA2015121007488](https://openairdocs.org/sdr/DALA2015121007488.md): Splice · loose · Dec 9, 2015 · N992DL · Doug MD88 · Vertical Stabilizer
  > LOOSE FASTENERS ON SPLICE OF L/E AT VERTICAL STABILIZER BS ZFS=52.26. ALL HOLES COUNTERSINK WERE MEASURED IAW CARD 5530-01045-05, STEP 2, JOB 055-0001 AND WAS FOUND OUT OF LIMITS, 49 EA. REPAIRED IAW CARD 5530-01045-08, STEP 1, JOB 167-0001 AND SRM 55-03D,
- [SDR DALA2015121007487](https://openairdocs.org/sdr/DALA2015121007487.md): Doubler · corroded · Dec 9, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER RADIO ALTIMETER ANTENNA SETTLEMENT CUTOUT BS 724 TO 714. PRODUCTION DOUBLER DUE TO EXCECESIVE CORROSION WAS REPLACED IAW DWG 5911412-309, REV DV AND 51-30-5, 51-30-2.
- [SDR DALA2015120907470](https://openairdocs.org/sdr/DALA2015120907470.md): Slat Track · worn · Dec 8, 2015 · N992DL · Doug MD88 · Leading Edge Devices
  > WEAR RT WING SLAT TRACK 13. SLAT TRACK 13 AT RT WING WAS REPLACED IAW AMM 27-80-00.
- [SDR DALA2015120907469](https://openairdocs.org/sdr/DALA2015120907469.md): Slat Track · worn · Dec 8, 2015 · N992DL · Doug MD88 · Leading Edge Devices
  > WEAR ON FLANGES OF LT WING SLAT TRACKS 7, 9 AND 13. LT WING SLAT TRACKS 7, 9 AND 13 WERE REPLACED IAW AMM 27-80-00.
- [SDR DALA2015120907461](https://openairdocs.org/sdr/DALA2015120907461.md): Access Panel · corroded · Dec 8, 2015 · N992DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION OUT OF LIMITS ON 2 COUNTERSINK HOLES ON FUEL ACCESS PLATE NR. 1371C. SRM 51-22-2A. FUEL ACCESS PLATE AND BUSHINGS WERE TREATED IAW SRM 51-10-3, NEW BUSHINGS WERE INSTALLED.
- [SDR DALA2015120907460](https://openairdocs.org/sdr/DALA2015120907460.md): Frame · corroded · Dec 8, 2015 · N992DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME 1380 BETWEEN BS 24L-24R. FRAME WAS REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-4, 53-01 FIG 1.
- [SDR DALA2015120907468](https://openairdocs.org/sdr/DALA2015120907468.md): Skin · dented · Dec 7, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN BS 148 BETWEEN LONGERON 24 LT ON LONG 25 LT. FOUND WITHIN LIMITS IAW SRM 53-04-1, PARR 7E CONDITION 1B.
- [SDR DALA2015120907467](https://openairdocs.org/sdr/DALA2015120907467.md): Skin · damaged · Dec 7, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PROTRUSION ON EXTERNAL FUSELAGE, SKIN BS 200-207 BETWEEN LONGERON 30-29 LT ALSO 214 LONGERON 28-29 LT. DENTS ON FUSELAGE SKIN WERE MEASURED PRESENTING THE FOLLOWING CONDITIONS: BS 200-207, LONGERON 29-30 LT X= DEPTH= 0.042 ", D= DIMENTION= 1.500". D/X = 1.56
- [SDR DALA2015120907466](https://openairdocs.org/sdr/DALA2015120907466.md): Skin · damaged · Dec 7, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON AFT EDGE AT WINDOW BELT NR 57 EXTERNAL FUSELAGE SKIN. DAMAGE WAS REMOVED, MEASURED AND TREATED IAW 53-05, FIG 111, SHEET 10 AND 51-10-3 PAR-21. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK IAW TOPP 30-10-70 PAR I PAGE 13.
- [SDR DALA2015120807451](https://openairdocs.org/sdr/DALA2015120807451.md): Pan · cracked · Dec 7, 2015 · N992DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED REPAIR DOUBLER ON FORWARD UPPER PAN AT FORWARD PASSENGER DOOR LT. FORWARD UPPER PAN AT FWD PASSENGER DOOR L1 WAS REPLACE IAW SRM 51-30-4, 51-30-1, 51-30-2 AND DWG 591421, REV AV.
- [SDR DALA2015120807450](https://openairdocs.org/sdr/DALA2015120807450.md): Access Panel · corroded · Dec 7, 2015 · N992DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION AT SETTLEMENT AND COUNTERSKIN AREAS OF FUEL ACCESS PANEL 1409C. FUEL ACCESS 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION II PARAGRAPH, B.
- [SDR DALA2015120707433](https://openairdocs.org/sdr/DALA2015120707433.md): Hinge · damaged · Dec 6, 2015 · N992DL · Doug MD88 · Fuselage, Door Hinge
  > ELONGATED HOLE ON FWD/AFT HINGE AT AFT CARGO COMPARTMENT DOOR. DAMAGED HOLE ON FWD HINGE WAS REPAIRED IAW ER/A 497387-14MA, REV B AND AFT HINGE WAS REPLACED FOR A NEW HINGE.
- [SDR DALA2015120707426](https://openairdocs.org/sdr/DALA2015120707426.md): Skin · worn · Dec 6, 2015 · N992DL · Doug MD88 · Fuselage Main, Plate/Skin
  > WORN PREVIOUS REPAIR FILLER ON FUSELAGE SKIN BETWEEN BS 1287-1309 AND LONGERONS 18R-19R. FILLER WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-04-2, FIG 2.
- [SDR DALA2015120707425](https://openairdocs.org/sdr/DALA2015120707425.md): Vane · worn · Dec 6, 2015 · N992DL · Doug MD88 · Trailing Edge Flaps
  > WORN PREVIOUS REPAIR DOUBLER ON INBD VANE, OTBD FLAP AT RT WING. REPAIR DOUBLER INBD VANE, OTBD FLAP AT RT WING WAS REPLACED IAW A/C 0992, CARD 2000-8149-05.
- [SDR DALA2015120707424](https://openairdocs.org/sdr/DALA2015120707424.md): Skin · cracked · Dec 6, 2015 · N992DL · Doug MD88 · Leading Edge Devices
  > CRACK ON RT WING SLAT PANEL NR 2 INNER SKIN BS XOS 240, CARD 04, ZONE 12. CRACK ON INNER SKIN WAS ATTENDED IAW SRM 57-01, FIG 3, SHT 2.
- [SDR DALA2015120707423](https://openairdocs.org/sdr/DALA2015120707423.md): Cargo Track · corroded · Dec 6, 2015 · N992DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO TRACK, AROUND FASTENERS FROM BS 1003 TO 1155. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, 51-10-4, 51-10-3 PARS 14 AND 21 AND 38.
- [SDR DALA2015120607421](https://openairdocs.org/sdr/DALA2015120607421.md): Floor Panel · cracked · Dec 5, 2015 · N992DL · Doug MD88 · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 1079A. FLOOR PANEL REPAIRED IAW SRM 51-70-1, PAR 10.
- [SDR DALA2015120607420](https://openairdocs.org/sdr/DALA2015120607420.md): Cusp Web · cracked · Dec 5, 2015 · N992DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT PREVIOUS REPAIR IN AFT CARGO RT SIDE BETWEEN BS 1136-1155. CUSP WEB REPAIR IAW SRM 51-30-2, 53-05, FIG 131A-1, 51-30-5.
- [SDR DALA2015120607422](https://openairdocs.org/sdr/DALA2015120607422.md): Floor Support · cracked · Dec 4, 2015 · N992DL · Doug MD88 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT UPPER SUPPORT ANGLE BETWEEN CABIN FLOORBEAMS 1271-1287 LBL 5. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01 51-30-2 AND 51-30-5.

Next page: https://openairdocs.org/deregistered/N992DL-2022-12-30/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 = 'N992DL' AND deregistration_id = 'N992DL-2022-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N992DL-2022-12-30/reports

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