# Service difficulty reports: N962DL, cancelled Dec 30, 2024

A list on [N962DL, cancelled Dec 30, 2024](https://openairdocs.org/deregistered/N962DL-2024-12-30.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 2 · 92 reports

- [SDR DALA2019101705945](https://openairdocs.org/sdr/DALA2019101705945.md): Battery Pack · inoperative · Oct 17, 2019 · N962DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOP IN F/C. R/R BATTERY PACK AT 4CD PER MD88 AMM 33-53. CK GOOD. (LP6604852)
- [SDR DALA2019101705946](https://openairdocs.org/sdr/DALA2019101705946.md): Smoke Detector · malfunctioned · Oct 16, 2019 · N962DL · Doug MD88 · Smoke Detection
  > SMOKE DETECTOR CHIRPING LOC 203. REMOVED & REPLACED 203 SMOKE DETECTOR OPS CHK GOOD. REF MD88 AMM 26-13. (LP1317887)
- [SDR DALA2019050802892](https://openairdocs.org/sdr/DALA2019050802892.md): Battery Pack · discharged · May 8, 2019 · N962DL · Doug MD88 · Emergency Lighting
  > DURING CK FOUND FIRST CLASS CEILING PANEL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IN PWR SUPPLY B5-100 IAW AMM 33-53. OPS CKS NML. (LP5800797)
- [SDR DALA2019042602656](https://openairdocs.org/sdr/DALA2019042602656.md): Frame · cracked · Apr 25, 2019 · N962DL · Doug MD88 · Fuselage Main, Frame
  > UPPER CANTED FRAME CRACKED AT 12 OCLOCK POSITION. REMOVED UPPER CTR FRAME ASSY. DRILLED UP REPLACEMENT FRAME PER MD88 DRAWING 5966768Y1. 301936. REINSTALLED UPPER CTR FRAME ASSY PER MD88 DRAWING 5966768Y1.
- [SDR DALA2019032501889](https://openairdocs.org/sdr/DALA2019032501889.md): Unknown · odor · Mar 24, 2019 · N962DL · Doug MD88 · Air Distribution System
  > DEPARTED AND SMELLED BAD ODOR DIVERTED TO MCI AFTER DELARING AN EMERGENCY NORMAL LANDING. OPENED BORESCOPE INSPECTION PORTS REF AMM 72-00-00-290-801C1. BORESCOPED 6TH STAGE 7TH STAGE 13TH STAGE ALSO INSPECTED INLET NO DAMAGE NOTED. CLOSED BORESCOPE INSPECTION
- [SDR DALA2018112906875](https://openairdocs.org/sdr/DALA2018112906875.md): Skin · corroded · Nov 20, 2018 · N962DL · Doug MD88 · Fuselage Main, Plate/Skin
  > MD-88 FUSELAGE STA 480 & L-30 CORROSION - REQUIRED PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION LEVEL OF ER/A 563889-14 IS REV. A. RESULTS OF DTA/DTE HAVE BEEN INCORPORATED AT THIS REVISION LEVEL. ACCOMPLISH SECTION II: PERMANENT REPAIR AT OR PRIOR TO THE
- [SDR DALA2018102506275](https://openairdocs.org/sdr/DALA2018102506275.md): Connector · not seated · Oct 25, 2018 · N962DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT AT 20 ED NOT ILLUMINATING. RESEATED CONNECTOR.
- [SDR DALA2018102506270](https://openairdocs.org/sdr/DALA2018102506270.md): Battery · discharged · Oct 25, 2018 · N962DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT IN AFT VENTRAL STARS OVERHEAD PANEL NOT ILLUMINATING. REPLACED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY B5-28 IAW AMM 33-53.
- [SDR DALA2018101706133](https://openairdocs.org/sdr/DALA2018101706133.md): Battery · discharged · Oct 17, 2018 · N962DL · Doug MD88 · Emergency Lighting
  > ROW 16-20 ABC OVERHEAD E-LIGHTS INOP. R+R BATTERIES IN B5-102. OPS CK SAT. PER AMM 33-50. (LP4414850)
- [SDR DALA2018081605105](https://openairdocs.org/sdr/DALA2018081605105.md): Slide · no test · Aug 16, 2018 · N962DL · Doug MD88 · Escape Slide
  > JETTISON TAIL CONE AND DEPLOY AFT SLIDE ROUTINE CARD 2562-7267 FAILED THE DEPLOYMENT TEST. CABLE IMPROPERLY ROUTED. ROUTED CABLE THE CORRECT WAY INSTALLED NEW SLIDE IAW AMDS ROUTINE CARD 2561-4001 AND LOG # 0697306 SCHEDULED PARTS CHANGE CARD JOB # 001-0001.(L
- [SDR DALA2018081004973](https://openairdocs.org/sdr/DALA2018081004973.md): Smoke Detector · malfunctioned · Aug 10, 2018 · N962DL · Doug MD88 · Smoke Detection
  > RT AFT LAVATORY SMOKE DETECTOR WAS BEEPING. REPLACED THE SMOKE DETECTOR IAW AMM 26-13. OPS CHECKED GOOD.
- [SDR DALA2018040202048](https://openairdocs.org/sdr/DALA2018040202048.md): Smoke Detector · dirty · Apr 2, 2018 · N962DL · Doug MD88 · Smoke Detection
  > AFT LEFT SIDE LAVATORY SMOKE DETECTOR ACTIVATED DURING CRUISE. A/C PACKS AT 12 & 1 O'CLOCK IN AUTO MODE. COOLED PACKS AND SMOKE DETECTOR STOPPED. FOUND SMOKE DETECTOR DIRTY AND WET. CLEANED AND DRIED THE AREA. ALL FUNCTIONAL CHECKED GOOD.
- [SDR DALA2018020200605](https://openairdocs.org/sdr/DALA2018020200605.md): Slide · abnormal · Feb 1, 2018 · N962DL · Doug MD88 · Escape Slide
  > LATE FINDING: UNFOLDING TAIL CONE SLIDE AT AFT ACCESORIES COMPARMENT. TAIL CONE SLIDE S/N:1586RP WAS REMOVED PER MD88 AMM 25-62-01 AND SERVICIABLE TAIL CONE SLIDE S/N:1082 WAS INSTALLED PER MD88 AMM 25-62-01.
- [SDR DALA2018013100518](https://openairdocs.org/sdr/DALA2018013100518.md): Door Frame · corroded · Jan 30, 2018 · N962DL · Doug MD88 · Fuselage Main, Structure
  > SEVERAL CORROSION POINTS AROUND FWD CARGO COMPARTMENT DOOR JAMB. CORROSION LEVEL 2 FWD CARGO COMPARTMENT DOOR JAMB WAS REPAIRED (PERMANENT REPAIR) PER ER/A 565444-14 REV ORIGINAL AND ETI-88-18-007 REV 1 REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL AIRFRAME FLIGH
- [SDR DALA2018013000499](https://openairdocs.org/sdr/DALA2018013000499.md): Skin · cracked · Jan 28, 2018 · N962DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > CRACKS ( 2 EA) ON DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER. DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER WAS REPAIRED (AS PERMANENT) PER ER/A 516509-14MA (SECTION I) REV 4 AND SRM 51-30-2 AND 51-30-5.
- [SDR DALA2018013000498](https://openairdocs.org/sdr/DALA2018013000498.md): Angle · cracked · Jan 28, 2018 · N962DL · Doug MD88 · Engine Cowling System
  > CRACK IN ELBOW DUCT ANGLE AT RT NOSE COWLING YN= 19.430 AND 12 O'CLOCK POSITION, ALSO MISALIGNED MIXING TUBE AT RT NOSE COWLING 12 O'CLOCK POSITION. ELBOW DUCT ANGLE (P/N: 5938038-41) AT RT NOSE COWLING YN= 19.430 WAS REPLACED PER SRM 51-30-2, 51-30-5 AND DWG
- [SDR DALA2018012900466](https://openairdocs.org/sdr/DALA2018012900466.md): Frame · cracked · Jan 27, 2018 · N962DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME ON STA Y=1510 CANT 5HRS POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME ON STA Y=1510 CANT 5 HRS. POSITION AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER DWG 9911843 REV "AC" AND SRM 51-30-2 AND 51-30-5.
- [SDR DALA2018012900465](https://openairdocs.org/sdr/DALA2018012900465.md): Frame · cracked · Jan 26, 2018 · N962DL · Doug MD88 · Fuselage Main, Frame
  > OUT OF LIMITS: EXCESSIVE CORROSION ON FRAME STA=1287 BTW LONG 28R AND 28L AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER SRM 53-03D FIG 2A.
- [SDR DALA2018012900464](https://openairdocs.org/sdr/DALA2018012900464.md): Longeron · cracked · Jan 26, 2018 · N962DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK IN LONGERON 4L STA 200 AT PAX CABIN. DAMAGE LONGERON 4L STA 200 AT PAX CABIN WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-02 FIG 18.
- [SDR DALA2018012900463](https://openairdocs.org/sdr/DALA2018012900463.md): Skin · corroded · Jan 26, 2018 · N962DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORRO
- [SDR DALA2018012900462](https://openairdocs.org/sdr/DALA2018012900462.md): Skin · corroded · Jan 26, 2018 · N962DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORRO
- [SDR DALA2018012900460](https://openairdocs.org/sdr/DALA2018012900460.md): Fitting · corroded · Jan 26, 2018 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > OUT OF LIMITS: CORROSION ON FRAME CLIP STA Y=1231 BTW LONG 29R TO 30 AT AFT CARGO COMPARTMENT. FRAME CLIP (EXTRUSION P/N: S2506195-12000) STA Y=1231 BTW LONG 29R TO 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 53-14-3 FIG 3, 51-30-5 AND SRM 51-30-2.
- [SDR DALA2018012900457](https://openairdocs.org/sdr/DALA2018012900457.md): Skin · corroded · Jan 25, 2018 · N962DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > CORROSION ON RT APU ACCESS DOOR INTERNAL AND EXTERNAL SKIN. THE APU DOOR THAT WAS REMOVED WITH THE PART NUMBER 5914694-95 AND SERIAL NUMBER: DL14 AND THE SERVICEABLE DOOR WITH THE PART NUMBER 5914694-501 AND SERIAL NUMBER DL9 WAS REPLACED PER CMM 52-44-1 CORRO
- [SDR DALA2018012400401](https://openairdocs.org/sdr/DALA2018012400401.md): Lanyard · damaged · Jan 23, 2018 · N962DL · Doug MD88 · Emergency Equipment
  > INITIAL INSPECTION: DAMAGE LANYARD OF FWD PASSENGER ENTRANCE DOOR L1 SLIDE. L1 RELEASE LANYARD CABLE WAS REPLACED AND VERIFIED PER IPC 25-60-00-34.
- [SDR DALA2017120408409](https://openairdocs.org/sdr/DALA2017120408409.md): Skin · cracked · Dec 3, 2017 · N962DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ON WALKAROUND FOUND CORROSION WITH CRACK ON OUTER SKIN ON LOWER UHF ANTENNA. CUT OUT DAMAGE OND REMOVED INTERNAL PARTS FOR ACCESS. C/W ER/A 563889-14 REV 0 ON NRC4 SCEPTOR LOG 0323707. (LP3884696)
- [SDR DALA2017120408414](https://openairdocs.org/sdr/DALA2017120408414.md): Not Reported · corroded · Dec 3, 2017 · N962DL · Doug MD88 · Fuselage Main, Structure
  > C/W PRI 563889-14 REV ORIGINAL. CORROSION FUSELAGE STATION 480 AND LONGERON L-30. C/W PRI 563889-14 REV 1. C/W 563889-14 REV 0. (LP0323707)
- [SDR DALA2017111708214](https://openairdocs.org/sdr/DALA2017111708214.md): Battery Pack · inoperative · Nov 17, 2017 · N962DL · Doug MD88 · Emergency Lighting
  > COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017102307713](https://openairdocs.org/sdr/DALA2017102307713.md): Battery Pack · inoperative · Oct 23, 2017 · N962DL · Doug MD88 · Emergency Lighting
  > OVERHEAD TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERIES, OPS CHECKED LIGHTS AND BATTERY CHARGER IAW AMM 33-50.
- [SDR DALA2017072405645](https://openairdocs.org/sdr/DALA2017072405645.md): Tire · failed · Jul 21, 2017 · N962DL · Doug MD88 · Tire
  > NR 1 MAIN TIRE, LEFT TIRE MAIN CORD SHREDDED. TIRE DAMAGED AFTER USING MAX AUTO BRAKE AND THEN ACFT CAME TO ABRUPT STOP. SMOKE FROM TIRE WAS NOTED BY TOWER. REPLACED THE NR 1 MAIN WHEEL ASSY IAW AMM 32-40. INSPECTED UNDERSIDE OF LT WING NO DAMAGE NOTED. BI
- [SDR DALA2017070705270](https://openairdocs.org/sdr/DALA2017070705270.md): Light · inoperative · Jul 7, 2017 · N962DL · Doug MD88 · Emergency Lighting
  > SEAT 29 MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-53. OPS CHECKED OK.
- [SDR DALA2017030501770](https://openairdocs.org/sdr/DALA2017030501770.md): Angle · cracked · Mar 4, 2017 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > LEFT LOUVER PANEL FOUND A CRACKED ANGLE, BS 1463. REPLACED THE ANGLE IAW DWG 9911839.
- [SDR DALA2017030501769](https://openairdocs.org/sdr/DALA2017030501769.md): Support · cracked · Mar 4, 2017 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > BS 1463 FOUND BRIDGE SUPPORT ROD BRACKET CRACKED. REMOVED BRIDGE SUPPORT. FABRICATED AND REPLACED IAW DWG 5930556.
- [SDR DALA2016111008444](https://openairdocs.org/sdr/DALA2016111008444.md): Connector · damaged · Nov 10, 2016 · N962DL · Doug MD88 · Engine Oil System Wiring
  > RIGHT ENGINE OIL TEMPERATURE ERRATIC AND HIGH. FOLLOWED QRH PROCEDURES AND SHUT ENGINE DOWN. POSITIVE OIL PRESSURE WAS MAINTAINED DURING WINDMILLING TIME. MAINTENANCE FOUND CONNECTOR P1-812 WITH A PUSHED BACK PIN. REPLACED AND RE PINNED THE CONNECTOR. ALSO RE
- [SDR DALA2016070705207](https://openairdocs.org/sdr/DALA2016070705207.md): Coffeemaker · malfunctioned · Jul 6, 2016 · N962DL · Doug MD88 · Buffet/Galleys
  > COFFEEMAKER, F303, NR 1 TURNED ON. IN FLT, SMELLED ELECTRICAL BURNING. SECURED, ODOR DISSIPATED IMMEDIATELY. DEFERRED IAW NEF 253602. COFFEEMAKER REPLACED ON 08JUL16.
- [SDR DALA2016021201002](https://openairdocs.org/sdr/DALA2016021201002.md): Door Sill · corroded · Feb 11, 2016 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > LOWER CARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AND EDGE SEAL DETERIORATED. REPAIRED IAW PRI 543287-14 ALL REVISIONS AND COMPLIED WITH ERA 543287-14, REV ORIGINAL.
- [SDR DALA2015121807665](https://openairdocs.org/sdr/DALA2015121807665.md): Heater · failed · Dec 17, 2015 · N962DL · Doug MD88 · Heating System
  > ACFT HAD SLIGHT ODOR, HAZE IN CABIN AND COCKPIT. FLIGHT CREW NOTED 1 PHASE OF CARGO HEAT C/B POPPED. PULLED REMAINING C/BS AND ALL DISSIPATED. MAINTENANCE FOUND THE FORWARD CARGO HEAT INTERNAL ELEMENT FAILED AND REPLACED THE FORWARD CARGO HEATER. MAINTENAN
- [SDR DALA2015112007083](https://openairdocs.org/sdr/DALA2015112007083.md): Spar Cap · cracked · Nov 19, 2015 · N962DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > ER/A 519139-14, REV A,VERTICAL STABILIZER REAR SPAR CAP, CRACK REPAIRED IAW ER/A 519139-14, REV A.
- [SDR DALA2015091405621](https://openairdocs.org/sdr/DALA2015091405621.md): Battery Pack · inoperative · Sep 11, 2015 · N962DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK, MAINTENANCE FOUND FOUND EMERGENCY LIGHTS IN CEILING FORWARD OF AFT CABIN DOOR INOPERATIVE. BATTERIES AT B5-27 AND B5-28 WERE REPLACED.
- [SDR DALA2015030901992](https://openairdocs.org/sdr/DALA2015030901992.md): Power Supply · inoperative · Mar 5, 2015 · N962DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND 3 CEILING EMERGENCY LIGHTS INOPERATIVE IN THE FWD CABIN AREA. MSP MAINTENANCE R & R THE EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-00. OPS CHECKED NORMAL. LP6972433.
- [SDR DALA2015022401621](https://openairdocs.org/sdr/DALA2015022401621.md): Wire · damaged · Feb 24, 2015 · N962DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE FLOOR MOUNTED EMERGENCY PATHWAY LIGHTING FOR ROWS 1-12 AND THE OVERHEAD LIGHTS AT DOORS L1 & R1 WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT ROW 11E WAS SHORTING TO GROUND. WIRE WAS REPAIRED WITH A SPLICE
- [SDR DALA2016110808569](https://openairdocs.org/sdr/DALA2016110808569.md): Cusp Web · corroded · Mar 5, 2014 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB X=-54 TO X=-60 BETWEEN STA Y=793 TO STA Y=800, FLOOR CABIN STRUCTURE. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, TRIMMED, DRILLED, TREATED, PAINTED, AND INSTALLED.
- [SDR DALA13071080962](https://openairdocs.org/sdr/DALA13071080962.md): Cam · misinstalled · Dec 22, 2013 · N962DL · Doug MD88 · Aerodynamic Fairings
  > DURING ZONE FINAL CHECK, NOTED MISINSTALLED RELEASE MECHANISM CAM OF TAILCONE. INSTALLED RELEASE MECHANISM CAM CORRECTLY IAW AMM 53-53-02-201.
- [SDR DALA13071090962](https://openairdocs.org/sdr/DALA13071090962.md): Access Panel · corroded · Dec 21, 2013 · N962DL · Doug MD88 · Wing, Plate/Skin
  > DURING CHECK, CORROSION FOUND ON RT WING HEATER BLANKET AROUND FUEL ACCESS PANEL. REPLACED ACCESS PANEL IAW AMM 30-80-02.
- [SDR DALA13071070962](https://openairdocs.org/sdr/DALA13071070962.md): Access Panel · corroded · Dec 21, 2013 · N962DL · Doug MD88 · Wing, Plate/Skin
  > DURING CHECK, CORROSION FOUND ON LT WING HEATER BLANKET AROUND FUEL ACCESS PANEL. REPAIRED IAW ER/A 519147-14.
- [SDR DALA13071060962](https://openairdocs.org/sdr/DALA13071060962.md): Spar Cap · cracked · Dec 21, 2013 · N962DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > DURING CHECK, A CRACK FOUND ON RT HORIZONTAL STABILIZER REAR SPAR CAP APPROXIMATELY STA XE 14.525. SPAR CAP REPLACED IAW DWG SR09550030, REV "C" CONFIG. 7006.
- [SDR DALA13070260962](https://openairdocs.org/sdr/DALA13070260962.md): Frame · corroded · Dec 17, 2013 · N962DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME BS 1380 L25LT & RT AT AFT ACCESSORY COMPARTMENT. LOWER FRAME TEE AT BS 1380 WAS REPLACED IAW ER/A 521172-14 REV ORIGINAL AND DWG 9912246, REV DE & SRM 51-30-2 AND 51-30-5 AND ER/A N.- 521175-14, REV ORIG ORIGINAL.
- [SDR DALA13069760962](https://openairdocs.org/sdr/DALA13069760962.md): Web · damaged · Dec 15, 2013 · N962DL · Doug MD88 · Horizontal Stabilizer Structure
  > ELONGATED HOLES ON WEB, ANGLES AND FITTING BETWEEN XH=27 AND XHS=97 ALSO ON PRODUCTION DOUBLER BETWEEN XH=27 AND XHS=41 AT RT HORIZONTAL STABILIZER REAR SPAR. DAMAGED WEB, ANGLES AND FITTING AND DOUBLER REMOVED IAW SRM 51-30-1, 51-30-2 AND 51-30-5, FABRICATE
- [SDR DALA13069750962](https://openairdocs.org/sdr/DALA13069750962.md): Skin · cracked · Dec 13, 2013 · N962DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3&4R. DAMAGE REMOVED, REPAIR FABRICATED, TREATED, PAINTED AND REPAIR INSTALLED IAW SRM 51-30-2, 53-04 FIG. 27, 51-10-3.
- [SDR DALA13068940962](https://openairdocs.org/sdr/DALA13068940962.md): Skin · damaged · Dec 12, 2013 · N962DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE AT LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 522 - 541. BLENDED IAW SRM 53-05, FIG III,
- [SDR DALA13067050962](https://openairdocs.org/sdr/DALA13067050962.md): Intercostal · corroded · Dec 6, 2013 · N962DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON INTERCOSTAL BELOW DOOR FRAME WEB, BS 1183 AND 1193 AT AFT CARGO BAY. INTERCOSTALS REMOVED IAW SRM 51-30-2-51-30-5. NEW INTERCOSTALS INSTALLED IAW SRM 51-30-2 - 51-30-5.

Next page: https://openairdocs.org/deregistered/N962DL-2024-12-30/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 = 'N962DL' AND deregistration_id = 'N962DL-2024-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N962DL-2024-12-30/reports

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