# Service difficulty reports: N990DL

A list on [N990DL](https://openairdocs.org/aircraft/N990DL.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 · 238 reports

- [SDR DALA2020012600597](https://openairdocs.org/sdr/DALA2020012600597.md): Angle · cracked · Jan 25, 2020 · N990DL · Doug MD88 · Engine Cowling System
  > 2EA CLIPS ARE CRACKED INSIDE #2 ENG NOSE COWL. REPLACED THE #2 NOSE COWL PER MD88 AMM 71-10-01 OFF PT # 5930645-509 S# DL 56 ON PT #5930654-509 S# 49416 FTN 91VRMK. (LP1461577)
- [SDR DALA2020012000393](https://openairdocs.org/sdr/DALA2020012000393.md): Power Supply · inoperative · Jan 19, 2020 · N990DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK FOUND EMERGENCY LIGHTS INOP @ ROW 31 AFT INTO AFT ACCESSORY COMPARTMENT. R/R POWER SUPPLY AND BATTERY PACK B5-212 MULTIPLE TIMES PER MD88 AMM 33-53. LIGHTS WORKED INITIALLY BUT AFTER 5 MINUTES STOPPED WORKING AGAIN (354789) FOUND L2-873 SH
- [SDR DALA2019111806738](https://openairdocs.org/sdr/DALA2019111806738.md): Bracket · cracked · Nov 18, 2019 · N990DL · Doug MD88 · Fuselage Main, Attach Fittings
  > RT WHEEL WELL FAIRING BRACKET CRACKED JUST LOWER OF PROXIMITY SENSOR. REPLACED RT WHEEL WELL FWD DOOR JAMB PER BAC DWG5930584. (LP5962266)
- [SDR DALA2019102806190](https://openairdocs.org/sdr/DALA2019102806190.md): Battery Pack · inoperative · Oct 28, 2019 · N990DL · Doug MD88 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHTS NOT ILLUMINATED WHEN TESTED ON SVC CHECK. REPLACED EMER LIGHT BATTERIES AND FUSE PER MD88 AMM 33-53. FOUND NORMAL OPERATION WHEN TESTED. (LP5587087)
- [SDR DALA2019090105109](https://openairdocs.org/sdr/DALA2019090105109.md): Fuse · blown · Aug 31, 2019 · N990DL · Doug MD88 · Emergency Lighting
  > SEAT 31DEF THROUGH 36DEF SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED FUSE 1 IN BATTERY PACK B5-212 REF AMM 33-53 CHECKS GOOD. (LP6018365)
- [SDR DALA2019072904447](https://openairdocs.org/sdr/DALA2019072904447.md): Smoke Detector · faulty · Jul 26, 2019 · N990DL · Doug MD88 · Smoke Detection
  > LT AFT LAVATORY SMOKE DETECTOR CHIRPING. R/R SMOKE DETECTOR PER AMM 26-13. (LP1191067)
- [SDR DALA2019061203521](https://openairdocs.org/sdr/DALA2019061203521.md): Connector · disconnected · Jun 7, 2019 · N990DL · Doug MD88 · Light System Wiring
  > FOUND DOOR L1 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED L1 DOOR EMERGENCY LIGHT PER MD88 AMM 33-53. NO FIX. FOUND LIGHT ASSEMBLY DISCONNECTED BEHIND CEILING AND RECONNECTED IT. LIGHT OPERATIONAL CHECK IS OK PER MD88 AMM 33-53. (LP #5453557)
- [SDR DALA2019053103332](https://openairdocs.org/sdr/DALA2019053103332.md): Wire · burned · May 31, 2019 · N990DL · Doug MD88 · Light System Wiring
  > UPON ARRIVAL TO RAMP IN ATL AND APU SPOOL UP SMELLED ELEC BURNING, A/C CROSSTIE LOCKOUT, RIGHT GEN FELL OFF LINE, APU GEN PICKED UP LOAD, SPARK WAS SEEN IN FIRST CLASS SEAT 1 C/D OVERHEAD. RAN SMOKE/FIRE/FUME CHECKLIST. CABIN STAND BY LGTS C/B, (L) COND REG VA
- [SDR DALA2019053003316](https://openairdocs.org/sdr/DALA2019053003316.md): Wire · damaged · May 29, 2019 · N990DL · Doug MD88 · Oxygen System Wiring
  > REF WDM 35-24-01 WIRE W638CL20 HAS HEAT DAMAGE IN F/C CABIN OVER HEAD AREA. REMOVED AND REPLACED WIRE #W638CL20 FROM CONNECTOR R5-1200 PIN FF TO BUTT SPICE REPAIR ABOVE CEILING PANEL ROW 2CD PER SPWD 20-31. WIRING CKS IAW WDM 35-24-01. PERFORMED PAX O2 SYSTEM
- [SDR DALA2019053003315](https://openairdocs.org/sdr/DALA2019053003315.md): Wire · burned · May 29, 2019 · N990DL · Doug MD88 · Flight Control System Wiring
  > REF WDM 30-31-03 PG 2 WIRE F1551B20 FOUND BURNT THROUGH IN OVERHEAD F/C CABIN. RAN AND SPLICED WIRE F1551B20 IAW SWPM 20-10. TERMINATED AT R5-1201 IAW SWPM 20-31. 903393. WIRING CKS C/W IAW WDM 30-31-03. 399270. OPS CHECK PRIM STAM TRIM MOTOR HEATER PER AMM 27
- [SDR DALA2019050502814](https://openairdocs.org/sdr/DALA2019050502814.md): Lens · missing · May 3, 2019 · N990DL · Doug MD88 · Exterior Lighting
  > DURING WALKAROUND FOUND LEFT AFT POS LIGHT COVER MISSING. RPLCD LENS. (LP5564700)
- [SDR DALA2019042982688](https://openairdocs.org/sdr/DALA2019042982688.md): Brake · malfunctioned · Apr 27, 2019 · N990DL · Doug MD88 · Landing Gear Brake System
  > FELT LIKE (R) BRAKE CAUGHT DURING T/O ROLL GSP. NOSE CAME RIGHT AND SOON AFTER BRAKE OVERTEMP LIGHT FLASHED ON + OFF. INSPECTED #3 BRAKE,NO TROUBLE FOUND, OK FOR SVC. (LP5799880)
- [SDR DALA2019040402156](https://openairdocs.org/sdr/DALA2019040402156.md): Battery Pack · inoperative · Apr 4, 2019 · N990DL · Doug MD88 · Emergency Lighting
  > FOUND FLIGHT DECK AND CABIN EMERGENCY LIGHTS B523/P5 INOP. RELAMPED NO HELP. CHECKED AND FOUND ONE BATTERY WITH ZERO VOLTS. REPLACED BATTERY SET, CKS NML REF MD88 AMM 33-53. (LP5767472)
- [SDR DALA2019021500962](https://openairdocs.org/sdr/DALA2019021500962.md): Cooler · leaking · Feb 14, 2019 · N990DL · Doug MD88 · Engine Fuel/Oil Cooler
  > DURING PAX BOARDING APU STARTED AND A/C PACKS TURNED ON. AFTER APPROX. 5 MINUTES WE SMELLED JET EXHAUST/ JET A FUMES IN CABIN. SHUT DOWN APU AND SMELL/ FUMES DISSIPATED WITH GROUND AIR CONNECTED. FOUND FUEL LEAK AT NO 1 ENG. FUEL/OIL COOLER AFT SIDE. R/R O-RI
- [SDR DALA2018111206596](https://openairdocs.org/sdr/DALA2018111206596.md): Fuse · blown · Nov 11, 2018 · N990DL · Doug MD88 · Emergency Lighting
  > SEAT EMERGENCY LIGHTS ROW 1-12 AND L1 L2 DOOR EXIT SIGNS INOP. T/S PER WDM 33-51-14. FOUND FUSES BLOWN ON B5-211 BATTERY PACK ASSEMBLY. CHANGED FUSES AND OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR DALA2018100805915](https://openairdocs.org/sdr/DALA2018100805915.md): Schrader Valve · leaking · Oct 6, 2018 · N990DL · Doug MD88 · Nose/Tail Landing Gear Strut/Axle
  > A/C RETURNED BACK TO SAV FOR NOSE GEAR UNABLE TO RETRACT. PILOTS FOLLOWED QRH PROCEDURES. FOUND SHRADER VALVE LEAKING, REPLACED SAME PER M/M 32-20. SERVICED NOSE STRUT PER W/C 3221-644 OK FOR SERVICE. REPORTED DUE TO DECLARED EMERGENCY. (LP4188484)
- [SDR DALA2018061203951](https://openairdocs.org/sdr/DALA2018061203951.md): Panel · cracked · Jun 8, 2018 · N990DL · Doug MD88 · Wing, Plate/Skin
  > PERFORM GVI OF RT WING UPPER SURFACE. DUE TO PASSENGER REPORT OF A CRACK ON THE RT WING UPPER SURFACE AS OBSERVED FROM THE CABIN, PLEASE SET- UP TO PERFORM A GVI OF THE RT WING UPPER SURFACE FOR ANY SIGNS OF A CRACK. WHILE WORKING MD LOG 0592224 FOR POSSIBLE
- [SDR DALA2018020500634](https://openairdocs.org/sdr/DALA2018020500634.md): Door · cracked · Feb 2, 2018 · N990DL · Doug MD88 · Landing Gear Doors
  > CRACK ON LWR INNER SIDE AT RT STRUT DOOR. RIGHT MAIN DOOR OUTBOARD P/N 5936791-504 S/N:UNK WAS REMOVED AND SERVICEABLE RIGHT DOOR OUTBOARD P/N 5936791-504 S/N DL105 WAS INSTALLED PER AMM 32-12-01-201.
- [SDR DALA2018013000497](https://openairdocs.org/sdr/DALA2018013000497.md): Intercostal · cracked · Jan 27, 2018 · N990DL · Doug MD88 · Landing Gear Doors
  > CRACK INTERCOSTAL ON STA Y= 958 RT MLG DOOR. INTERCOSTAL ON STA Y= 958 RT MLG DOOR WAS REPLACED PER SRM 51-30-2, 51-30-5 AND DWG:5930583 REV DA.
- [SDR DALA2018012900459](https://openairdocs.org/sdr/DALA2018012900459.md): Doubler · cracked · Jan 26, 2018 · N990DL · Doug MD88 · Horizontal Stabilizer Structure
  > INITIAL INSPECTION: CRACK PRODUCTION DOUBLER LT SIDE ON STABILIZER JACKSCREW. PRODUCTION DOUBLER LT SIDE ON STABILIZER JACKSCREW WAS REPLACED PER SRM 51-30-5AND DWG 9911808 REV U.
- [SDR DALA2017100207234](https://openairdocs.org/sdr/DALA2017100207234.md): Battery Pack · inoperative · Oct 1, 2017 · N990DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 17 AND 29. REPLACED THE BATTERY PACKS AT ROW 17 AND 29, OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017092507062](https://openairdocs.org/sdr/DALA2017092507062.md): Battery Pack · discharged · Sep 23, 2017 · N990DL · Doug MD88 · Emergency Lighting
  > THREE EMERGENCY LIGHTS INOPERATIVE. FOUND THE BATTERY DISCHARGED IN AFT RT LAVATORY. REPLACED THE BATTERIES IAW MM 33-53. EMERGENCY LIGHTS CHECKED OK.
- [SDR DALA2017022701585](https://openairdocs.org/sdr/DALA2017022701585.md): Rheostat · failed · Feb 19, 2017 · N990DL · Doug MD88 · Flight Compartment Lighting
  > CAPTAIN`S YOKE, CHART LIGHT SPARKED AND ARCED. REPLACED RHEOSTAT ON THE CHART HOLDER.
- [SDR DALA2016052404136](https://openairdocs.org/sdr/DALA2016052404136.md): Slide · inoperative · May 24, 2016 · N990DL · Doug MD88 · Escape Slide
  > MAIN CABIN DOOR WAS OPENED WITHOUT SLIDE BEING DISARMED. SLIDE DID NOT DEPLOY, BUT IS OUT OF THE DOOR. RE-INSTALLED 1L SLIDE IAW AMM 25-62. CHECK NORMAL. NO FURTHER DISCREPANCIES NOTED. AC OK FOR SERVICE.
- [SDR DALA2016021100980](https://openairdocs.org/sdr/DALA2016021100980.md): Handle · misinstalled · Feb 10, 2016 · N990DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE FOUND THE TAILCONE EXTERNAL RELEASE HANDLE IMPROPERLY INSTALLED. CABLE WAS REINSTALLED PROPERLY IAW AMM 53-53-00-501.
- [SDR DALA2016020800917](https://openairdocs.org/sdr/DALA2016020800917.md): Former · cracked · Feb 7, 2016 · N990DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER LEADING EDGE INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW DC9/MD80 SRM 55-02D, FIG 27, PERFORM INSPECT FOR CRACKS ON L/E SKIN EVERY C-CHECK IAW SRM 55-02D, FIG 27 PAG 113
- [SDR DALA2016020800929](https://openairdocs.org/sdr/DALA2016020800929.md): Hinge · damaged · Feb 6, 2016 · N990DL · Doug MD88 · Fuselage, Door Hinge
  > ELONGED HOLES AT FWD AND AFT HINGES OF MID CARGO DOOR. HOLES OF HINGES WERE REPAIRED IAW ER/A 497387-14 MA, REV B, HOLE HINGE AFT ID 0.798" AND HOLE HINGE FWD ID 0.799.
- [SDR DALA2016020600914](https://openairdocs.org/sdr/DALA2016020600914.md): Frame · corroded · Feb 5, 2016 · N990DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME CHANNEL IN BS 1307 BETWEEN LONGERON 27RT-LONGERON 27LT AT AFT CARGO COMPARTMENT. REPAIR WAS REPLACED IAW SRM 53-03D, FIG 2A.
- [SDR DALA2016020600913](https://openairdocs.org/sdr/DALA2016020600913.md): Angle · cracked · Feb 5, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE ON BS 991 AND X=7 AT LT MLG WHEEL WELL. ANGLE WAS REPAIRED IAW ER/A413026-14 MA, REV ORIGINAL SRM 51-10-3, PAR 14, 21 AND 51-30-5.
- [SDR DALA2016020600912](https://openairdocs.org/sdr/DALA2016020600912.md): Vane · worn · Feb 5, 2016 · N990DL · Doug MD88 · Trailing Edge Flaps
  > WEAR ON RT WING, OTBD FLAP, OTBD VANE AT INBD AFT LWR EDGE. RT WING OTBD FLAP, OTBD VANE AT INBD AT LWR EDGE WAS REPAIRED IAW SRM 57-03, PAR 11, CARD 2000-8149-12 JOB 000-0052 AND ER/A 521199-14 MA, REV ORIGINAL.
- [SDR DALA2016020600911](https://openairdocs.org/sdr/DALA2016020600911.md): Cargo Track · corroded · Feb 4, 2016 · N990DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT CARGO TRACK BETWEEN BS 1220-1322 UPPER AND LOWER SURFACES AT AFT CARGO COMPARTMENT. LT CARGO TRACK WAS REPLACED IAW 51-30-1, 51-30-2, 51-10-4, 51-10-3 PAR 21 AND 14.
- [SDR DALA2016020500897](https://openairdocs.org/sdr/DALA2016020500897.md): Doubler · not reported · Feb 4, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING NDT INSPECTION, A DISCREPANT DOUBLER WAS FOUND ON UPPER FWD CORNER, FS 370 TO 381, IAW SRM 53-05, FIG 68. THESE NRC IS ATTENDED WITH ER/A NO 541596-14AD, REV ORIGINAL.
- [SDR DALA2016020500895](https://openairdocs.org/sdr/DALA2016020500895.md): Skin · cracked · Feb 4, 2016 · N990DL · Doug MD88 · Rudder, Plate/Skin
  > CRACK ON RUDDER RT SKIN UPPER EDGE. RUDDER RT SKIN UPPER EDGE WAS REPAIRED IAW ER/A 541617-14, REV ORIGINAL AND CARD 2000-8149-06, JOB 000-0018.
- [SDR DALA2016020500893](https://openairdocs.org/sdr/DALA2016020500893.md): Doubler · worn · Feb 4, 2016 · N990DL · Doug MD88 · Trailing Edge Flaps
  > WEAR ON DOUBLER LT WING OTBD FLAP INBD VANE BETWEEN BS XV1:159.5 AND XV1: 166 UPPER SKIN. LT WING OTBD FLAP INBD VANE BETWEEN BS XV1: 159.5 AND XV1: 166 UPPER SKIN WAS REPAIRED IAW SRM 57-03D, PAR. 11.
- [SDR DALA2016020500885](https://openairdocs.org/sdr/DALA2016020500885.md): Intercostal · bent · Feb 4, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous Structure
  > BENT INTERCOSTAL JUST ABOVE LONGERON 29 LT BS 1231 TO 1227 AT AFT CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21, 51-10-2 AND 53-01, FIG 2.
- [SDR DALA2016020500884](https://openairdocs.org/sdr/DALA2016020500884.md): Structure · cracked · Feb 4, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK RADIO RACK EXHAUST. RADIO RACK EXHAUST WAS REPAIRED IAW ER/A 464964-14 MA REV C.
- [SDR DALA2016020500881](https://openairdocs.org/sdr/DALA2016020500881.md): Skin · delaminated · Feb 4, 2016 · N990DL · Doug MD88 · Trailing Edge Flaps
  > DELAMINATION ON UPPER SKIN OF LT INBD FLAP OTBD GUIDE VANE. DELAMINATION ON UPPER SKIN OF LT INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW 57-03 PARR 11.
- [SDR DALA2016020500880](https://openairdocs.org/sdr/DALA2016020500880.md): Pan · cracked · Feb 4, 2016 · N990DL · Doug MD88 · Cargo/Baggage Doors
  > CRACK FWD EDGE PAN WITH BEAM 1 OF MID CARGO DOOR. ACCOMPLISHED AROUND STOP DRILLS NO MORE CRACKS WERE FOUND IAW SRM 51-01, PAR 21, B, NEW DOUBLER WAS FABRICATED, PAINTED AND INSTALLED IAW ETI 88-16-041 AND 51-10-3, PAR 14 AND ER/A 543134-14 REV ORIGINAL.
- [SDR DALA2016020500879](https://openairdocs.org/sdr/DALA2016020500879.md): Skin · damaged · Feb 4, 2016 · N990DL · Doug MD88 · Rudder, Plate/Skin
  > DAMAGE METALLIZER ON RUDDER BOTH SIDE. METALIZER ON RUDDER BOTH SIDE WAS REPAIRED IAW SRM 51-70-1A PAR 23 AND CARD 2000-8149-01, JOB 000-0004.
- [SDR DALA2016020500878](https://openairdocs.org/sdr/DALA2016020500878.md): Frame · cracked · Feb 4, 2016 · N990DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON FRAME 1510 CANT APPROXIMATELY 2 O`CLOCK POSITION. FRAME WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3.
- [SDR DALA2016020500887](https://openairdocs.org/sdr/DALA2016020500887.md): Cargo Track · corroded · Feb 3, 2016 · N990DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT TIE TRACK BETWEEN BS Y=1007-1220, UPPER AND LOWER SURFACES, AT AFT CARGO COMPARTMENT. DUE TO EXCCESIVE CORROSION TIE TRACK LT BS Y=1007-1220 AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-30-1 AND 51-10-4.
- [SDR DALA2016020400841](https://openairdocs.org/sdr/DALA2016020400841.md): Cargo Track · corroded · Feb 3, 2016 · N990DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT CARGO TRACK BETWEEN BS 1007-1155, UPPER AND LOWER SURFACES, IN AFT CARGO BAY. DUE TO EXCESIVE CORROSION THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1.
- [SDR DALA2016020400840](https://openairdocs.org/sdr/DALA2016020400840.md): Longeron · cracked · Feb 3, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 7R WITH FRAME, BS 1380. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. LONGERON WAS TREATED AND PAINTED IAW, SRM 51-10-3, PAR 21, 14.
- [SDR DALA2016020400839](https://openairdocs.org/sdr/DALA2016020400839.md): Door Frame · cracked · Feb 3, 2016 · N990DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON NLG DOOR FRAME BS 45 RBL 17 AT NOSE WHEELWELL. DOOR FRAME WAS REPAIRED IAW SRM 51-30-2, 51-30-3, 51-30-5, PAR 14 AND 21. 51-10-2, 51-10-4 AND 53-05, FIG 110.
- [SDR DALA2016020400846](https://openairdocs.org/sdr/DALA2016020400846.md): Floor Panel · damaged · Feb 2, 2016 · N990DL · Doug MD88 · Fuselage Floor Panel
  > CRACK AND CORROSION ON FLOOR PANEL COVER LT COCKPIT. REPAIR FABRICATED AND INSTALLED IAW SRM 53-01, FIG 4, SH 4.
- [SDR DALA2016020300829](https://openairdocs.org/sdr/DALA2016020300829.md): Skin · damaged · Feb 2, 2016 · N990DL · Doug MD88 · Wing, Plate/Skin
  > ELONGATED SEVERAL ATTACHING HOLES ON LT WING TIP T/E UPPER SKIN SURFACE. LEFT WING TIP UPPER SKIN SURFACE WAS REPAIRED IAW EA 09-478904-14MA, REV ORIGINAL.
- [SDR DALA2016020300828](https://openairdocs.org/sdr/DALA2016020300828.md): Skin · damaged · Feb 2, 2016 · N990DL · Doug MD88 · Wing, Plate/Skin
  > ELONGATED SEVERAL ATTACHING HOLES ON LT WING TIP LOWER SKIN SURFACE. LT WING TIP LOWER SKIN SURFACE WAS REPAIRED IAW EA 09-478904-14.
- [SDR DALA2016020300826](https://openairdocs.org/sdr/DALA2016020300826.md): Angle · cracked · Feb 2, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK FRAME CLIP BETWEEN LONG 2L TO 4L AT FRAME BS 1437. FRAME CLIP WAS R & R IAW 51-30-5, 53-14-4, 51-10-3 PAR 14, 21.
- [SDR DALA2016020300821](https://openairdocs.org/sdr/DALA2016020300821.md): Skin · corroded · Jan 31, 2016 · N990DL · Doug MD88 · Elevator, Plate/Skin
  > CORROSION ON AFT BARREL NUT HOLE 1 AND 2 AT LT SIDE UPPER PANEL REAR SPAR BS XH 26.625. AT LT SIDE WAS PERFORMED IAW ERA 541607-14, REV: A.
- [SDR DALA2016020100779](https://openairdocs.org/sdr/DALA2016020100779.md): Pan · cracked · Jan 31, 2016 · N990DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED FWD EDGE PAN WITH BEAM 5 OF MID CARGO DOOR. CRACKS WERE FOUND STOPPED IAW SRM 51-01, 21, A AND STEPS 1, 2 HFEC INSPECTION WAS ACCOMPLISHED AROUND STOP DRILLS NO MORE CRACKS WERE FOUND IAW SRM 51-01, PAR 21, B NEW DOUBLER WAS FABRICATED PAINTED AND INS

Next page: https://openairdocs.org/aircraft/N990DL/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 = 'N990DL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N990DL/reports

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