# Service difficulty reports: N998DL, cancelled Nov 29, 2022

A list on [N998DL, cancelled Nov 29, 2022](https://openairdocs.org/deregistered/N998DL-2022-11-29.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 · 232 reports

- [SDR DALA2020030501639](https://openairdocs.org/sdr/DALA2020030501639.md): Start Valve · malfunctioned · Mar 4, 2020 · N998DL · Doug MD88 · Engine Start Valves/Controls
  > R START VALVE OPEN ANNUNCIATED IN FLIGHT. SDR REPORTED DUE TO EMERGENCY DECLARED ACCORDING TO MCC EVENT NOTIFICATION. RT VALVE ANNUN ON EOAP ON ARRIVAL. R/R RT ENG START VALVE PER MD88 AMM 80-10. R/R EOAP PER MD88 AMM 31-00, LEAK CK GOOD, RAN ENG, SYS OPERATIN
- [SDR DALA2019092605516](https://openairdocs.org/sdr/DALA2019092605516.md): Wire Harness · defective · Sep 26, 2019 · N998DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT AT 30ED INOP. R&R HARNESS OPS NML REF AMM 33-52. (LP5596570)
- [SDR DALA2019080704631](https://openairdocs.org/sdr/DALA2019080704631.md): Light · inoperative · Aug 7, 2019 · N998DL · Doug MD88 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT 28D. REPLACED THE LIGHT ASSY PER AMM 33-50.
- [SDR DALA2019042422597](https://openairdocs.org/sdr/DALA2019042422597.md): Line · leaking · Apr 22, 2019 · N998DL · Doug MD88 · APU Engine Fuel and Control
  > AFT F/A SAID STRONG SMELL OF FUEL ONLY AFTER LANDING. THEN SMELL DISSIPATED BY THE TIME WE ARRIVED AT THE GATE. NO GO ODI. HAS EXCESSIVE AMOUNT OF FUEL IN APU FUEL LINE SHROUD DRAIN. POSSIBLE APU INLET CONTAMINATION. T/S FUEL LINE SHROUDS FOR LEAKS, NO FURTHER
- [SDR DALA2019042432595](https://openairdocs.org/sdr/DALA2019042432595.md): Door Frame · cracked · Apr 22, 2019 · N998DL · Doug MD88 · Fuselage Main, Structure
  > WHILE PERFORMING SVC CHECK FOUND 2" CRACK ON RT WHEEL WELL FWD FRAME BELOW DOOR PROX SWITCH. REPLACED RIGHT FWD WHEEL WELL DOOR JAMB PER BOEING DWG # 5930584. (LP5655004)
- [SDR DALA2019022701258](https://openairdocs.org/sdr/DALA2019022701258.md): Light · miswired · Feb 26, 2019 · N998DL · Doug MD88 · Light System Wiring
  > LT/RT OVERWING EMER LIGHT STAYS WITH SHIP BATT OFF AND COMPLETELY DEAD. FOUND B5-105 MISWIRED AND AFT EXIT SIGNS INOP. REPLACED B5-105 AND 2 EXIT SIGN BULBS PER MD88 AMM 33-53 AND WDM 33-51. (LP5308368)
- [SDR DALA2019011800331](https://openairdocs.org/sdr/DALA2019011800331.md): Wire · damaged · Jan 17, 2019 · N998DL · Doug MD88 · Light System Wiring
  > SEAT 24ED - 30ED, SEAT MOUNTED EMERGENCY LIGHT INOP. FOUND FUSE BLOWN IN PWR SUPPLY B5212. FOUND DAMAGED WIRE @ SEAT 30. REPAIRED WIRE IAW AMM 20-50. REPLACED FUSE IN PWR SUPPLY B5212 SYSTEM CKS GOOD. A/C OK FOR SVC. (LP4809443)
- [SDR DALA2019010300016](https://openairdocs.org/sdr/DALA2019010300016.md): Battery · discharged · Jan 2, 2019 · N998DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOP ROW 24LEFT AND RIGHT OVERWING EXITS THROUGH ROW 30. REPLACED BATTERY'S & PACK B5-212 ROW35 OVERHEAD REPLACED FUSES OF PACK OPS CKS PER AMM 33-53-00. (LP5236894)
- [SDR DALA2018123107447](https://openairdocs.org/sdr/DALA2018123107447.md): Fuse · blown · Dec 31, 2018 · N998DL · Doug MD88 · Emergency Lighting
  > RT SIDE EMERG SEAT LIGHTS INOP. FOUND 2 FUSES BLOWN IN POWER SUPPLY. R/R FUSES PER MD88 AMM 33-51. (LP5236881)
- [SDR DALA2018122707420](https://openairdocs.org/sdr/DALA2018122707420.md): Battery Pack · unknown · Dec 26, 2018 · N998DL · Doug MD88 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS STILL ON FROM INBOUND FLIGHT AND PWR OFF. R/R BOTH BATTERY PACK ASSY REF MD88 AMM 33-53. SYSTEM OPS CK GOOD. (LP5236865)
- [SDR DALA2018110506442](https://openairdocs.org/sdr/DALA2018110506442.md): Wire · shorted · Nov 3, 2018 · N998DL · Doug MD88 · Light System Wiring
  > EMERGENCY EXIT ROW LIGHTS OUT ROW 24-29. T/S FOUND SEAT 29 WIRING SHORTING. REPAIRDED WIRING PER SWPM AND REPLACED FUSE IN AFT BAT. PACK B5-212 CKS GOOD PER MD88 AMM 33-53. (LP4807245)
- [SDR DALA2018073004751](https://openairdocs.org/sdr/DALA2018073004751.md): Skin Panel · not reported · Jul 28, 2018 · N998DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > AWR, MTC REQUEST: TO REPAIR HORIZ STAB UPPER SKIN PANEL. REMOVE AND INSTALL RT ELEVATOR HYD POWER CONTROL VALVE AND HYD LINES PER AMM 27-30-07-201.
- [SDR DALA2018072604697](https://openairdocs.org/sdr/DALA2018072604697.md): Floor Panel · damaged · Jul 25, 2018 · N998DL · Doug MD88 · Fuselage Floor Panel
  > DAMAGE FLOOR PANLES NR 693C AND 1003D AT CABIN PAX. FLOOR PANELS NR 693C AND 1003D AT CABIN PAX. WERE REPLACCED PER AMM 53-20-01-201 P 7.
- [SDR DALA2018072604694](https://openairdocs.org/sdr/DALA2018072604694.md): Frame · cracked · Jul 24, 2018 · N998DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON FRAME Y=1510 CANT BTW 5 AND 6 HRS POSITION AT AFT ACCESORY COMPARTMENT. CRACK ON FRAME Y=1510 CANT BTW 5 AND 6 HRS POSITION AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER ERA 497316-14MA REV ORG.
- [SDR DALA2018072404634](https://openairdocs.org/sdr/DALA2018072404634.md): Skin Panel · cracked · Jul 23, 2018 · N998DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > CRACK OF 1.250" LENGTH WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL STA XH=-8.500. UPPER AFT SKIN WAS REPAIRED PER DWG SR09550028 REV D AND SRM 51-30-2 AND 51-30-5(ET). HFEC INSPECTION WAS ACCOMPLISHED ON RT HORIZONTAL STABILIZER UPPER AFT SKIN P
- [SDR DALA2018072304605](https://openairdocs.org/sdr/DALA2018072304605.md): Beam · corroded · Jul 21, 2018 · N998DL · Doug MD88 · Fuselage Miscellaneous Structure
  > OUT OF LIMITS CORROSION ON LOWER BEAM AT MID CARGO COMPARTMENT DOOR JAMB BTW STA 652 AND 673. BEAM AT MID CARGO COMPARTMENT DOOR JAMB BTW STA 652 AND 673 WAS REPAIRED PER SRM 53-05 FIG 123 CORROSION LEVEL 2.
- [SDR DALA2018070604390](https://openairdocs.org/sdr/DALA2018070604390.md): Pump · clogged · Jul 4, 2018 · N998DL · Doug MD88 · Hydraulic Pump (Electric/Engine), Main
  > ALTERNATE GEAR EXTENSION, CREW REPORTS THAT WHILE ENROUTE THE RIGHT HYDRAULIC SYSTEM BECAME INOPERATIVE WITH ZERO PRESSURE INDICATION. CREW USED ALTERNATE GEAR EXTENSION TO LOWER THE LANDING GEAR. MAINTENANCE FOUND RIGHT ENGINE DRIVEN PUMP AND CASE DRAIN FILTE
- [SDR DALA2018042302715](https://openairdocs.org/sdr/DALA2018042302715.md): Battery Pack · inoperative · Apr 22, 2018 · N998DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN THE AFT TAIL ARE INOPERATIVE, UPPER. REMOVED AND REPLACED THE BATTERIES IN THE AFT LAVATORY. EMERGENCY LIGHTS OPS NORMAL IAW AMM 33-50.
- [SDR DALA2018042302712](https://openairdocs.org/sdr/DALA2018042302712.md): Light · inoperative · Apr 22, 2018 · N998DL · Doug MD88 · Emergency Lighting
  > SEAT 18D EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT, OPS OK IAW AMM 33-50.
- [SDR DALA2018072604693](https://openairdocs.org/sdr/DALA2018072604693.md): Door · missing · Mar 25, 2018 · N998DL · Doug MD88 · Leading Edge Devices
  > LT WING LOWER SLAT TRACK COVER DOOR MISSING **DISPATCHER SELECT EXTENSION**. SLAT TRACK DOOR NR 6 LT WAS FABRICATED PER ERA 512356-14MA REV ORIGINAL SECTION II.
- [SDR DALA2018010300034](https://openairdocs.org/sdr/DALA2018010300034.md): Megaphone · inoperative · Jan 1, 2018 · N998DL · Doug MD88 · Emergency Equipment
  > AFT MEGAPHONE INOP. REPLACED INOP MEGAPHONE PER AMM 25-60. CKS GOOD. S/N OFF: 3541.
- [SDR DALA2017121208520](https://openairdocs.org/sdr/DALA2017121208520.md): Stringer · cracked · Dec 11, 2017 · N998DL · Doug MD88 · Wing, Longeron/Stringer
  > MD88 - WINGS / STRINGERS / RH STRINGER #17 AT XCW 12 / CRACK. DTA MONITOR INSPECTION LOG REFERENCE ER/A 546518-14, SECTION I REPAIR IS PENDING A DTA EVALUATION FROM BOEING WITHIN 18 MONTHS. ER/A 546518-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, LOGPAGE
- [SDR DALA2017101607539](https://openairdocs.org/sdr/DALA2017101607539.md): Battery Pack · inoperative · Oct 13, 2017 · N998DL · Doug MD88 · Emergency Lighting
  > SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE BETWEEN SEATS 13 AND 16. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-53.
- [SDR DALA2017091106779](https://openairdocs.org/sdr/DALA2017091106779.md): Cam · out of adjust · Sep 11, 2017 · N998DL · Doug MD88 · Aerodynamic Fairings
  > DURING TAIL ESCAPE SLIDE CHANGE. FOUND THE TAILCONE RELEASE CAM CLOCKED INCORRECTLY. ADJUSTED THE TAIL CONE RELEASE CAM IAW AMM 53-53-02.
- [SDR DALA2017020500995](https://openairdocs.org/sdr/DALA2017020500995.md): Wire · broken · Feb 5, 2017 · N998DL · Doug MD88 · Light System Wiring
  > SEAT 30 DE SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT CONTACT PIN IN CONNECTOR. TERMINATED THE WIRE IAW SWPM 20-90-03. CHECKED GOOD.
- [SDR DALA2016090206362](https://openairdocs.org/sdr/DALA2016090206362.md): Wire Harness · defective · Sep 2, 2016 · N998DL · Doug MD88 · Light System Wiring
  > EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 15DE. REPLACED ESCAPE PATH LIGHT HARNESS REF AMM 33-51. OPS CHECK GOOD.
- [SDR DALA2016062905017](https://openairdocs.org/sdr/DALA2016062905017.md): Lanyard · damaged · Jun 27, 2016 · N998DL · Doug MD88 · Emergency Equipment
  > BROKEN WIRES ON L1 EVACUATION SLIDE LANYARD CABLE, SN 00599. LANYARD CABLE WAS REPLACED IAW AMM 25-62-00-201.
- [SDR DALA2016062804970](https://openairdocs.org/sdr/DALA2016062804970.md): Access Door · corroded · Jun 27, 2016 · N998DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1335C. ACCESS PLATE 1335C WAS REPLACED.
- [SDR DALA2016062804968](https://openairdocs.org/sdr/DALA2016062804968.md): Stop · cracked · Jun 27, 2016 · N998DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED FORWARD EDGE STOPS NR 1 AND NR 3 AT FORWARD CARGO COMPARTMENT DOOR. CRACKED FORWARD EDGE STOPS 1 AND 3 WERE REPLACED IAW SRM 51-30-1,51-30-5 AND DWG 5910141, REV FE.
- [SDR DALA2016062704953](https://openairdocs.org/sdr/DALA2016062704953.md): Hinge · excess play · Jun 25, 2016 · N998DL · Doug MD88 · Cargo/Baggage Doors
  > FREE PLAY ON FWD/AFT HINGE AT FWD CARGO COMPARTMENT DOOR. FWD/AFT FWD CARGO DOOR HINGES WERE REMOVED IAW AMM 52-31-02-201. HINGES WERE REPAIRED IAW ER/A 497387-14MA, REV 13. REPAIRED HINGES WERE INSTALLED IAW AMM 52-31-02-201. FREE PLAY WAS CORRECTED.
- [SDR DALA2016062704949](https://openairdocs.org/sdr/DALA2016062704949.md): Frame · cracked · Jun 25, 2016 · N998DL · Doug MD88 · Wing, Rib/Bulkhead
  > CRACK WAS FOUND ON LT WING MAIN FRAME STR 11, STA 160. TASK CARD WAS PERFORMED WITH CARD 5712-01030-03. LT WING MAIN FRAME STR 11 REPAIR RII SECTION.
- [SDR DALA2016062704948](https://openairdocs.org/sdr/DALA2016062704948.md): Structure · corroded · Jun 25, 2016 · N998DL · Doug MD88 · Wing Miscellaneous Structure
  > CORROSION ON AREA OF SETTLEMENT OF AFT BOOST PUMP SECONDARY ACCESS COVER AT LT WING HEATER BLANKET. DUE TO EXCESSIVE DAMAGE LT WING HEATER BLANKET WAS REPLACED IAW AMM 30-80-02.
- [SDR DALA2016062704941](https://openairdocs.org/sdr/DALA2016062704941.md): Attach Fitting · cracked · Jun 25, 2016 · N998DL · Doug MD88 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LT DORSAL FIN ATTACH FITTING. FITTING WAS INSTALLED IAW SRM 51-30-5 BOLTS WERE TIGHTEN IAW AMM 20 30 01.
- [SDR DALA2016062604939](https://openairdocs.org/sdr/DALA2016062604939.md): Web · worn · Jun 25, 2016 · N998DL · Doug MD88 · Passenger/Crew Doors
  > WEAR ON UPPER WEB OVER UPPER HINGE AT AFT CABIN PRESSURE BULKHEAD DOOR. DAMAGE WEB WAS REPAIRED IAW SRM 52-01, FIG 4, SHEET 3.
- [SDR DALA2016062504932](https://openairdocs.org/sdr/DALA2016062504932.md): Cargo Track · corroded · Jun 24, 2016 · N998DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT TIE TRACK BETWEEN Y=1322 AND Y=1220 AT C3 COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-1 AND 51-30-5.
- [SDR DALA2016062504929](https://openairdocs.org/sdr/DALA2016062504929.md): Longeron Splice · cracked · Jun 23, 2016 · N998DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AWR, HIDDEN DAMAGE. CRACKED LONGERON SPLICE ON LONGERON 30 BETWEEN Y=1287 AND Y=1309 AT AFT CARGO COMPARTMENT. LONGERON SPLICE WAS REMOVED, FABRICATED NEW SPLICE ADJUSTED AND DRILLED, INSTALL AND APPLIED CIC IAW SRM 51-30-5,53-02 PAR 12, 5I-IO-4, 51-10-3 PAR
- [SDR DALA2016062404909](https://openairdocs.org/sdr/DALA2016062404909.md): Doubler · corroded · Jun 23, 2016 · N998DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL DOUBLER OF RADIO ALTIMETER CUTOUT ANTENNA LOCATED FROM STA Y=674-693 BETWEEN LONGERONS 30 AND 29LT. REMOVED FASTENERS STA Y=660 TO Y=693, LONG 30 AND LONG 29 LT IAW SRM 51-30-2 DOUBLER INTERNAL WAS REMOVED IAW SRM 51-30-2 DOUBLER INTERNA
- [SDR DALA2016062404908](https://openairdocs.org/sdr/DALA2016062404908.md): Cargo Track · corroded · Jun 23, 2016 · N998DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT & LT TIE TRACK BETWEEN STA Y=1003 AND Y=1155 AT AFT CARGO COMPARTMENT. NEW TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, TIE TRACK LT WAS ATTENDED WITH NRC 00779.
- [SDR DALA2016062404898](https://openairdocs.org/sdr/DALA2016062404898.md): Pan · cracked · Jun 23, 2016 · N998DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON PAN FORWARD EDGE BETWEEN BEAM 4 AND 5 AT AFT SERVICE DOOR, SN 00969. CRACK ON PAN WAS REPAIRED IAW ETI-88-16-231 REV 1 AND ER/A 541548-14, REV ORIGINAL.
- [SDR DALA2016062704946](https://openairdocs.org/sdr/DALA2016062704946.md): Nose Cowl · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Engine Cowling System
  > CRACKED LT NOSE COWLING LIP INTERNAL STRUCTURE. SERVICEABLE NOSE COWL WAS INSTALLED IAW AMM 71-10-01-201.
- [SDR DALA2016062404897](https://openairdocs.org/sdr/DALA2016062404897.md): Strap · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED STRAP REPAIR ON LOWER DOOR JAMB BETWEEN STA Y=1193 TO Y=1212 AT AFT CARGO DOOR JAMB C3. STRAP WAS REPLACED IAW SRM 53-05, FIG 123, SHEET 3, -9.
- [SDR DALA2016062304876](https://openairdocs.org/sdr/DALA2016062304876.md): Fitting · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Emergency Exits
  > CRACKED CLIPS ON AFT UPPER INTERNAL STRUCTURE AT AFT RT EMERGENCY EXIT DOOR. CLIPS WERE REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9957735, REV G.
- [SDR DALA2016062304875](https://openairdocs.org/sdr/DALA2016062304875.md): Beam · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON BEAM NR 1 FWD EDGE AT R1 DOOR IN REF NRTC, SN 1600. BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911579, REV L. BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911579, REV L.
- [SDR DALA2016062304874](https://openairdocs.org/sdr/DALA2016062304874.md): Beam · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON BEAM NR 1 FWD AND AFT EDGE AT MAIN ENTRY PASSENGER DOOR. BEAM WAS REPAIRED IAW SRM 52-05D, FIG 81 AND 82.
- [SDR DALA2016062304873](https://openairdocs.org/sdr/DALA2016062304873.md): Frame · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME STA Y=1510 CANT, POS 7 HRS AND 10 HRS AT AFT ACCESSORY COMPARTMENT. FRAMES UPPER SECTION AND LOWER SECTION LT SIDE WERE REPLACED IAW SRM 51-10-4, SRM 51-30-2, SRM 51-10-3 PAR 14.21 AND DWG 9911843, REV AC.
- [SDR DALA2016062304868](https://openairdocs.org/sdr/DALA2016062304868.md): Skin · punctured · Jun 22, 2016 · N998DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PUNCTURE ON AFT VENTRAL STAIR OUTER SKIN, STA Y=1474, CANT. DAMAGE WAS REPAIRED IAW SRM 53-04-2 FIG1.
- [SDR DALA2016062204837](https://openairdocs.org/sdr/DALA2016062204837.md): Exhaust Duct · cracked · Jun 22, 2016 · N998DL · Doug MD88 · Cabin Cooling System
  > CRACKED EXAHUST ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 20 LT AND 21 LT STA Y=256 TO Y=275. CRACKS ON EXHAUST WAS REPAIRED WITH METHOD 1 POSTERILY WITH METHOD 2 OF ER/A 464964-14MA, REV C, ETI 88-14-237, REV ORIGINAL. FPI WAS ACCOMPLISHED ON WELDED AREAS,
- [SDR DALA2016062304877](https://openairdocs.org/sdr/DALA2016062304877.md): Tab · debonded · Jun 21, 2016 · N998DL · Doug MD88 · Rudder, Tab Structure
  > PART RACKS DISBONDED LOWER CUP AT RUDDER CONTROL TAB DUE TO WEIGHT AND BALANCE IS OUT OF LIMITS. THE RUDDER CONTROL TAB WAS REPLACED UNDER CARD SN 01633.
- [SDR DALA2016062204836](https://openairdocs.org/sdr/DALA2016062204836.md): Doubler · corroded · Jun 21, 2016 · N998DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN Y=1287 AND Y=1309 AND LONGERON 29 RT AND 30 AT C3 COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 53-04-2, FIG 2.
- [SDR DALA2016062204834](https://openairdocs.org/sdr/DALA2016062204834.md): Skin · cracked · Jun 21, 2016 · N998DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON DOOR SKIN BETWEEN BEAM NR 4 AND BEAM 5 AT FWD MAIN ENTRY DOOR. SKIN WAS REPAIRED IAW ERA 501106-14MA, REV C AND ETI-88-16-151, REV 2.

Next page: https://openairdocs.org/deregistered/N998DL-2022-11-29/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 = 'N998DL' AND deregistration_id = 'N998DL-2022-11-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N998DL-2022-11-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.