# Service difficulty reports: N993DL, cancelled Apr 25, 2022

A list on [N993DL, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N993DL-2022-04-25.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 6 · 255 reports

- [SDR DALA2019123107630](https://openairdocs.org/sdr/DALA2019123107630.md): Access Door · missing · Dec 30, 2019 · N993DL · Doug MD88 · Nacelle/Pylon, Main Frame
  > FND ON ARRIVAL, NBR 2 ENG MISSING STARTER VALVE ACCESS DOOR. REPLACED NBR 2 ENGINE LOWER FWD COWL PER MD88 AMM 71-10. COWL ROBBED OFF SHIP 963. (LP6748864)
- [SDR DALA2019101505897](https://openairdocs.org/sdr/DALA2019101505897.md): Battery Pack · inoperative · Oct 15, 2019 · N993DL · Doug MD88 · Emergency Lighting
  > BOTH AFT OVERWING EMERGENCY EXIT DOOR LIGHTS INOP ON WALK AROUND. SERVICED ASSOCIATED BATTERY PACK PER MD88 AMM 33-53. LIGHTS CKS GOOD NOW. OK FOR SERVICE.
- [SDR DALA2019082604948](https://openairdocs.org/sdr/DALA2019082604948.md): Sensor · sparks · Aug 25, 2019 · N993DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > WHEN TURNING ON WINDSHIELD ANTI-FOG, A LOUD POP WAS HEARD AND SPARKS EMITTED FROM CAPTAIN'S WINDSHIELD HEAT SENSOR. FOUND TERMINAL ENDS LOOSE ON CAPT'S WINDSHIELD THERMAL SWITCH. SECURED SAME PER MD88 AMM 30-41. ANTI FOG OPS GOOD. REAPPLIED THERMAL HEAT SINK C
- [SDR DALA2019041002373](https://openairdocs.org/sdr/DALA2019041002373.md): Unknown · odor · Apr 9, 2019 · N993DL · Doug MD88 · Air Distribution System
  > CLIMBING THRU 30K FOR 34K NOTIFIED OF L AFT LAV SMOKE ALARM WITH FAINT HAZE & ODOR. CLEARED WITHIN 5 MIN. ENG HEAT TURNED ON APROX THE SAME TIME PERFORMED NO GO ODI ATA 21-72. C/W MD88 WORK CARD 2120-2367. C/W MD88 WORK CARD 7100-2619 STEPS 1 THROUGH 10. SS C/
- [SDR DALA2019031801766](https://openairdocs.org/sdr/DALA2019031801766.md): Battery Pack · discharged · Mar 18, 2019 · N993DL · Doug MD88 · Emergency Lighting
  > AFT CAT WALK TAIL CONE EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT REAR BATTERY PACK. IAW AMM 35-33 OPS CHECK OK. PN AD4002P. (LP5765082)
- [SDR DALA2019031101557](https://openairdocs.org/sdr/DALA2019031101557.md): Battery · discharged · Mar 11, 2019 · N993DL · Doug MD88 · Emergency Lighting
  > FWD GALLEY EMERG LIGHTS INOP. REPLACED BATTERIES. OPS CK GOOD. REF AMM 33-53. (LP5765059)
- [SDR DALA2019031001552](https://openairdocs.org/sdr/DALA2019031001552.md): Engine · damaged · Mar 9, 2019 · N993DL · Doug MD88 · Engine (Turbine/Turboprop)
  > PASSING 1100' IN CLIMB POWER, HEARD LOUD BANG FROM RIGHT ENGINE. RIGHT ENGINE ROLLED BACK AND STOPPED PRODUCING USEABLE THRUST. N1 APPROX 30 %. OIL PRESSURE 43 PSI. ENG CONTINUED TO ROTATE. THROTTLE PULLED TO IDLE AND FUEL LEVER TO OFF. ENG CONTINUED TO ROTATE
- [SDR DALA2019030501471](https://openairdocs.org/sdr/DALA2019030501471.md): Battery · discharged · Mar 4, 2019 · N993DL · Doug MD88 · Emergency Lighting
  > BOTH FWD OVERWING EMER EXIT DOOR L + R LTS INOP. REMOVED AND REPLACED BATTERIES FOR ASSOCIATED LTS. OPS CHECK NORMAL. OK FOR SVC PER AMM 33-53. (LP5765027)
- [SDR DALA2019010700058](https://openairdocs.org/sdr/DALA2019010700058.md): Retract Cylinder · bypassing · Jan 7, 2019 · N993DL · Doug MD88 · Landing Gear Door Actuator
  > AFTER T/O OUT OF TLH, L MAIN GEAR INDICATED UNSAFE WITH GEAR HANDLE UP. CYCLED GEAR HANDLE PER QRH, BUT LIGHT DID NOT GO OUT. FOUND LT MLG RETRACT CYL BYPASSING R/R RETRACT CYL ON LT MLG PER AMM 32-32. FOUND CK VALVE LEAKING. RPLD SAME. LEAK CK GOOD. C/W NO GO
- [SDR DALA2018121217154](https://openairdocs.org/sdr/DALA2018121217154.md): Control Box · contaminated · Dec 10, 2018 · N993DL · Doug MD88 · Brake Anti-Skid Section
  > SHIP 993 - BRAKE - AFTER LANDING GEAR EXTENSION ALL ANTI-SKID MESSAGES ILLUMINATED ON EOAP. THE CREW RAN THE QRH PROCEDURE BUT THE MESSAGES REMAINED. AFTER TOUCHDOWN, THE CREW HAD NO BRAKES AND USED REVERSERS TO SLOW THE AIRCRAFT. THE CREW THEN EXITED TO THE T
- [SDR DALA2018101005980](https://openairdocs.org/sdr/DALA2018101005980.md): Light · missing · Oct 9, 2018 · N993DL · Doug MD88 · Exterior Lighting
  > LOWER ANTI-COLLISION LIGHT MISSING. C/W ERA 572237-14 SECTION 1 TIME LIMITED REPAIR. SDR REPORTED DUE TO FACT THAT PART MAY HAVE DEPARTED FROM THE AIRCRAFT DURING FLIGHT.
- [SDR DALA2018090405395](https://openairdocs.org/sdr/DALA2018090405395.md): Battery Pack · discharged · Sep 1, 2018 · N993DL · Doug MD88 · Emergency Lighting
  > SEAT 15-23 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53 OP CHECK GOOD. OK FOR SRV.
- [SDR DALA2018081505089](https://openairdocs.org/sdr/DALA2018081505089.md): Battery Pack · inoperative · Aug 15, 2018 · N993DL · Doug MD88 · Emergency Lighting
  > OVERWING EXIT SIGNS INOPERATIVE. R & R BATTERY PACKS, B5103, AND B5105 IAW AMM 33-50, OPS CHECKED NORMAL.
- [SDR DALA2018061103937](https://openairdocs.org/sdr/DALA2018061103937.md): Panel · dislodged · Jun 10, 2018 · N993DL · Doug MD88 · Electrical Power System
  > AFT FLT ATTENDANT CALL PANEL DISLODGED DURING LANDING. F/A REPORTED AN ELECTRICAL SHOCK.
- [SDR DALA2018051903448](https://openairdocs.org/sdr/DALA2018051903448.md): Connector · defective · May 17, 2018 · N993DL · Doug MD88 · Light System Wiring
  > WIRE HARNESS TO SEAT 26D/E HAS BAD PLUG AT SIDE WALL PANEL. REPLACED SEAT JUMPER HARNESS AS REQ'D. ALL CKS GOOD. MEL AND PLACARD REMOVED.
- [SDR DALA2018042602826](https://openairdocs.org/sdr/DALA2018042602826.md): Door Frame · corroded · Apr 25, 2018 · N993DL · Doug MD88 · Fuselage Main, Structure
  > DURING INSPECTION, CORROSION FOUND ON THE LOWER BEAM OF THE AFT CARGO DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 123, 51-10-4, AND 51-10-2.
- [SDR DALA2018042402763](https://openairdocs.org/sdr/DALA2018042402763.md): Angle · cracked · Apr 24, 2018 · N993DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE ON THE AFT DOOR FRAME, OTBD END, AT THE LT MLG WW. THE ANGLE WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.
- [SDR DALA2018042002654](https://openairdocs.org/sdr/DALA2018042002654.md): Frame · cracked · Apr 20, 2018 · N993DL · Doug MD88 · Fuselage Main, Frame
  > BS 1463 CANTED FRAME CAP CRACKED. REPAIRED IAW ER/A 543145-14, REV A.
- [SDR DALA2018041902631](https://openairdocs.org/sdr/DALA2018041902631.md): Intercostal · cracked · Apr 18, 2018 · N993DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRAKED INTERCOSTAL, BS 1510, LONGERON 23L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-4.
- [SDR DALA2018010300026](https://openairdocs.org/sdr/DALA2018010300026.md): Strap · broken · Dec 31, 2017 · N993DL · Doug MD88 · Aerodynamic Fairings
  > VELCRO STRIP ON INTERIOR TAILCONE BARRIER STRAP BROKEN. REATTACHED VELCRO STRIP FOR AFT STAIR DOOR BARRIER STRAP. OPN CKS GOOD. OK FOR SVC.
- [SDR DALA2017112608286](https://openairdocs.org/sdr/DALA2017112608286.md): Battery Pack · inoperative · Nov 24, 2017 · N993DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE AT SEAT 32 CEILING. REPLACED BATTERY PACK IAW AMM 33-53. CHECKED NORMAL.
- [SDR DALA2017082206330](https://openairdocs.org/sdr/DALA2017082206330.md): Hydraulic System · failed · Aug 20, 2017 · N993DL · Doug MD88 · Hydraulic System, Main
  > EXPERIENCED A LEFT SYSTEM HYDRAULIC FAILURE WHILE IN CRUISE TO CUN. AN EMERGENCY LANDING WAS DECLARED. NO LEAKS WERE FOUND BY MAINTENANCE. THE LEFT SYSTEM RESERVOIR WAS BLED AND RE-SERVICED. THE PTU, EDP PRESSURE FILTER, CASE DRAIN FILTER, AND THE LEFT SYSTEM
- [SDR DALA2017050103520](https://openairdocs.org/sdr/DALA2017050103520.md): Circuit Breaker · defective · Apr 27, 2017 · N993DL · Doug MD88 · Hydraulic Pump, Auxiliary
  > RIGHT HYDRAULIC AUX PUMP CIRCUIT BREAKER POPPED AFTER TAKEOFF. CHECKED RT HYD AUX PUMP WIRING REF W/C 2920-01098-0201. FOUND NO POWER TO AUX PUMP ON ALL THREE PHASES. INSPECTED AUX PUMP C/B AND FOUND B PHASE WIRE BURNED AND B PHASE BUS BAR BURNED. REMOVED AND
- [SDR DALA2017011600385](https://openairdocs.org/sdr/DALA2017011600385.md): Altimeter · failed · Jan 14, 2017 · N993DL · Doug MD88 · Altimeter, Barometric/Encoder
  > CAPTAIN`S ALTIMETER OFF FLAG DURING CRUISE. MINOR BURNING ODOR AFTER ALTIMETER FROZE. PULLED A-3 CIRCUIT BREAKER AND ODOR SUBSIDED. REMOVED AND REPLACED CAPTAIN`S ALTIMETER IAW AMM 34-12, CHECKED GOOD.
- [SDR DALA2016061504721](https://openairdocs.org/sdr/DALA2016061504721.md): Power Supply · inoperative · Jun 15, 2016 · N993DL · Doug MD88 · Emergency Lighting
  > ON SERVICE, FOUND FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. T/S AND FOUND BATTERY AND POWER SUPPLY BAD. R & R POWER SUPPLY AND BATTERY IAW AMM 33-53. OP CHECK GOOD, OK FOR SERVICE.
- [SDR DALA2016041102770](https://openairdocs.org/sdr/DALA2016041102770.md): Charger · inoperative · Apr 9, 2016 · N993DL · Doug MD88 · Emergency Lighting
  > THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS AT ROWS 1 THROUGH 12 INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY PACK AND THE LIGHTS CHECKED OK.
- [SDR DALA2016040402524](https://openairdocs.org/sdr/DALA2016040402524.md): Line · loose · Apr 3, 2016 · N993DL · Doug MD88 · Fuel Storage
  > STRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONNEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.
- [SDR DALA2016040402511](https://openairdocs.org/sdr/DALA2016040402511.md): Line · loose · Apr 3, 2016 · N993DL · Doug MD88 · Fuel Storage
  > STRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.
- [SDR DALA2016032202233](https://openairdocs.org/sdr/DALA2016032202233.md): Cap · cracked · Mar 21, 2016 · N993DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED LOWER CAP BS 1463, CANT 11 HRS POSITION AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI 88-16-059, REV 7 AND ER/A 543145-14, REV ORIG SECTION I, TEMPORARY REPAIR, LENGHT CRACK 4".
- [SDR DALA2016032202232](https://openairdocs.org/sdr/DALA2016032202232.md): Spar Cap · cracked · Mar 21, 2016 · N993DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED VERTICAL STABILIZER SPAR CAP ON WEB BS 1463 CANT POS 11 HRS AT AFT ACCESORIES COMPARTMENT. VERTICAL STABILIZER SPAR CAP WAS REPAIRED IAW ER/A 543145-14, REV ORIGINAL AND ETI 88-16-059, REV 7, LENGHT CRACK 6".
- [SDR DALA2016032102132](https://openairdocs.org/sdr/DALA2016032102132.md): Skin · corroded · Mar 19, 2016 · N993DL · Doug MD88 · Airfoil Anti/De-ice System
  > CORROSION ON RT HEATER BLANKET SKIN AROUND ACCESS PLATE 1410C. RT HEATER BLANKET SKIN WAS REPAIRED WITH ER/A 543147-14AD, REV ORIGINAL.
- [SDR DALA2016032002112](https://openairdocs.org/sdr/DALA2016032002112.md): Frame · cracked · Mar 19, 2016 · N993DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED LOWER CAP BS 1463, CANT 11 HRS POSITION AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI-88-16-059, REV 7 AND ER/A 543145-14, REV ORIGINAL. SECTION I.
- [SDR DALA2016032002109](https://openairdocs.org/sdr/DALA2016032002109.md): Spar Cap · cracked · Mar 19, 2016 · N993DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED VERTICAL STABILIZER SPAR CAP ON WEB BS 1463 CANT POS 11 HRS AT AFT ACCESSORIES COMPARTMENT. VERTICAL STABILIZER SPAR CAP WAS REPAIRED IAW ER/A 543145-14 REV ORIGINAL SECTION I AND ETI-88-16-059, REV 7, TEMPORARY REPAIR. THIS REPAIR WILL BE MONITORIN
- [SDR DALA2016032002104](https://openairdocs.org/sdr/DALA2016032002104.md): Frame · cracked · Mar 19, 2016 · N993DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME ANGLE BS 1437 BETWEEN LONGERONS 3L - 3R. THE FRAME ANGLE WAS REPAIRED IAW ETI-88-16-113, REV 1 AND ER/A 543208-14, REVISION ORIGINAL.
- [SDR DALA2016032102136](https://openairdocs.org/sdr/DALA2016032102136.md): Skin · dented · Mar 18, 2016 · N993DL · Doug MD88 · Cargo/Baggage Doors
  > SEVERAL DENTS ON OUTER SKIN OF C3 DOOR. DENTS ON OUTER SKIN WERE MEASURED ARE CONSIDERED ADJACENT THEREFORE ARE OUT LIMITS IAW SRM 53-04-1, PAR 7C DENTS ADJACENT WERE ATTENDED WITH ERA 543153-14, REV ORIGINAL.
- [SDR DALA2016031902094](https://openairdocs.org/sdr/DALA2016031902094.md): Panel · damaged · Mar 18, 2016 · N993DL · Doug MD88 · Leading Edge Devices
  > NICK ON RIB BORE AT RT SLAT PANEL NR 3 XOS= 286. BORE WAS REPAIRED IAW ER/A 543189-14 REV ORIG.
- [SDR DALA2016031802078](https://openairdocs.org/sdr/DALA2016031802078.md): Web · cracked · Mar 16, 2016 · N993DL · Doug MD88 · Wing Miscellaneous Structure
  > CRACKED INNER WEB XRS 173 AT RT WING FIXED L/E INNER STRUCTURE. WEB CREAKED WAS REPAIRED IAW ETI-88-16-06 REV 2 AND ER/A 543205-14 REV ORIGINAL.
- [SDR DALA2016031602011](https://openairdocs.org/sdr/DALA2016031602011.md): Frame · cracked · Mar 15, 2016 · N993DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED CAP ON FRAME, BS 1463, CANT 4 HRS POS AT AFT ACCESSORY COMPARTMENT. CAP WAS REPAIRED IAW SRM 53-01, FIG 1, FIG 2, SRM 51-30-5, SRM 51-01, PAR 21.
- [SDR DALA2016031602008](https://openairdocs.org/sdr/DALA2016031602008.md): Longeron · cracked · Mar 15, 2016 · N993DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON END FITTING 1 BS 1338. LONGERON END WAS REPLACED IAW SRM 53-14-3, 51-30-5 AND 51-10-3, PAR 21 AND 14.
- [SDR DALA2016031501948](https://openairdocs.org/sdr/DALA2016031501948.md): Longeron · cracked · Mar 14, 2016 · N993DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 4 RT BS 1437 AT AFT ACC COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 1, 51-30-5, 51-10-3 PAR 21 AND 14 51-10-4.
- [SDR DALA2016031501947](https://openairdocs.org/sdr/DALA2016031501947.md): Finger Doubler · corroded · Mar 14, 2016 · N993DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER FINGER DOUBLER AT SPLICE 26 LT BETWEEN BS 1193 AND BS 1231. FASTENERS WERE REMOVED IAW SRM 51-30-2. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. FINGER DOUBLER WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. FINGER DOUBLER WAS FABRICATED IAW SRM
- [SDR DALA2016031501946](https://openairdocs.org/sdr/DALA2016031501946.md): Intercostal · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM BS 769 TO BS 788 BETWEEN LONGERON 27RT TO 28RT AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REMOVED AND NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-30-5 NEW INTERCOSTAL WAS FABRICATED IAW DWG 9915554, REV J AND SRM 51-10-2.
- [SDR DALA2016031501945](https://openairdocs.org/sdr/DALA2016031501945.md): Intercostal · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM BS 769 TO BS 788 BETWEEN LONGERON 28LT TO 27LT AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REPLACED BY NEW 1 IAW SRM 51-30-2, 51-30-5, 51-10-4.
- [SDR DALA2016031501944](https://openairdocs.org/sdr/DALA2016031501944.md): Pressure Panel · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON SLANT PRESSURE PANEL BS 939 BETWEEN BS 939 BETWEEN X=22 TO X=44 AT WING BOX. SLANT PRESSURE PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38 51-10-4 DWG 9923419, REV AG, AMM 20-30-01.
- [SDR DALA2016031401915](https://openairdocs.org/sdr/DALA2016031401915.md): Bushing · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Spoilers
  > CORROSION ON BUSHING HOUSING AT REACTION LEVER FITTING LT INBD SPOILER AREA. BUSHINGS HOUSINGS WERE REPAIRED IAW ER/A 543179-14, REV ORIGINAL.
- [SDR DALA2016031401914](https://openairdocs.org/sdr/DALA2016031401914.md): Bushing · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Spoilers
  > CORROSION ON BUSHING HOUSING AT REACTION LEVER FITTING RT INBD SPOILER AREA. BUSHINGS HOUSINGS WERE REPAIRED IAW ER/A 543179-14, REV ORIGINAL.
- [SDR DALA2016031401906](https://openairdocs.org/sdr/DALA2016031401906.md): Hinge · corroded · Mar 13, 2016 · N993DL · Doug MD88 · Elevator Structure
  > CORROSION ON BORE TO ATTACH BUSINGS AT LT ELEVATOR HINGE NR 1. BORES WERE REPAIRED IAW ETI-88-16-101, REV 1 AND ER/A 543191-14 REV ORIGINAL.
- [SDR DALA2016031401905](https://openairdocs.org/sdr/DALA2016031401905.md): Frame · cracked · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED WEB ON FRAME STA 463 CANT POS 11 HRS AT AFT ACCESORIES COMPARTMENT. WEB, STIFFENERS AND DOUBLERS WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. WEB WAS FABRICATED IAW DWG 9953015, REV. CB ITEM-53. NEW WEB AND STIFFENERS DOUBLER WERE INSTALLED IAW SRM 51-3
- [SDR DALA2016031401904](https://openairdocs.org/sdr/DALA2016031401904.md): Stiffener · cracked · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED STIFFENER ON FRAME BS 1463 CANT POS 11 HRS AT AFT ACCESSORIES COMPARTMENT. STIFFENER WAS REPLACED IAW SRM 51-10-3, 51-30-5 AND 51-10-4 AND DWG 9953015 REV. CB.
- [SDR DALA2016031401903](https://openairdocs.org/sdr/DALA2016031401903.md): Frame · cracked · Mar 13, 2016 · N993DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED WEB ON FRAME BS 1463 CANT 2 HRS POS AT AFT ACCY COMPARTMENT. WEB AND DOUBLER WERE REPLACED IAW DWG 9953015, REV CB ITEMS -58 AND -38 AND SRM 51-10-3, 51-10-3, 51-30-5 AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N993DL-2022-04-25/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 = 'N993DL' AND deregistration_id = 'N993DL-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N993DL-2022-04-25/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.