# Service difficulty reports: N932DL, cancelled Sep 16, 2019

A list on [N932DL, cancelled Sep 16, 2019](https://openairdocs.org/deregistered/N932DL-2019-09-16.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 3 · 110 reports

- [SDR DALA2018082405240](https://openairdocs.org/sdr/DALA2018082405240.md): Fastener · missing · Aug 23, 2018 · N932DL · Doug MD88 · Landing Gear Doors
  > LMLG INBD DOOR MISSING FASTENERS AND IS CRACKED AT FWD HINGE. REMVD LMLG DOOR REF MD88 AMM 32-12-01. INSTLD LMLG DOOR THROUGH STEP 3D REF MD88 AMM 32-12-01(520426. DOOR INSTALLATION AND RIG CKS COMPLETED IAW MD88 AMM 32-12-01. (LP4591052)
- [SDR DALA2018071004436](https://openairdocs.org/sdr/DALA2018071004436.md): Light · inoperative · Jul 10, 2018 · N932DL · Doug MD88 · Emergency Lighting
  > ENTRY LIGHT FWD INOP. F/A REPORT ENTRY L1 DOOR LT BULB INOP. RE-LAMPED ENTRY WAY BULB AT L1 DOOR. OPS GOOD OK FOR SVC.
- [SDR DALA2018042002663](https://openairdocs.org/sdr/DALA2018042002663.md): Lamp · inoperative · Apr 19, 2018 · N932DL · Doug MD88 · Passenger Compartment Lighting
  > THRESHOLD LIGHT INOPERATIVE. ENTRY LIGHT BLEW WITH SPARKS. REPLACED THE LAMPS. CHECKED OK.
- [SDR DALA2018022701206](https://openairdocs.org/sdr/DALA2018022701206.md): Panel · corroded · Feb 26, 2018 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON THE AFT LAVATORY SERVICE PANEL. REPAIRED IAW TOPP 20-50-20, AND PRI 541624-14 REV O -2. ERA 541624-14 REV A STEPS 1-13.
- [SDR DALA2018022601126](https://openairdocs.org/sdr/DALA2018022601126.md): Spar · cracked · Feb 23, 2018 · N932DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > RT VERTICAL STAB FRONT SPAR FORWARD FLANGE L/E ATTACH HOLES 3 EACH INDICATE CRACK. HOLES ARE MARKED 4,7, AND 8 BELOW L/E SPLICE PLATE. COMPLIED WITH ERA 556177-14AD REV A AND FOUND TO MATCH PRI 556177-14 REV A REVISION 0.
- [SDR DALA2018013000500](https://openairdocs.org/sdr/DALA2018013000500.md): Battery Pack · defective · Jan 29, 2018 · N932DL · Doug MD88 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHTS FROM 31 BACK INOP. SUSPECT BATTERY PACK B5-212, STA 1233, RT OVERHEAD BIN. ACCESS PANEL OPENED. T/S PER WDM 33-51-14 SHT2, FOUND FUSE OF B5-212 BLOWN. ISOLATED TAIL CONE HANDLE LT ASSY, LT OPN NML, REMOVED WIRES L982T14 AND L983E1
- [SDR DALA2018012500418](https://openairdocs.org/sdr/DALA2018012500418.md): Fuse · blown · Jan 24, 2018 · N932DL · Doug MD88 · Emergency Lighting
  > IN SEAT EMERGENCY LIGHTS OUT ROWS 31 AFT. REMOVED BATTERY PACK FOR ASSOCIATED SEATS AND FOUND ONE FUSE BAD ON THE CRADLE. REPLACED FUSE, REINSTALLED BATTERY AND OPS CK GOOD REF AMM 33-53.
- [SDR DALA2018012200327](https://openairdocs.org/sdr/DALA2018012200327.md): Fuse · failed · Jan 22, 2018 · N932DL · Doug MD88 · Emergency Lighting
  > SEAT EMERGENCY LIGHTS AT ROWS 31-36 FOUND INOPERATIVE. REPLACED THE FUSES FOR THE BATTERY PACK IAW AMM 33-53. CHECKED GOOD.
- [SDR DALA2018012200326](https://openairdocs.org/sdr/DALA2018012200326.md): Battery Pack · inoperative · Jan 22, 2018 · N932DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN THE TAIL SECTION FOUND INOPERATIVE. REPLACED THE BATTERIES, CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017122008759](https://openairdocs.org/sdr/DALA2017122008759.md): Smoke Detector · false activation · Dec 19, 2017 · N932DL · Doug MD88 · Smoke Detection
  > FWD LAVATORY SMOKE DETECTION SYSTEM- SMOKE DETECTOR SOUNDED WITH NO EVIDENCE OF SMOKE OR ODORS. REMOVED AND REPLACED THE FWD LAV TRASH SMOKE DETECTOR.
- [SDR DALA2017091806921](https://openairdocs.org/sdr/DALA2017091806921.md): Fire Loop · malfunctioned · Sep 16, 2017 · N932DL · Doug MD88 · Fire Detection
  > LEFT ENGINE FIRE LIGHT ILLUMINATED WITH AURAL WARNING DURING DESCENT. ACCOMPLISHED QRH PROCEDURE. ENGINE FIRE LIGHT REMAINED ON AFTER BOTH FIRE BOTTLE AGENTS USED. ENGINE SHUTDOWN AT 27,000 FT. ALL ENGINE INDICATIONS NORMAL BEFORE SHUTDOWN. LEFT ENGINE LOO
- [SDR DALA2017071905534](https://openairdocs.org/sdr/DALA2017071905534.md): Engine · making metal · Jul 18, 2017 · N932DL · Doug MD88 · Turbine Engine Oil System
  > LEFT ENGINE OIL STRAINER CLOGGED. EMERGENCY DECLARED. CHIP DETECTOR CLEAN AND FILTER CHECKED GOOD. FOUND METAL IN OIL TANK AND REPLACED ENGINE.
- [SDR DALA2017070505220](https://openairdocs.org/sdr/DALA2017070505220.md): Cap · displaced · Jul 4, 2017 · N932DL · Doug MD88 · APU Oil System
  > ON TAXI IN, CABIN BEGAN TO FILL WITH SMOKE. FOUND APU OIL CAP ON CROOKED AND OIL DRIPPING OUT OF APU INLET.
- [SDR DALA2017031101966](https://openairdocs.org/sdr/DALA2017031101966.md): Spar · cracked · Mar 10, 2017 · N932DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER SPAR LEADING EDGE CRACKED. COMPLIED WITH ERA 556177-14AD, REV ORIG, AND PRIS 556177-14AD, REV 0-8.
- [SDR DALA2017031101965](https://openairdocs.org/sdr/DALA2017031101965.md): Spar Cap · cracked · Mar 10, 2017 · N932DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB FRONT SPAR CAP HAD CRACK INDICATIONS, REPAIRED IAW ERA 556177-14 AD REV ORIG.
- [SDR DALA2016031401942](https://openairdocs.org/sdr/DALA2016031401942.md): Charger · failed · Mar 13, 2016 · N932DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 1 TO 30. THE BATTERY CHARGER AND DIODE WAS REPLACED.
- [SDR DALA2016030301652](https://openairdocs.org/sdr/DALA2016030301652.md): Battery Pack · inoperative · Mar 3, 2016 · N932DL · Doug MD88 · Emergency Lighting
  > THE FLIGHT CREW OF FLIGHT 333, FOUND EMERGENCY EXIT LIGHTS AT LT AND RT FORWARD DOORS, FORWARD GALLEY, AND SEAT ROWS ROWS 1 THROUGH 30 INOPERATIVE. CVG MAINTENANCE REPLACED BATTERY PACK AND CHARGER B5-211 AND THE LIGHTS CHECKED OK.
- [SDR DALA2016012500570](https://openairdocs.org/sdr/DALA2016012500570.md): Support Bracket · cracked · Jan 23, 2016 · N932DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED UPPER BRACKET SUPPORT AND MISSING SCREW ON LOWER BRACKET SUPPORT OF EST NDAR ELECTRONIC MODULE AT FWD FACE OF FUEL CENTER TANK BRACKET SUPPORT WAS REPLACED IAW DWG 5939757-3, REV K.
- [SDR DALA2016012400551](https://openairdocs.org/sdr/DALA2016012400551.md): Skin · corroded · Jan 23, 2016 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AND INNER PRODUCTION DOUBLER AROUND AFT LAV SERVICE PANEL. ALSO CORROSION IS RUNNING UNDER SKIN, PANEL AND DOUBLERS. DUE TO EXCESSIVE CORROSION AREA WAS REPAIRED IAW ERA 541624-14, REV ORIG.
- [SDR DALA2016012200528](https://openairdocs.org/sdr/DALA2016012200528.md): Door Frame · corroded · Jan 22, 2016 · N932DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER EDGE AT DOOR JAMB AFT, MID AND FWD CARGO. MID CARGO WAS ATTENDED WITH NRC 20000097097, CARD 156, ZONE 100, AFT CARGO: NEW SPACER WAS INSTALLED IAW ERA 489172-14, REV ORIGINAL SRM 51-10-3, PAR 21, 14, 38 AND 26 FWD CARGO WAS ATTENDED WITH NR
- [SDR DALA2016012300537](https://openairdocs.org/sdr/DALA2016012300537.md): Skin · corroded · Jan 21, 2016 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > EXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.
- [SDR DALA2016012100500](https://openairdocs.org/sdr/DALA2016012100500.md): Access Panel · damaged · Jan 20, 2016 · N932DL · Doug MD88 · Rudder, Plate/Skin
  > DAMAGE PAINT ON ACCESS PLATE 6508A, RUDDER. ACCESS PLATE 6508A, RUDDER WAS PAINTED IAW SRM 51-10-3B. PROCESS B & C AND METALIZED WAS REPAIRED IAW SRM 51-70-1A, D PAR 27.
- [SDR DALA2016012000443](https://openairdocs.org/sdr/DALA2016012000443.md): Access Panel · damaged · Jan 19, 2016 · N932DL · Doug MD88 · Standard Practices/Structures
  > DAMAGE FLAME SPRAY ON ACCESS PLATE 6504A0. ACCESS PLATE 6504A WAS REPAIRED IAW SRM 51-70-1AD, PAR 23, AND CARD 2000-8149-01, JOB 000-002.
- [SDR DALA2016012300543](https://openairdocs.org/sdr/DALA2016012300543.md): Bottle · low pressure · Jan 18, 2016 · N932DL · Doug MD88 · Escape Slide
  > MAINTENANCE FOUND THE R1 EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE INDICATOR IN THE RED. THE R1 EMERGENCY ESCAPE SLIDE WAS REPLACED.
- [SDR DALA2016011800416](https://openairdocs.org/sdr/DALA2016011800416.md): Longeron · cracked · Jan 17, 2016 · N932DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 4L AT INTERSECTION WITH FRAME AT BS 200. SECTION OF THE LONGERON WAS REMOVED IAW SRM 53-02, PAR 12, FIG 18. A NEW SECTION AND REPAIR SPLICE WERE ADJUSTED IAW SRM 53-02, PAR 12, FIG 18. THE NEW LONGERON AND SPLICE WERE TREATED AND PAINTED IA
- [SDR DALA2016011800415](https://openairdocs.org/sdr/DALA2016011800415.md): Skin · worn · Jan 17, 2016 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > WEAR ON BS 1309, LONGERON 19R OUTER FUSELAGE SKIN. REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 3.
- [SDR DALA2016011500361](https://openairdocs.org/sdr/DALA2016011500361.md): Skin · dented · Jan 14, 2016 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.
- [SDR DALA2016011400300](https://openairdocs.org/sdr/DALA2016011400300.md): Skin · cracked · Jan 13, 2016 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1480. THE SKIN WAS REPAIR IAW SRM 53-01.
- [SDR DALA2016010600052](https://openairdocs.org/sdr/DALA2016010600052.md): Fuse · failed · Jan 5, 2016 · N932DL · Doug MD88 · Emergency Lighting
  > FWD CABIN, ROWS 30 AND UP, AISLE EMERGENCY LIGHTS INOPERATIVE, SEAT MOUNTED. REPLACED FUSE IN BATTERY PACK B5-211. OPS CHECK GOOD.
- [SDR DALA2016010300015](https://openairdocs.org/sdr/DALA2016010300015.md): Wire · damaged · Jan 2, 2016 · N932DL · Doug MD88 · Light System Wiring
  > MAINTENANCE FOUND ALL AISLE AND L1 AND R1 EMERGENCY EXIT SIGNS INOPERATIVE. A WIRE FOR SEAT ROW 13-23 WAS FOUND DISCONNECTED AT PLUG AND COMING IN CONTACT WITH AIRFRAME. THE WIRE WAS REINSTALLED AND THE LIGHTS CHECKED OK.
- [SDR DALA2015123107770](https://openairdocs.org/sdr/DALA2015123107770.md): Fuse · failed · Dec 30, 2015 · N932DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY LIGHTING INOPERATIVE AFT OF SEAT ROW 35. THE BATTERY PACK FUSE WAS REPLACED AT ROW 35. LIGHTS CHECKED OK.
- [SDR DALA2015071504389](https://openairdocs.org/sdr/DALA2015071504389.md): Support Angle · cracked · Jul 14, 2015 · N932DL · Doug MD88 · Vertical Stabilizer
  > DURING JACKSCREW INSPECTION FOUND RT VERTICAL STABILIZER STRUCTURE CRACKED. REMOVED RT VERTICAL STABILIZER SUPPORT ANGLE. THE SUPPORT ANGLE WAS FABRICATED, HEAT TREATED, DRILLED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04.
- [SDR DALA2015071504388](https://openairdocs.org/sdr/DALA2015071504388.md): Support · cracked · Jul 14, 2015 · N932DL · Doug MD88 · Vertical Stabilizer
  > DURING JACKSCREW INSPECTION, FOUND LT VERTICAL SUPPORT STRUCTURE CRACKED. REMOVED LT VERTICAL STABILIZER SUPPORT STRUCTURE, CLIP, REPLACEMENT CLIP WAS FABRICATED. DRILLED, PAINTED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04 AS A REF.
- [SDR DALA2015052803572](https://openairdocs.org/sdr/DALA2015052803572.md): Unknown · smoke · May 26, 2015 · N932DL · Doug MD88 · Air Distribution System
  > FLIGHT RETURNED TO DEPARTURE AFTER SMOKE ACCUMULATED IN THE CABIN AND COCKPIT. THE AFT LAVATORY SMOKE DETECTOR ALSO SOUNDED BRIEFLY. MAINTENANCE REPLACED A LEAKING APU AND ACCOMPLISHED THE PNEUMATIC SYS DUCT BURN OUT PROCEDURES.
- [SDR DALA2015051903361](https://openairdocs.org/sdr/DALA2015051903361.md): Gasket · leaking · May 17, 2015 · N932DL · Doug MD88 · APU Oil System
  > F/A AND PASSENGERS EXPERIENCED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. THE AFT LAVATORY SMOKE DETECTOR WAS SOUNDING DURING THE CLIMB THROUGH 7000 FT. THE CREW DECLARED AN EMERGENCY AND RETURNED. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH OIL. A LEAK AT
- [SDR DALA2014072804254](https://openairdocs.org/sdr/DALA2014072804254.md): Pin · unsecure · Jul 26, 2014 · N932DL · Doug MD88 · Escape Slide
  > DURING INSPECTION OF THE L1 DOOR SLIDE, MAINTENANCE FOUND THE SLIDE PIN NOT ENGAGED AND SLIDE PARTIALLY INFLATED. MAINTENANCE R & R THE SLIDE PACK.
- [SDR DALA14015820932](https://openairdocs.org/sdr/DALA14015820932.md): Wire · broken · Mar 7, 2014 · N932DL · Doug MD88 · Light System Wiring
  > EMERGENCY ESCAPE LIGHT AT ROW 28 INOPERATIVE. FOUND WIRE BROKEN AT CONNECTOR. INSTALLED NEW CONNECTOR IAW CH 20, OPS CHECKED OK.
- [SDR DALA14005160932](https://openairdocs.org/sdr/DALA14005160932.md): Bracket · worn · Jan 23, 2014 · N932DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN BEYOND 50 PERCENT. BRACKETS REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK COMPLETED SATISFACTORILY.
- [SDR DALA14005150932](https://openairdocs.org/sdr/DALA14005150932.md): Conduit · out of position · Jan 23, 2014 · N932DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT.5. CLAMPS REPLACED AND CONDUIT ADJUSTED IAW THE MM.
- [SDR DALA14005140932](https://openairdocs.org/sdr/DALA14005140932.md): Skin · cracked · Jan 22, 2014 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON SKIN ABOVE PYLON BS 1380, LONGERON 13L, ACCOMPLISHED HFEC OF AREA IAW NDT SPM 06-10-01, CRACK INDICATION VERIFIED. REMOVED CRACK COMPLETED, DAMAGE CONTAINED USING HFEC NDT 06-10-01-001.
- [SDR DALA13037540932](https://openairdocs.org/sdr/DALA13037540932.md): Turnbuckle · broken · Aug 2, 2013 · N932DL · Doug MD88 · Aerodynamic Fairings
  > DURING INSPECTION, MX FOUND THAT THE TAILCONE CATWALK COUNTER BALANCE CABLE WAS BROKEN ON THE RT SIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE MOVEABLE CATWALK COUNTER BALANCE CABLE
- [SDR DALA13013840932](https://openairdocs.org/sdr/DALA13013840932.md): Connector · inoperative · Mar 27, 2013 · N932DL · Doug MD88 · Light System Wiring
  > DURING SERVICE CHECK, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT ROW 35D. REPLACED SEAT 35D EMERGENCY LIGHT HARNESS CONNECTOR AND OPERATION CHECKED NORMALLY.
- [SDR DALA12016490932](https://openairdocs.org/sdr/DALA12016490932.md): Battery · inoperative · Dec 14, 2012 · N932DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN ABOVE ROW 23 WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA1250260932](https://openairdocs.org/sdr/DALA1250260932.md): Connector · loose · Oct 6, 2012 · N932DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING BETWEEN SEAT ROWS 16 TO 30 WERE INOPERATIVE. MX FOUND A LOOSE CONNECTION AT THE BATTERY PACK AND SECURED. THE FUNCTIONAL CHECK OF THE SYSTEM WAS SATISFACTORY.
- [SDR DALA1248580932](https://openairdocs.org/sdr/DALA1248580932.md): Longeron · cracked · Sep 17, 2012 · N932DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, A CRACK WAS FOUND ON LT LONGERON 16 BS Y=1437. REPLACED LONGERON SECTION AND SPLICE IAW SRM 51-30-2 51-30-5 53-14-4 AND DWG 5910228, REV KH.
- [SDR DALA1248570932](https://openairdocs.org/sdr/DALA1248570932.md): Longeron Splice · damaged · Sep 17, 2012 · N932DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, ELONGATED HOLES WERE FOUND ON SPLICE AND LONGERON 2L STA Y=227 AT FUSELAGE INNER STRUCTURE. REPAIRED LONGERON AND SPLICE IAW SRM 53-02, FIG 18.
- [SDR DALA1248550932](https://openairdocs.org/sdr/DALA1248550932.md): Skin · corroded · Sep 16, 2012 · N932DL · Doug MD88 · Wing, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND ON LT WING LOWER SKIN AT STATION XRS=118 LENGTH 3.218" WIDE 0.531" AND DEPTH 0.054". AREA WAS BLENDED OUT AND LEAVE AS IS CONDITION IAW ER/A 506622-14 REV, ORIG.
- [SDR DALA1248450932](https://openairdocs.org/sdr/DALA1248450932.md): Skin · cracked · Sep 14, 2012 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CRACKS WERE FOUND ON FUSELAGE SKIN PRODUCTION. DOUBLER BS 1429 BTW LONGERON 2-3R AND BTW LONGERON 2-3L. REPLACED FUSELAGE SKIN PRODUCTION DOUBLER IAW DWG 5910011, REV CJ.
- [SDR DALA1248440932](https://openairdocs.org/sdr/DALA1248440932.md): Skin · cracked · Sep 14, 2012 · N932DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN FWD SERVICE DOOR FRAME AREA AFT LOWER SECTION STA Y=195. CUT OUT DAMAGE SKIN AND INSTALL DOUBLER TRIPLER FILLED IAW ER/A 504401-14AD.
- [SDR DALA1248430932](https://openairdocs.org/sdr/DALA1248430932.md): Door Frame · worn · Sep 14, 2012 · N932DL · Doug MD88 · Fuselage Main, Structure
  > DURING HMV, WEAR WAS FOUND ON FWD SERVICE DOOR FRAME FWD LOWER SECTION BS 172. REPLACED LOWER SERVICE DOOR FRAME IAW ER/A 506610-14 REV ORIG AND SRM 53-05 FIG 55.

Next page: https://openairdocs.org/deregistered/N932DL-2019-09-16/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 = 'N932DL' AND deregistration_id = 'N932DL-2019-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N932DL-2019-09-16/reports

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