# Service difficulty reports: N872SJ

A list on [N872SJ](https://openairdocs.org/aircraft/N872SJ.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 · 54 reports

- [SDR U2RA449SPIM003](https://openairdocs.org/sdr/U2RA449SPIM003.md): Skin · corroded · Feb 11, 2011 · N872SJ · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > RT HORIZ STAB BETWEEN XE 75.672 AND XE 147.906 T/E UPPER PANEL SKIN WITH CORROSION AROUND FASTENERS.
- [SDR U2RA449SPIM004](https://openairdocs.org/sdr/U2RA449SPIM004.md): Drive Assy · cracked · Feb 7, 2011 · N872SJ · Doug DC871F · Rudder Tab Control System
  > RUDDER TAB DRIVE SECTOR BROKEN.
- [SDR U2RA449SPIM002](https://openairdocs.org/sdr/U2RA449SPIM002.md): Web · cracked · Jan 6, 2011 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > FUSELAGE TAIL SECTION INTERIOR, FS 1817 TO FS 1823 UPPER WEB WITH 11" CRACK.
- [SDR U2RA449SPIM001](https://openairdocs.org/sdr/U2RA449SPIM001.md): Skin · worn · Jan 5, 2011 · N872SJ · Doug DC871F · Wing, Plate/Skin
  > LT WING, T/E UPPER SURFACE, XRS 272 EXISTING REPAIR WITH WEAR.
- [SDR 2009F00089](https://openairdocs.org/sdr/2009F00089.md): Line · cracked · Oct 1, 2009 · N872SJ · Doug DC871F · Hydraulic System, Main
  > DURING DESCENT HYD QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYD CHECKLIST FOR APPROACH AND LANDING. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. ACFT RETURNED TO SERVICE.
- [SDR U2RA2009F00088](https://openairdocs.org/sdr/U2RA2009F00088.md): Line · cracked · Oct 1, 2009 · N872SJ · Doug DC871F · Hydraulic System, Main
  > IN DESCENT HYDRAULIC QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYDRAULIC CHECKLIST FOR APPROACH AND LANDING AT LBBG. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. AIRCRAFT RETURNED TO SERVICE.
- [SDR U2RA872LP2993](https://openairdocs.org/sdr/U2RA872LP2993.md): Cable · out of rig · Dec 25, 2008 · N872SJ · Doug DC871F · Fuel Controlling System
  > NR 1 ENGINE FLAMED OUT AT IDLE AT 30,000 FT. BEGAN PERFORMING ENGINE FLAMEOUT ABNORMAL CK LIST. ENGINE RELITE AND PERFORMED NORMALLY AFTER IGNITION TURNED ON. FINISHED ABNORMAL CK LIST. WEATHER VMC. PERFORMED PULL, TRAVEL AND RIGGING CHECKS OF VBV AND VSV
- [SDR U2RA872CWO1839](https://openairdocs.org/sdr/U2RA872CWO1839.md): Strap · cracked · Oct 24, 2008 · N872SJ · Doug DC871F · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND RT WING XFS 6.225 CENTER LEADING EDGE INTERIOR LOWER STRAP HAS 5 INCH CRACK.
- [SDR U2R2008F00010](https://openairdocs.org/sdr/U2R2008F00010.md): Strap · cracked · Oct 14, 2008 · N872SJ · Doug DC871F · Wing Miscellaneous Structure
  > DURING C-CHECK FOUND RT WING XFS 341.500 CENTER LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 12 INCHES CRACK. (K)
- [SDR U2R2008F00012](https://openairdocs.org/sdr/U2R2008F00012.md): Fitting · corroded · Oct 13, 2008 · N872SJ · Doug DC871F · Engine Thrust Reverser
  > DURING C-CHECK FOUND NR 1, 2, 3, 4 ENGINE THRUST REVERSER TRANSLATING COWL RAIL FITTINGS CORRODED. (K)
- [SDR U2R2008F00011](https://openairdocs.org/sdr/U2R2008F00011.md): Strap · cracked · Oct 13, 2008 · N872SJ · Doug DC871F · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND RT WING XFS 430.000 CTR LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 18 INCH CRACK. (K)
- [SDR U2R2008F00009](https://openairdocs.org/sdr/U2R2008F00009.md): Skin · corroded · Aug 25, 2008 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSP, FOUND FUSELAGE EXTERIOR FS 8.000, L-21R SKIN WITH BULGING AND CHERRY MAX RIVETS. (K)
- [SDR U2R2008F00008](https://openairdocs.org/sdr/U2R2008F00008.md): Structure · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, FOUND LWR CARGO COMPARTMENT, STA 560.000 RT CUSP EXTRUSION WITH 2 INCH CRACK. (K)
- [SDR U2R2008F00007](https://openairdocs.org/sdr/U2R2008F00007.md): Strap · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, FOUND AFT SERVICE DOOR (R2) AFT UPPER JAMB CORNER WITH CRACK OF 0.800 LENGTH ON BEAR STRAP (AFTER ACCOMPLISHED X-RAY INSPECTION). (K)
- [SDR U2R2008F00006](https://openairdocs.org/sdr/U2R2008F00006.md): Frame · corroded · Aug 25, 2008 · N872SJ · Doug DC871F · Fuselage Main, Frame
  > DURING C-CHECK INSP, FOUND FWD CARGO COMPARTMENT F3 8.00 BTW L-24R FRAME WITH CORROSION. (K)
- [SDR U2R2008F00005](https://openairdocs.org/sdr/U2R2008F00005.md): Stringer · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Wing, Longeron/Stringer
  > DURING C-CHECK INSP, FOUND RT WING X RS 202 NR 4 MAIN FUEL TANK STRINGER 67 HAS 2 INCH CRACK BY ACCESSORY PANEL NR 5050. (K)
- [SDR U2R2008F00004](https://openairdocs.org/sdr/U2R2008F00004.md): Stringer · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Wing, Longeron/Stringer
  > DURING C-CHECK INSP, FOUND RT WING X RS NR 4 MAIN FUEL TANK STRINGER 58 HAS 2 INCH TRANSVERSAL CRACK BY ACCESSORY PANEL NR 5050. (K)
- [SDR U2R2008F00003](https://openairdocs.org/sdr/U2R2008F00003.md): Support Angle · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Wing Miscellaneous Structure
  > DURING C-CHECK INSP, FOUND LT WING X RS 71, 5-52 NR 2 MAIN FUEL TANK INTERIOR LOWER SUPPORT ANGLE CRACKED. (K)
- [SDR U2R2008F00002](https://openairdocs.org/sdr/U2R2008F00002.md): Bracket · cracked · Aug 25, 2008 · N872SJ · Doug DC871F · Wing, Attach Fittings
  > DURING C-CHECK INSP, FOUND LT WING NR 1 ALTERNATE FUEL TANK INTERIOR BOOST PUMP BRACKET FITTING (2) CRACKS. (K)
- [SDR U2R2008F00001](https://openairdocs.org/sdr/U2R2008F00001.md): Skin · dented · Aug 25, 2008 · N872SJ · Doug DC871F · Elevator, Plate/Skin
  > DURING C-CHECK INSP, FOUND RT ELEVATOR XE117-594 LOWER SURFACE DENTED. (K)
- [SDR U2RA872LP2804](https://openairdocs.org/sdr/U2RA872LP2804.md): Engine · flamed out · Nov 28, 2007 · N872SJ · Doug DC871F · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FLAMED OUT TOP OF DESCENT AT IDLE. RELIGHT PERFORMED IAW INFLIGHT ENGINE START PROCEDURES, OBSERVED NORMAL START AND INDICATION.
- [SDR U2RA872LP2801](https://openairdocs.org/sdr/U2RA872LP2801.md): Skin · corroded · Nov 25, 2007 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1440 LONGERON 36 RT EXTERNAL LOWER SKIN.
- [SDR U2RA1576872](https://openairdocs.org/sdr/U2RA1576872.md): Skin · cracked · Jan 23, 2007 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND CRACK AT AFT CARGO COMPARTMENT STATION 1380 STRINGER 36 RT ON EXTERNAL LOWER SKIN. COMPLETED FUSELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FUSELAGE STATION 1380/LONG 36R PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-07027-1 AND FAA FO
- [SDR U2RA1535872](https://openairdocs.org/sdr/U2RA1535872.md): Skin · corroded · Jan 19, 2007 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND CORROSION AT AFT CARGO COMPARTMENT AREA STATION 1418 STRINGER 36 RT ON EXTERNAL LOWER SKIN. FOUND 1" CRACK FWD OF FLIGHT STATION 1418 STRINGER 36 RT EXTERNAL SKIN. COMPLETED FUSELAGE SKIN TEMPORARY EXTERNAL REPAIR AT FS 1418/LONG 36 R
- [SDR U2RAM83088](https://openairdocs.org/sdr/U2RAM83088.md): Fitting · corroded · Jun 21, 2005 · N872SJ · Doug DC871F · Fuselage Main, Attach Fittings
  > LONGERON END FITTING LOCATED AT FRAME 80 AFT, L27R FOUND CORRODED BEYOND LIMITS. CLASSIFIED AS LEVEL 2 CORROSION.
- [SDR U2RA3056](https://openairdocs.org/sdr/U2RA3056.md): Bellcrank · disconnected · May 26, 2005 · N872SJ · Doug DC871F · Elevator Tab Control System
  > DURING INSPECTION, RT ELEVATOR GEARED TAB OUTBOARD CRANK P/N 4710542-3 FOUND DISCONNECTED FROM LINK P/N 271442-501. NOTE: AIRCRAFT IS CURRENTLY CLASSIFIED PART 91.
- [SDR 872SJ009](https://openairdocs.org/sdr/872SJ009.md): Floor Support · corroded · Jan 7, 2005 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > LT W/W UPPER LT SIDE FWD AND AFT OF SIXTH FLOOR SUPPORT HAS CORROSION. GBAMC NR 4178 CLEANED, CHECKED FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED LT W/W, L/H SIDE AFT FLOOR SUPPORT AT STA 960.00 AND REPLACED FLOOR SUPPORT FITTING AT STA 960.00 IAW
- [SDR 872SJ008](https://openairdocs.org/sdr/872SJ008.md): Gusset · cracked · Nov 2, 2004 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > RT UPPER GUSSET CRACKED AT STA XW5.000 GBAMC NR#04187. STOP DRILLED, FAB`D DOUBLER IAW DC-8 SRM. INSTALLED TOP AND BOTTOM DOUBLER IAW DC-8 SRM 51-1-21 AT STA XW5.000
- [SDR 872SJ006](https://openairdocs.org/sdr/872SJ006.md): Finger Doubler · corroded · Oct 27, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > LT OB TOP SIDE OF WHEEL WELL PRESSURE DOGHOUSE BETWEEN STA 960 AND 980, FINGER DOUBLER HAS CORROSION ON FWD UNDERSIDE. GBAMC NR304186 -OPEN-
- [SDR 872SJ005](https://openairdocs.org/sdr/872SJ005.md): Finger Doubler · corroded · Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > CARGO AREA RT SIDE STA 960 HAS CORROSION UNDER FINGER DOUBLER UNDER FLOORBOARD. GBAMC NR04182 -OPEN-
- [SDR 872SJ007](https://openairdocs.org/sdr/872SJ007.md): Structure · corroded · Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Main, Structure
  > LT WW UPPER LT SIDE FWD AND AFT OF NR 6 FLOOR SUPPORT HAS CORROSION. GBAMC NR04178 -OPEN-
- [SDR 872SJ004](https://openairdocs.org/sdr/872SJ004.md): Floor Support · corroded · Oct 22, 2004 · N872SJ · Doug DC871F · Fuselage Miscellaneous Structure
  > LT W/W LT SIDE UPPER, SECOND FLOOR SUPPORT HAS CORROSION ON LOWER SIDE. GBAMC NR04176 -OPEN-
- [SDR 872SJ003](https://openairdocs.org/sdr/872SJ003.md): Door · corroded · Oct 22, 2004 · N872SJ · Doug DC871F · Tail Cone Doors
  > D-PIT, AFT BULKHEAD DOOR 645 CORRODED GBAMC NR#04172 CUT OUT DAMAGED MATERIAL ON D PIT DOOR AFT BULKHEAD DOOR 645 IAW DC-8 SRM 52-2-0 FIG 4 SHEET 2. FABRICATED DOUBLER PATCH OUT OF 7075T6.032 AND INSTALLED DOUBLER PATCH ON D-PIT BULKHEAD DOOR IAW DC-8 SRM 52
- [SDR 872SJ001](https://openairdocs.org/sdr/872SJ001.md): Skin · corroded · Oct 21, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > LAV ACCESS SERVICE PANEL HAS CORROSION UNDER PAINT GBAMC NR 04161 AND NR 04185 UPON INVESTIGSTION FOUND SKIN TO BE OUT OF LIMITS BELOW LIP ON ACCESS DOOR, REMOVED DAMAGED SKIN AREA OF 1.75X9.00 FABED FILLER,FABED FINGER DOUBLER FOR BACK, FAB DOUBLER FOR EXTERN
- [SDR 872SJ002](https://openairdocs.org/sdr/872SJ002.md): Skin · corroded · Oct 21, 2004 · N872SJ · Doug DC871F · Fuselage Main, Plate/Skin
  > A/C COMP AREA INTERIOR A/C OUTFLOW DUCT HAS CORROSION GBAMC NR 04160 CLEANED CORRISON ON INTERIOR A/C OUTFLOW DUCT PANEL IAW DC-8 SRM 51-1-8,CORRISON FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. MATERIAL THICKNESS.130,MATERIAL LOSS.104 FABED DOUBLER IAW COT
- [SDR FWT2001F00001](https://openairdocs.org/sdr/FWT2001F00001.md): Altimeter · erratic · Jan 11, 2001 · N872SJ · Doug DC871F · Altimeter, Barometric/Encoder
  > ON CLIMB OUT MIA AT 17,000 CAPT. ALTIMETER BECAME ERRACTIC AND STICKING AND GIVING ERRONEOUS READINGS, LOG BOOK, PAGE 201510. REMOVED AND REPLACED CAPT. ALTIMETER, ACCOMPLISHED PITOT STATIC SYSTEM LEAK CHECK AND OPS CHECK- FOUND NORMAL IAW MM. PITOT STATIC T
- [SDR FWT2001F00000](https://openairdocs.org/sdr/FWT2001F00000.md): Engine · failed · Oct 16, 2000 · N872SJ · Doug DC871F · Engine (Turbine/Turboprop)
  > ENGINE NR 4 SHUTDOWN DURING FLT. DUE TO LOSS OF OIL QUANITY AND PRESSURE. AFTER LANDING, MAINT FOUND TRANSFER GEARBOX MOTORING PAD COVER AND SPLINE-SHAFT IN COWLING, ALL CHIP DETECTORS INSPECTED AND FOUND TRANSFER GEARBOX SCAVENGE IN AND SUPPLY OIL FILTER AN
- [SDR FWT2001F00003](https://openairdocs.org/sdr/FWT2001F00003.md): Actuator · inoperative · Jul 12, 2000 · N872SJ · Doug DC871F · Trailing Edge Flap Actuator
  > WING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROL VALVE IAW
- [SDR FWT2001F00002](https://openairdocs.org/sdr/FWT2001F00002.md): Actuator · inoperative · Jul 12, 2000 · N872SJ · Doug DC871F · Trailing Edge Flap Actuator
  > WING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP, WHEN FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROL
- [SDR FWT2001F00004](https://openairdocs.org/sdr/FWT2001F00004.md): Indicator · faulty · May 16, 2000 · N872SJ · Doug DC871F · Engine EGT/TIT Indicating System
  > ON CLIMB OUT, NR 3 EGT STARTED TO RISE AND REACHED TEMP LIMIT. WITH POWER LEVER BACK EGT STAYED WITHIN LIMITS. WITH PMC OFF TEMP STARTED TO RISE. DUMPED FUEL IAW AIRCRAFT ABNORMAL PROCEDURES CHECK LIST. BORESCOPE NR 3 ENGINE HPC AND HPT IAW MM. PERFORMED
- [SDR SRAA971211](https://openairdocs.org/sdr/SRAA971211.md): Actuator · failed · Dec 16, 1997 · N872SJ · Doug DC871F · Trailing Edge Flap Actuator
  > ON ARRIVAL AT BRU FLIGHT NR 081, DURING ENGINE SHUTDOWN, HYDRAULIC QTY INDICATOR DROPPED TO 6 GAL. INSPECTED AIRCRAFT AND FOUND MID WING ACTUATOR ON LT FLAP SHEARED AND LEAKING AT CONNECTOR. REPLACED ACTUATOR, SYSTEM OPS CHECKED GOOD PER MM CH 27-00.
- [SDR SRAA971011](https://openairdocs.org/sdr/SRAA971011.md): Wire · broken · Oct 27, 1997 · N872SJ · Doug DC871F · Smoke Detection
  > DURING PREFLIGHT, NR 9 AND NR 10 SMOKE DETECTOR, WOULD NOT TEST. INSPECTED AND FOUND WIRE BROKEN DURING LOADING. NR 9 SMOKE DETECTOR REPAIRED, OPS CHECK GOOD IAW DC8 MM CH 26.
- [SDR SRAA970610](https://openairdocs.org/sdr/SRAA970610.md): Fire Loops · malfunctioned · Jun 15, 1997 · N872SJ · Doug DC871F · Fire Detection
  > ON DESCENT, NR 1 ENGINE SHORT CIRCUIT LIGHT FLICKERED ON. REMOVED AND REPLACED ALL FIRE LOOPS ON NR 1 ENGINE. PERFORMED ENGINE RUN, OPS CHECKED GOOD IAW ATA CH 26.
- [SDR SRAA970608](https://openairdocs.org/sdr/SRAA970608.md): Fire Control · inoperative · Jun 14, 1997 · N872SJ · Doug DC871F · Fire Detection
  > DURING FLIGHT, NR 1 ENGINE FIRE LOOP SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. UPON TAXI IN FIRE WARNING ON NR 1 ENGINE CAME ON AND SHORT CIRCUIT LIGHT CAME ON STEADY. REMOVED AND REPLACED NR 1 FIRE WARNING CONTROL, SYSTEM OPS CHECKED GOOD PER MM CH 26-00.
- [SDR SRAA970605](https://openairdocs.org/sdr/SRAA970605.md): Connector · dirty · Jun 8, 1997 · N872SJ · Doug DC871F · Fire Detection
  > DURING FLIGHT, NR 1 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT FLICKERS ON AND OFF. VISUALLY OBSERVED NR 1 ENGINE, NO FIRE CONDITION EXISTS. AIRCRAFT CONTINUED TO DESTINATION WITHOUT INCIDENT. REMOVED AND CLEANED CANNON PLUG ON NR 1 FIRE CONTROL BOX, OPS CHECK
- [SDR SRAA970402](https://openairdocs.org/sdr/SRAA970402.md): Fire Detector · failed · Apr 2, 1997 · N872SJ · Doug DC871F · Fire Detection
  > DURING FLIGHT, NR 1 ENGINE FIRE SHORT CIRCUIT LIGHT, MASTER WARNING LIGHT AND FIRE HANDLE LIGHT ILLUMINATED INTERMITTENTLY, ALL OTHER INDICATIONS WERE NORMAL. OBSERVED NR 1 ENGINE AND FOUND NO ABNORMAL CONDITION EXISTS. AIRCRAFT LANDED WITHOUT INCIDENT. FOU
- [SDR SRAA970309](https://openairdocs.org/sdr/SRAA970309.md): Actuator Seal · deteriorated · Mar 27, 1997 · N872SJ · Doug DC871F · Trailing Edge Flap Control System
  > AFTER TAKEOFF FOR FLIGHT 128 OUT OF EKCH, DURING GEAR RETRACTION, AIRCRAFT HYDRAULIC QUANTITY INDICATED A RAPID FLUID LOSS. FOLLOWED EMERGENCY PROCEDURE AND SELECTED HYDRAULIC SYSTEM TO STAND BY RUDDER PUMP, AIRCRAFT LANDED SAFELY USING AUXILARY PUMP, INSPECT
- [SDR SRAA970303](https://openairdocs.org/sdr/SRAA970303.md): Fire Warn Light · illuminated · Mar 3, 1997 · N872SJ · Doug DC871F · Fire Detection
  > NR 1 ENGINE FIRE WARNING LIGHT CAME ON AFTER ENGINE SHUT-DOWN AT THE BLOCK, WITHIN 15 SECONDS FIRE LIGHT AND BELL WENT OFF, ENGINE SHORT CIRCUIT LIGHT ALSO CAME ON WITH FIRE WARNING WOULD NOT TEST WENT OFF. VISUALLY VERIFIED NR 1 ENGINE HAD NO FIRE, INSPECTED
- [SDR SRAA970302](https://openairdocs.org/sdr/SRAA970302.md): Switch · ice build-up · Mar 2, 1997 · N872SJ · Doug DC871F · Landing Gear Position and Warning
  > DURING FLIGHT 577 TO KEF, LEFT MAIN GEAR GREEN DOWN LIGHT NOT ON AND GEAR UNSAFE LIGHT ILLUMINATED, RECYCLED GEAR WITH SAME RESULT. PERFORMED CHECK PER QRH AND DETERMINED GEARS WERE DOWN AND LOCKED, AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED LT GEAR DOWNLOC
- [SDR SRAA961214](https://openairdocs.org/sdr/SRAA961214.md): Fire Loop · out of position · Dec 25, 1996 · N872SJ · Doug DC871F · Fire Detection
  > DURING DESCENT, FIRE BELL RANG ONCE AND NR 1 SHORT CIRCUIT TEST LIGHT FLICKERED ON BRIEFLY THEN STOPPED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND FIRE LOOP OUT OF POSITION, REPOSITIONED FIRE LOOP, PERFORMED FUNCTIONAL CHECK AND ENGINE R

Next page: https://openairdocs.org/aircraft/N872SJ/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 = 'N872SJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N872SJ/reports

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