# Service difficulty reports: N8970D

A list on [N8970D](https://openairdocs.org/aircraft/N8970D.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 · 94 reports

- [SDR REXA2022032400492](https://openairdocs.org/sdr/REXA2022032400492.md): Spar · deformed · Mar 10, 2022 · N8970D · Cndair CL6002B19 · Rudder, Spar/Rib
  > RUDDER LEADING EDGE HAS DAMAGE TO LIGHTING HOLE AT FRONT SPAR LOWER SECTION JC:55-320-519 EMP#:2006BRT REPAIRED RUDDER L/E LIGHTING HOLE @ FRONT SPAR IAW ENDEAVOR E.A. CRJ255-13042
- [SDR REXA2022032400491](https://openairdocs.org/sdr/REXA2022032400491.md): Anchor · corroded · Mar 10, 2022 · N8970D · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR COUNTER BALANCE CABLE ANCHOR ON FS349 SEPERATED ADJUSTMENT PLATE ON FRAME EXFO CORROSION J/C:53-900-500 EMP#:2003BB "REMOVED THE CORRODED PASSENGER DOOR AFT COUNTER BALANCE CABLE ANCHOR, SERATED PLATE & HARDWARE AND INSTALLED NEW AFT COUNT
- [SDR REXA2022032400493](https://openairdocs.org/sdr/REXA2022032400493.md): Spar · corroded · Mar 1, 2022 · N8970D · Cndair CL6002B19 · Vertical Stabilizer, Spar/Rib
  > MULTIPLE GOUGES NEAR FASTNER HOLES UNDER PANEL 324AT (V-STAB LEADING BLENDED OUT MULTIPLE GOUGES NEAR FASTENERS HOLES UNDER PANEL 324AT AT V-STAB LEADING EDGE IAW CRJ/200 SRM 51-12-00.FOUND TO BE WITHIN LIMITS IAW CRJ/200 SRM 55-31-07
- [SDR REXA2020070600593](https://openairdocs.org/sdr/REXA2020070600593.md): Light · inoperative · Jul 2, 2020 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > FWD CEILING EMERGECNY LIGHT OUT. REMOVED AND REPLACED FORWARD CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.
- [SDR REXA2020020580182](https://openairdocs.org/sdr/REXA2020020580182.md): Skin · chafed · Jan 28, 2020 · N8970D · Cndair CL6002B19 · Trailing Edge Flaps
  > LH INBD FLAP VANE CHAFED 1"L X.5"W JUST INBD OF ACCESS PANEL 584DT. REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10
- [SDR REXA2020020580176](https://openairdocs.org/sdr/REXA2020020580176.md): Skin · chafed · Jan 28, 2020 · N8970D · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBD FLAP VANE CHAFED 1"L X.5"W JUST OTBD OF ACCESS PANEL 684ET REMOVED AND REPLACED RH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10
- [SDR REXA2020020580169](https://openairdocs.org/sdr/REXA2020020580169.md): Vane · chafed · Jan 28, 2020 · N8970D · Cndair CL6002B19 · Trailing Edge Flaps
  > LH INBD FLAP VANE CHAFED 1""L X.5""W JUST OTBD OF ACCESS PANEL 584ET. REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10
- [SDR REXA2020020570181](https://openairdocs.org/sdr/REXA2020020570181.md): Floor Support · corroded · Jan 27, 2020 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR BEAM (CAP) BETWEEN FS 574 AND FS 621 AT LBL 27 IS CORRODED AT SEVERAL LOCATIONS REMOVED AND REPLACED BEAM (CAP) IAW CRJ 200 SRM 51-40-11, TR51-42, 51-42-21 AND 51-42-23
- [SDR REXA2020020570180](https://openairdocs.org/sdr/REXA2020020570180.md): Floor Support · corroded · Jan 27, 2020 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR BEAM (CAP) BETWEEN FS 574 AND FS 621 AT LBL 27 IS CORRODED AT SEVERAL LOCATIONS REMOVED AND REPLACED BEAM (CAP) IAW CRJ 200 SRM 51-40-11, TR51-42, 51-42-21 AND 51-42-22
- [SDR REXA2020020560168](https://openairdocs.org/sdr/REXA2020020560168.md): Skin · corroded · Jan 26, 2020 · N8970D · Cndair CL6002B19 · Wing, Plate/Skin
  > LH LOWER WING PLANK ACCESS HOLE AT 540BB IS CORRODED AT SEVERAL LOCATIONS BLEND REPAIRED WING PLANK ACCESS HOLE IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05.
- [SDR REXA2020020560167](https://openairdocs.org/sdr/REXA2020020560167.md): Skin · corroded · Jan 26, 2020 · N8970D · Cndair CL6002B19 · Wing, Plate/Skin
  > LH LOWER WING PLANK ACCESS HOLE AT 510AB IS CORRODED AT SEVERAL LOCATIONS BLEND REPAIRED WING PLANK ACCESS HOLE IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05.
- [SDR REXA2020020500177](https://openairdocs.org/sdr/REXA2020020500177.md): Bulkhead Web · cracked · Jan 25, 2020 · N8970D · Cndair CL6002B19 · Fuselage Main, Structure
  > FS202.75 BULKHEAD FWD SIDE @BL23.71 HAS MULTIPLE INDICATORS AROUND ENTIRE CIRCUMFERENCE OF THE PARKING BRAKE CABLE CUTOUT.15"" LONG BY 80% FSH. FAILED NDT INSPECTION COMPLIED WITH REMAINING STEPS OF REO 601R-53-11
- [SDR REXA2020020540175](https://openairdocs.org/sdr/REXA2020020540175.md): Seat Track · corroded · Jan 24, 2020 · N8970D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED AT 2 EA LOCATIONS BETWEEN F.S. 513 AND F.S. 544 REMOVED TAPE AND COMPLIED WITH REO 601R-53-00-055 DATED 2017-03-21 REV-C REMOVED AND INSTALLED IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802. WVAC EMP# 603145
- [SDR REXA2020020540174](https://openairdocs.org/sdr/REXA2020020540174.md): Skin · damaged · Jan 24, 2020 · N8970D · Cndair CL6002B19 · Trailing Edge Flaps
  > ELONGATED RIVET HOLE FOUND AT THE INBOARD LEADING EDGE OF INBD FLAP VANE PANEL OUTBD OF ACCESS PANEL 584ET. REMOVED TAPE. REMOVED AND REPLACED DAMAGED BUTT STRAP P/N 601R14303-24 IAW CRJ 200 SRM 51-42-06 AND 51-41-02. WVAC STAMP EMP # 722 MTC
- [SDR REXA2020020530173](https://openairdocs.org/sdr/REXA2020020530173.md): Seat Track · corroded · Jan 23, 2020 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN F.S. 529 AND F.S. 559+16 AT SEVERAL LOCATIONS. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802/400-802 AND GREO 601R-53-00-055 REV C. WVAC STAMP EMP# 717 MTC
- [SDR REXA2020020530172](https://openairdocs.org/sdr/REXA2020020530172.md): Seat Track · corroded · Jan 23, 2020 · N8970D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL CORRODED AT 3 EA LOCATIONS BETWEEN F.S. 559+32 AND F.S. 559+80. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK AT RBL 9 BETWEEN FS 559+80 AND FS 559+112 IAW CRJ 200 AMM 53-01-01-000-802/400-802 AND GREO 601R-53-00-485 REV D.
- [SDR REXA2020020520185](https://openairdocs.org/sdr/REXA2020020520185.md): Bulkhead Web · chafed · Jan 22, 2020 · N8970D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD SIDE OF REAR PRESSURE BULKHEAD HAS A CREW CHAFE ON AN EXISTING REPAIR AT RBL 36 REPAIRED CHAFFED AREA ON FWD SIDE OF FS 621 BULKHEAD BY REMOVING AND REPLACING CHAFFED TRIPLER IAW BOMBARDIER REO 601R-53-61-7280 REV-- DATED 2020-01-18. TRIPLER FABRICATED F
- [SDR REXA2020020520183](https://openairdocs.org/sdr/REXA2020020520183.md): Seat Track · corroded · Jan 22, 2020 · N8970D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR SEAT TRACK AT F.S. 559+112 LBL 9 IS CORRODED REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK AT FS 559+112 LBL 9 CRJ 200 AMM 53-01-11-000-802/400-802 AND GREO 601R-53-00-485 REV D. WVAC STAMP EMP# 717 MTC
- [SDR REXA2020020520171](https://openairdocs.org/sdr/REXA2020020520171.md): Seat Track · corroded · Jan 22, 2020 · N8970D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR SEAT TRACK AT FS 559+80 RBL 27 IS CORRODED REMOVED AND REPLACED CARGO FLOOR SEAT TRACK P/N 601R38779-9 AT FS 559+80 & RBL 27 IAW CRJ 200 AMM 53-01-11-400-802. REMOVED TAPE. WVAC STAMP EMP# 711 MTC
- [SDR REXA2020020500178](https://openairdocs.org/sdr/REXA2020020500178.md): Bulkhead Web · cracked · Jan 20, 2020 · N8970D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RIGHT AILERON LEADING EDFGE ACCESS PANEL 699CB HAS 2 AREAS WITH CHAFE DAMAGE, WORST AREA MEASURES APPROX 1" X..25" X 0.008" DEEP REPAIRED 699CB IAW CRJ 200 SRM 57-60-00, TR51-44 AND 51-25-01. WVAC STAMP EMP# 771 MTC
- [SDR REXA2020020580184](https://openairdocs.org/sdr/REXA2020020580184.md): Bulkhead Web · chafed · Jan 18, 2020 · N8970D · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD SIDE OF REAR PRESSURE BULKHEAD HAS 10 SCREW CHAFES ON WEB BETWEEN RBL 27 TO LBL 27 AND WL 73.0 TO WL 137 REPAIRED CHAFFED AREAS ON FS 621 BULKHEAD BETWEEN RBL 27 & LBL 27 WL 73.0 TO WL 137 IAW BOMBARDIER REO'S 601R-53-61-1285 REV-E, DATED: 2016-10-31 & 6
- [SDR REXA2018082900765](https://openairdocs.org/sdr/REXA2018082900765.md): Oxygen Mask · leaking · Aug 29, 2018 · N8970D · Cndair CL6002B19 · Crew Oxygen System
  > FO OXYGEN MASK LEAKING AIR DISCOVERED ENROUTE. PERFORMED DETAILED INSPECTION OF THE CREW O2 FO SIDE MASK AS PER AMM 35-11-12. NO LEAK NOTED AT THIS TIME. A/C GOOD FOR SERVICE.
- [SDR REXA2018061100483](https://openairdocs.org/sdr/REXA2018061100483.md): Connector · disconnected · Jun 11, 2018 · N8970D · Cndair CL6002B19 · Light System Wiring
  > KNEE LEVEL EMERGENCY EXIT SIGN IN GALLEY BY SERVICE DOOR DOESN’T LIGHT UP AT ALL. RECONNECTED CONNECTOR PERFORMED OPS CHECK IAW AMM 33-51-00 OPS CHECK GOOD.
- [SDR REXA2018060610447](https://openairdocs.org/sdr/REXA2018060610447.md): Light · broken · Jun 1, 2018 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE THE SERVICE DOOR HAD THE BASE & LENS BROKE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-13-400-801. OPS TESTED GOOD IAW AMM 33-51-00-710-801.
- [SDR REXA2018060621453](https://openairdocs.org/sdr/REXA2018060621453.md): Bracket · cracked · May 21, 2018 · N8970D · Cndair CL6002B19 · Wing Miscellaneous Structure
  > SINGLE POINT REFUEL FILL NECK SUPPORT BRACKET WAS CRACKED. REMOVED & REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06, AND SRM 51-41-02.
- [SDR REXA2018060650448](https://openairdocs.org/sdr/REXA2018060650448.md): Stiffener · cracked · May 20, 2018 · N8970D · Cndair CL6002B19 · APU Cowling/Containment
  > INSIDE APU ENCLOSURE FORWARD LT STIFFENER WAS CRACKED AT TOP. FABRICATED AND INSTALLED DOUBLER OF WELD CRACKS IAW EA CRJ249-07093.
- [SDR REXA2018060618454](https://openairdocs.org/sdr/REXA2018060618454.md): Angle · cracked · May 18, 2018 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE FROM BS 621 TO 625, BS 621 BULKHEAD AFT FACE STGR 15L IS CRACKED. REMOVED THE ANGLE, FABRICATED, AND INSTALLED THE NEW ANGLE IAW SRM 51-42-21, SRM 51-40-11, AND SRM 51-24-36.
- [SDR REXA2018060618452](https://openairdocs.org/sdr/REXA2018060618452.md): Bracket · cracked · May 18, 2018 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > HYD PRESSURE TRANSDUCER MOUNTING BRACKET WAS CRACKED IN THE RT MLG WHEEL WELL, ON THE PRESSURE FLOOR LOWER SURFACE. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06.
- [SDR REXA2018051700455](https://openairdocs.org/sdr/REXA2018051700455.md): Stiffener · cracked · May 17, 2018 · N8970D · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LEFT ENGINE EXHAUST FAIRING, CIRCUMFERENTIAL STIFFNER WAS CHAFED AND CRACKED AT THE FIVE O`CLOCK POSITION. REPAIRED THE STIFFNER IAW CMM 78-11-00-306-810-A01.
- [SDR REXA2018060600451](https://openairdocs.org/sdr/REXA2018060600451.md): Skin · corroded · May 15, 2018 · N8970D · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING FUEL STORAGE ACCESS PANEL LANDING, AT WS 640BB HAD FRETTING CORROSION. REMOVED THE CORROSION AND RESTORED FINISH IAW REO 601R-57-21-030, REV L.
- [SDR REXA2018060650450](https://openairdocs.org/sdr/REXA2018060650450.md): Skin · corroded · May 15, 2018 · N8970D · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING FUEL STORAGE ACCESS PANEL LANDING AT WS 540BB HAD FRETTING CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW REO 601R-57-21-030.
- [SDR REXA2018060650446](https://openairdocs.org/sdr/REXA2018060650446.md): Oxygen Mask · no test · May 15, 2018 · N8970D · Cndair CL6002B19 · Passenger Oxygen System
  > OXYGEN MASKS FAILED TO DEPLOY. REMOVED & REPLACED THE F/A OXYGEN MASK LATCH ASSY IAW AMM 32-21-05. OPS CHECKED GOOD.
- [SDR REXA2018060650461](https://openairdocs.org/sdr/REXA2018060650461.md): Drag Angle · cracked · May 14, 2018 · N8970D · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING INBD DRAG ANGLE SUPPORT STRUCTURE WAS CRACKED AT WS 48, LT MLG WW AREA. CUT OUT THE DAMAGE IAW REO 601R-57-51-046, REV B, REPAIR 2, & INSTALLED IAW REO 601R-57-51-046, REV B, REPAIR 2.
- [SDR REXA2018060614457](https://openairdocs.org/sdr/REXA2018060614457.md): Riser · cracked · May 14, 2018 · N8970D · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER CRACKED IN RADIUS SECOND STEP FROM THE BOTTOM. REMOVED THE CRACK. FOUND WITHIN LIMITS. IAW SRM 53-00-00.
- [SDR REXA2018060614456](https://openairdocs.org/sdr/REXA2018060614456.md): Panel · cracked · May 14, 2018 · N8970D · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER IS CRACKED AT THE LOWER STEP CORNER. REMOVED THE CRACK.
- [SDR REXA2018060630459](https://openairdocs.org/sdr/REXA2018060630459.md): Hinge · cracked · May 13, 2018 · N8970D · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SILL FLAP CENTER HING EHAS SEVERAL CRACKED AND CORRODED LUGS. REMOVED AND REPLACED THE HINGE IAW SRM 51-42-06.
- [SDR REXA2018060630458](https://openairdocs.org/sdr/REXA2018060630458.md): Hinge · cracked · May 13, 2018 · N8970D · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SILL FLAP HINGE WAS FOUND CRACKED. REMOVED AND REPLACED THE HINGE IAW SRM 51-42-06.
- [SDR REXA2018060650462](https://openairdocs.org/sdr/REXA2018060650462.md): Angle · cracked · May 12, 2018 · N8970D · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE ANGLE ON THE FWD SIDE OF THE BS 280 FLOORBEAM WAS CRACKED JUST INBD OF LBL 12, IN THE VERY FWD E & E BAY. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND SRM 51-42-21.
- [SDR REXA2018051200460](https://openairdocs.org/sdr/REXA2018051200460.md): Angle · cracked · May 12, 2018 · N8970D · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AT BS 280, STRINGER 3, THE ANGLES INBD AND OTBD WERE CRACKED, TWO PLACES. REMOVED AND REPLACED THE ANGLES IAW SRM 51-42-06.
- [SDR REXA2018030300173](https://openairdocs.org/sdr/REXA2018030300173.md): Light · inoperative · Mar 3, 2018 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > LEFT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED& REPLACED THE LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2018021100130](https://openairdocs.org/sdr/REXA2018021100130.md): Battery Pack · inoperative · Feb 11, 2018 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > DURING LINE CHECK, THE EXTERIOR AND INTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE. R & R THE BATTERY PACK AT PS3LF IAW 33-900-701, OPS CHECKED GOOD.
- [SDR REXA2018020700099](https://openairdocs.org/sdr/REXA2018020700099.md): Battery Pack · inoperative · Feb 7, 2018 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED AND CHARGED THE BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR REXA2017072700819](https://openairdocs.org/sdr/REXA2017072700819.md): Battery Pack · inoperative · Jul 27, 2017 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > OUTSIDE EMERGENCY LIGHTS BY PAX DOOR AND SERVICE DOOR FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION PS1LF IAW CARD 33-900-701, OPS CHECKED GOOD.
- [SDR REXA2016122702500](https://openairdocs.org/sdr/REXA2016122702500.md): Bpsu · inoperative · Dec 27, 2016 · N8970D · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAP FAIL MESSAGE AT 20 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00 REV 51 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I),. FOUND EVIDENCE OF MOISTURE INGRESS AND MODERATE CORROSION ON BPSU ELECTRICAL CONNECTOR. THIS, IN COMBINATION WITH LRU "MO
- [SDR REXA2016083101669](https://openairdocs.org/sdr/REXA2016083101669.md): Battery Pack · inoperative · Aug 31, 2016 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS CAME ON BRIEFLY. THEN WENT OUT. REMOVED AND REPLACED ALL FOUR BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD IAW AMM 33-51-04.
- [SDR REXA2016032700442](https://openairdocs.org/sdr/REXA2016032700442.md): Flashlight · inoperative · Mar 27, 2016 · N8970D · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL 25-61-04 ACT C PLACARD INSTALLED & TRANSFERRED TO MMO2. REPLACED FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MMO2 UPDATED & PLACARD REMOVED. THIS CLEARS MEL CON
- [SDR REXA2016022700333](https://openairdocs.org/sdr/REXA2016022700333.md): Light · worn · Feb 27, 2016 · N8970D · Cndair CL6002B19 · Emergency Lighting
  > ALL CABIN PATH LIGHTING STAINED & WORN. DISCARDED & REPLACED ALL CABIN PATH LIGHTING IAW AMM 33-51-01-960-801 STEP 3A & 33-51-01-400-806 STEP 3A2. FOUND ON PANEL RACK. INSTALL TO BE COMPLIED WITH ON NR SN 4459697 1012648 2000-0088.
- [SDR REXA2016022600332](https://openairdocs.org/sdr/REXA2016022600332.md): Door Sill · corroded · Feb 26, 2016 · N8970D · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR OPENING, LOWER FRAME LONGERON, LOWER ANGLE HAS CORROSION, BETWEEN FS 310 & 349, IN CABIN. R & R PAX DOOR OPENING, LOWER SILL ASSEMBLY, BETWEEN FS 310 & 349 IAW SRM 51-42-21 & SRM 51-42-20.
- [SDR REXA2016022000331](https://openairdocs.org/sdr/REXA2016022000331.md): Web · cracked · Feb 20, 2016 · N8970D · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR UPPER WEB AFT CORNER IS CRACKED. FABRICATED, R & R REPAIR ANGLE & FILLER ON UPPER AFT WEB CORNER ON PAX DOOR IAW REO 601R-52-11-279.
- [SDR REXA2016022000330](https://openairdocs.org/sdr/REXA2016022000330.md): Seat Track · corroded · Feb 20, 2016 · N8970D · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT AISLE SEAT TRACK STICK 2 HAS CORROSION IN CABIN. R & R NEW RT AISLE SEAT TRACK STICK 2 IAW AMM 53-01-11 SUBTASK 53-01-11-420-001.

Next page: https://openairdocs.org/aircraft/N8970D/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 = 'N8970D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8970D/reports

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