# Service difficulty reports: N8891A

A list on [N8891A](https://openairdocs.org/aircraft/N8891A.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 · 75 reports

- [SDR REXA2020091600645](https://openairdocs.org/sdr/REXA2020091600645.md): Bulkhead Web · chafed · Sep 3, 2020 · N8891A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND CHAFES IN RPB FORWARD FACE AT LBL 36.20, LBL 18.00, RBL 18.00, RBL 27.50 AND RBL 36.20 AT WL 105. CHAFES ARE 0.200"L X 0.200"W X 0.003" DEEP. REPAIRED CHAFES ON LBL 36.2, LBL 18, RBL 18, RBL 27.50 & RBL 36.20, IAW REO 601R-53-61-2155 REV A & REO 601R-
- [SDR REXA2020091600644](https://openairdocs.org/sdr/REXA2020091600644.md): Bulkhead Web · cracked · Sep 3, 2020 · N8891A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CONTINUATION FROM JOB 8789185 OP 39. FOUND RPB HAS 2 LOCATIONS WITH MULTIPLE INDICATIONS NOTED. AT LBL 9 WL 120 2:L 80% FSH AND AT RBL 27.50 WL 136.5 2.5"L 90% FSH BOTH AREAS FAILED NDT INSPECTION. REPAIRED RPB INDICATIONS AT LB 9 WL 120 & RBL 27.50 WL 136.
- [SDR REXA2020091600643](https://openairdocs.org/sdr/REXA2020091600643.md): Intercostal · cracked · Aug 24, 2020 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS APPROX 1" LONG. REPLACED INTERCOSTAL, IAW CRJ 200 SRM 51-42-21.
- [SDR REXA2020072000602](https://openairdocs.org/sdr/REXA2020072000602.md): Battery Pack · inoperative · Jul 18, 2020 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > AFT EMERGENCY AXLE LIGHT STRIP AND AFT EMERGENCY EXTERIROR LIGHTS WILL NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACK PS4LF IAW CRJ 200 JOBCARD 33-900-701 P/N OFF: AD-2013-1A S/N OFF: 67985 P/N ON; 2013-1ASMI S/N ON: 12507. OPS CHECK GOOD.
- [SDR REXA2020032500363](https://openairdocs.org/sdr/REXA2020032500363.md): Wire · broken · Mar 24, 2020 · N8891A · Cndair CL6002B19 · Light System Wiring
  > FOUND EMERGENCY EXIT LIGHTS AT SERVICE DOOR (DS11LY), PAX DOOR (DS10LY), AND FLOOR TRACK LIGHTING LAMP 1 (DS12LY) INOPS WHILE T/S FOUND BROKEN WIRE AT FLOOR PROXIMITY EXIT SIGN PASSENGER DOOR (DS10LY), REPAIRED BROKEN WIRE IAW ESPM 20-17-10. ALSO FOUND FLOOR
- [SDR REXA2019061060814](https://openairdocs.org/sdr/REXA2019061060814.md): Light · inoperative · Jun 6, 2019 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > DURING LINE CHECK FOUNS SECTIONS OF EMERGENCY FLOOR LIGHTS PHOTOLUMINESCENT ELEMENT NOT ON. REPLACED 2 SECTIONS OF FLOOR EMERGENCY LIGHT STRIPS IAW CRJ200 AMM 33-51-01. CHECKS NORMAL.
- [SDR REXA2019042640519](https://openairdocs.org/sdr/REXA2019042640519.md): Battery Pack · inoperative · Apr 24, 2019 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > DURING WALK AROUND FOUND FWD EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT PS1LF AND PS2LF IAW AMM 33-51-04. OPS CHECK IS GOOD.
- [SDR 2019F00177](https://openairdocs.org/sdr/2019F00177.md): Frame · cracked · Mar 30, 2019 · N8891A · Cndair CL6002B19 · Fuselage Main, Frame
  > INSPECTION TASK 000-53-230-603 FOUND CRACK. EA CRJ253-06839 PROVIDES REPAIR INSTRUCTIONS FOR FRAME AT FS333.00 FOUND CRACKED AT A TOOLING HOLE JUST BELOW S-1L. THE CRACK EMANATES UP FROM A PRODUCTION TOOLING HOLE ORIGINALLY MEASURING 0.250” IN DIAMETER. THE FR
- [SDR REXA201812311357](https://openairdocs.org/sdr/REXA201812311357.md): Wire · disconnected · Dec 28, 2018 · N8891A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT STRIP ON FLOOR AFT OF EMERGENCY EXIT INOP RECONNECTED EMERGENCY LIGHT STRIP ON FLOOR BY LAVORTY IAW CRJ 200 AMM 33-51-01 OPS CHECK GOOD AT THIS TIME
- [SDR REXA201812311356](https://openairdocs.org/sdr/REXA201812311356.md): Light · malfunctioned · Dec 27, 2018 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT COME ON WHEN EITHER SWITCH IS PLACED ON. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR REXA2018062100534](https://openairdocs.org/sdr/REXA2018062100534.md): Light · inoperative · Jun 21, 2018 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT TRACK INOP. REMOVED AND REPLACED LIGHT ON EMERGENCY TRACK IAW AMM 33-51-01. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2017101101084](https://openairdocs.org/sdr/REXA2017101101084.md): Switch · dirty · Oct 11, 2017 · N8891A · Cndair CL6002B19 · Interphone/Passenger Announcement (PA) System
  > EMERGENCY BUTTON LIGHT ON THE PA PANEL FOUND INOPERATIVE. CLEANED EMERGENCY SWITCH AND RESEATED. PERFORMED AN OPS TEST OF INTERPHONE CONTROL UNIT, ALL CHECKED OK IAW CMM 23-30-07, AND AMM 23-31-07.
- [SDR REXA2017100901068](https://openairdocs.org/sdr/REXA2017100901068.md): Placard · missing · Oct 9, 2017 · N8891A · Cndair CL6002B19 · Placards and Markings
  > OVERWING EMERGENCY EXITS DOOR PLACARDS MISSING. INSTALLED DOOR WEIGHT PLACARDS.
- [SDR REXA2017093001040](https://openairdocs.org/sdr/REXA2017093001040.md): Bulb · inoperative · Sep 30, 2017 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT IS OUT ON LEFT SIDE. R & R THE BULB, OPS CHECKED GOOD IAW AMM 33-51-21.
- [SDR REXA2017072000800](https://openairdocs.org/sdr/REXA2017072000800.md): Cap · cracked · Jul 20, 2017 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT MLG WHEEL WELL UPPER CAP FOUND CRACKED, JUST OTBD OF WHEEL WELL OPENING AT BS 549.7, WS 48. PERFORMED TEMPORARY REPAIR ON THE RT BATT RIB CAP AT WS 48.30 IAW REO 601R57-51-781.
- [SDR REXA2017050900578](https://openairdocs.org/sdr/REXA2017050900578.md): Oxygen Mask · inoperative · May 9, 2017 · N8891A · Cndair CL6002B19 · Crew Oxygen System
  > OBSERVERS O2 MASK MICROPHONE INOPERATIVE. REMOVED AND REPLACED OBSERVERS O2 MASK P/N ON/OFF MC10-35-101 S/N OFF 107480I S/N ON 96368I IAW AMM 35-11-12. OPS/LEAK CHECK GOOD.
- [SDR REXA2016122802501](https://openairdocs.org/sdr/REXA2016122802501.md): Flashlight Assy · inoperative · Dec 28, 2016 · N8891A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT AND HOLDER IAW AMM 25-61-00. OPS TESTED GOOD.
- [SDR REXA2016091901819](https://openairdocs.org/sdr/REXA2016091901819.md): Bpsu · inoperative · Sep 19, 2016 · N8891A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL DURING CRUISE (FL 240), PERFORMED TROUBLESHOOTING IAW FIM REV 51 IAW AD2009-06-12 PARAGRAPH (H)(6)(I). REPLACED THE FECU IAW AMM 27-51-05. MEG CHECKED WIRING FROM CONNECTION 2P2CE & FLAP CONTROL UNIT, CHECKED GOOD. SWAPPED LT BPSU TO RT POSITION A
- [SDR REXA2016061001013](https://openairdocs.org/sdr/REXA2016061001013.md): Guard · displaced · Jun 10, 2016 · N8891A · Cndair CL6002B19 · Nose/Tail Landing Gear
  > GEAR DISAGREE AND NOSE DOOR WARNING MESSAGE UPON ROTATION. RAN QRM AND DID AIR RETURN. FOUND TOW GUARD DISLOCATED AND BRACKET SUB ASSY & WIRING HARNESS DAMAGED. RELOCATED TOWGUARD TO CORRECT POSITION AND R & R BRACKET AND WIRING HARNESS IAW AMM 32-21-01 AND
- [SDR REXA2016060100970](https://openairdocs.org/sdr/REXA2016060100970.md): Housing · cracked · Jun 1, 2016 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTS HAVE TWO CRACKED LAMP HOUSING TRACK TOPS. REMOVED CRACKED EMER LAMP HOUSING TRACK TOP & INSTALLED NEW LAMP HOUSING TRACK TOP IAW AMM 33-51-01-400-801 STEP 3A5-7. NO DEFECTS NOTED.
- [SDR REXA2016060100966](https://openairdocs.org/sdr/REXA2016060100966.md): Battery Pack · inoperative · Jun 1, 2016 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT FLOOR LEVEL AT SERVICE DOOR & BOTH FWD EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-05-400-801. R & R NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04-400-801. APPLICABLE OPERATIONS CH
- [SDR REXA2016060100962](https://openairdocs.org/sdr/REXA2016060100962.md): Panel · gouged · Jun 1, 2016 · N8891A · Cndair CL6002B19 · Wing Main, Frame Structure
  > PANEL 592BB HAS A GOUGE IN IT, NEEDS FURTHER INVESTIGATION. REMOVED GOUGED PLATE GUIDE FROM PANEL 592BB & INSTALLED NEW SERVICEABLE PLATE GUIDE IAW SRM 51-40-06, 51-40-11 & 51-42-06.
- [SDR REXA2016053000969](https://openairdocs.org/sdr/REXA2016053000969.md): Post · cracked · May 30, 2016 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128, RBL 18, OTBD VERTICAL POST HAS AN INDICATION IN THE AFT FLANGE RADIUS AT WL 69,.250" L BY 55% FSH & INBD VERTICAL POST HAS AN INDICATION IN THE AFT FLANGE RADIUS AT WL 62,.260" L BY 68% FSH. FAILED NDT INSPECTION. FABRICATED STIFFENER & INSTA
- [SDR REXA2016053000967](https://openairdocs.org/sdr/REXA2016053000967.md): Post · cracked · May 30, 2016 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128, BL 0, RT VERTICAL POST HAS AN INDICATION IN THE AFT FLANGE RADIUS AT WL 69,.250" L BY 80% FSH & LT POST HAS AN INDICATION IN THE AFT FLANGE RADIUS AT WL 69,.252" L BY 80% FSH. FAILED NDT INSPECTION. R & R BS 409+128 BL 0 POST ASSEMBLY IAW SRM 5
- [SDR REXA2016051800968](https://openairdocs.org/sdr/REXA2016051800968.md): Post · cracked · May 18, 2016 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128, LBL 18, OTBD VERTICAL POST HAS AN INDICATION IN THE AFT FLANGE RADIUS AT WL 69, 0.250" L BY 50% FSH & INBD VERTICAL POST HAS AN INDICATION 0.247" L BY 51% FSH IN THE AFT FLANGE RADIUS AT WL 69. FAILED NDT INSPECTION. R & R BS 409+128, LBL 18, INB
- [SDR REXA2016051800964](https://openairdocs.org/sdr/REXA2016051800964.md): Fitting · cracked · May 18, 2016 · N8891A · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT FITTING ON PILOT SIDE WINDOW POST LOWER END IS CRACKED. REMOVED TAPE. AFT FITTING ON PILOT SIDE WINDOW POST LOWER END R & R IAW SRM 51-42-21. PART 601R33235-3.
- [SDR REXA2016051800963](https://openairdocs.org/sdr/REXA2016051800963.md): Stringer Clip · cracked · May 18, 2016 · N8891A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER 3L CLIP IS CRACKED AT FS 280. REMOVED, LOCATED & DRILLED FASTENER HOLES & INSTALLED STRINGER CLIP AT FS 280 IAW SRM 51-40-06, 51-40-11, 51-42-06 & 51-42-21.
- [SDR REXA2016051600965](https://openairdocs.org/sdr/REXA2016051600965.md): Door Sill · corroded · May 16, 2016 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL IS CORRODED AT FWD FITTING. R & R SERVICE DOOR LOWER SILL 601R38303-253 IAW SRM 51-42-06, 51-42-13, 51-42-21 & 51-42-34.
- [SDR REXA2016022400259](https://openairdocs.org/sdr/REXA2016022400259.md): Flashlight · inoperative · Feb 24, 2016 · N8891A · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT IN CABINET DOES NOT HAVE DASHING RED LIGHT. DEFER FLIGHT ATTENDANTS FLASHLIGHT IAW MEL 25-61-04. PLACARD INSTALLED. REPLACED FLIGHT ATTENDANTS FLASHLIGHT IAW AMM 25-61-04. THIS CLEARS MEL 25-61-04, CONTROL 3262060-1. OPERATIONS
- [SDR REXA2016020200126](https://openairdocs.org/sdr/REXA2016020200126.md): Battery · discharged · Feb 2, 2016 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > ALL CABIN EMER LIGHTS WILL NOT TEST ON. CLEANED EMER LIGHT PANEL, CHARGED EMER LIGHT BATTERY IAW AMM 33-24-10 + 33-51=00. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR REXA2015111001059](https://openairdocs.org/sdr/REXA2015111001059.md): Light · damaged · Nov 10, 2015 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > ON PREFLIGHT BOTH FIRST OFFICERS & KICKOFF MECHANIC FOUND EMER OVERWING EXIT LIGHT ON RT SIDE TO BE MISSING. FOUND TO BE DAMAGED NOT MISSING. R & R LENS IAW AMM 33-51-21. OK FOR SERVICE.
- [SDR REXA2015110101007](https://openairdocs.org/sdr/REXA2015110101007.md): Wire · separated · Nov 1, 2015 · N8891A · Cndair CL6002B19 · Fire Protection System Wiring
  > FOUND WIRE SEPARATED FROM TERMINAL LUG AT LT WHEEL BIN FIRE DETECTION SYS. SECURED WIRE J5WL TO TERMINAL LUG & TERMINAL LUG TO GND IAW 26-14-04. OPERATIONS CHECKED MAIN WHEEL BINS FIRE DETECTION SYS IAW ESPM 26-20-00. OPERATIONS CHECKED GOOD. ACFT OK FOR S
- [SDR REXA2015062100611](https://openairdocs.org/sdr/REXA2015062100611.md): Life Vest · wrong part · Jun 21, 2015 · N8891A · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT LIFE VEST WRONG TYPE, NEEDS CREW VEST PN P0723E105PWC. R & R FLIGHT ATTENDANT LIFE VEST IAW AMM 25-60-00.
- [SDR REXA2015021000195](https://openairdocs.org/sdr/REXA2015021000195.md): Seal · broken · Feb 10, 2015 · N8891A · Cndair CL6002B19 · Emergency Equipment
  > AFT PBE SEAL IS BROKEN. REPLACED AFT PBE SEAL IAW AMM 25-60-00.
- [SDR REXA2014103001086](https://openairdocs.org/sdr/REXA2014103001086.md): Smoke Goggles · missing · Oct 30, 2014 · N8891A · Cndair CL6002B19 · Emergency Equipment
  > OBSERVER SEAT MISSING SMOKE GOGGLES. INSTALLED NEW SMOKE GOGGLES IAW AMM 25-60-00. NO DEFECTS NOTED, OK FOR SERVICE.
- [SDR REXA2014101701064](https://openairdocs.org/sdr/REXA2014101701064.md): Door Seal · obstructed · Oct 17, 2014 · N8891A · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT ATTENDANT REPORTS LOUD SQUEAL FROM PAX CABIN DOOR. WHEN CALL WAS MADE TO FLIGHT DECK ACFT ALT 24000 & CLIMBING TO FL 30000 CABIN DIFF 7.1 PSI CABIN PRESSURE DIFF CHECKED NORMAL IN ALL PHASES OF FLIGHT. CLEANED DEBRIS FROM DOOR SEAL & PERFORMED VISUAL
- [SDR REXA2014063000641](https://openairdocs.org/sdr/REXA2014063000641.md): Cover · cracked · Jun 30, 2014 · N8891A · Cndair CL6002B19 · Emergency Lighting
  > PASSENGER CABIN EMER FLOOR TRACK LIGHTING COVER IS CRACKED IN SEVERAL PLACES & END CAPS ARE MISSING. R & R PAX CABIN EMER FLOOR TRACK LIGHT COVER & INSTALLED TWO SERVICEABLE END CAPS AT EACH END OF PAX CABIN EMER FLOOR TRACK IAW AMM 33-51-01.
- [SDR REXA2014070100493](https://openairdocs.org/sdr/REXA2014070100493.md): Aileron · chafed · Jun 27, 2014 · N8891A · Cndair CL6002B19 · Ailerons
  > LEFT HAND AILERON CHAFED. REPAIRED IAW SRM 57-60-00 & 51-40-11/51-42-06.
- [SDR REXA2014070100492](https://openairdocs.org/sdr/REXA2014070100492.md): Skin · corroded · Jun 27, 2014 · N8891A · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 510AB & 540BB PITTED & CORRODED. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014062700490](https://openairdocs.org/sdr/REXA2014062700490.md): Skin · corroded · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK AT LANDING FOR PANEL 650BB FOUND CORRODED MEASURING 0.008 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014062700489](https://openairdocs.org/sdr/REXA2014062700489.md): Skin · corroded · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION FOUND ON RT WING PLANK AT LANDING FOR PANEL 650DB MEASURING 0.013 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014062700488](https://openairdocs.org/sdr/REXA2014062700488.md): Skin · corroded · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION FOUND ON RT WING PLANK PANEL LANDING FOR PANEL 650FB MEASURING 0.009 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014062700487](https://openairdocs.org/sdr/REXA2014062700487.md): Skin · corroded · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION FOUND ON RT WING PLANK LANDING FOR PANEL 640BB, 0.024 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.
- [SDR REXA2014062600486](https://openairdocs.org/sdr/REXA2014062600486.md): Fitting · cracked · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 280, LBL 9 CRACKED OTBD AFT. REPAIRED IAW REO 601R-53-11-136.
- [SDR REXA2014062600485](https://openairdocs.org/sdr/REXA2014062600485.md): Fitting · unknown · Jun 23, 2014 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 280, RBL 9 OTBD AFT. REPAIRED IAW REO 601R-53-11-136.
- [SDR REXA2014061900484](https://openairdocs.org/sdr/REXA2014061900484.md): Fitting · cracked · Jun 18, 2014 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 280 LBL 9 CRACKED AFT OTBD. REPAIRED IAW REO 601R-53-11-136.
- [SDR REXA2014061900483](https://openairdocs.org/sdr/REXA2014061900483.md): Fitting · cracked · Jun 18, 2014 · N8891A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 280, RBL 9 CRACKED AFT OTBD. REPAIRED IAW REO 601R-53-11-136.
- [SDR REXA2014061800048](https://openairdocs.org/sdr/REXA2014061800048.md): Frame · corroded · Jun 18, 2014 · N8891A · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON THE LOWER FRAME SECTOR AT FS 605.00 BETWEEN STRINGER 24R & 24L. REPAIRED IAW EA CRJ253-02665.
- [SDR REXA2013092201748](https://openairdocs.org/sdr/REXA2013092201748.md): Smoke Goggles · broken · Sep 22, 2013 · N8891A · Cndair CL6002B19 · Emergency Equipment
  > COCKPIT SMOKE GOGGLE BROKEN. REPLACED SMOKE GOGGLES IAW AMM 25-61-00. OK FOR SERVICE.
- [SDR REXA2013072601385](https://openairdocs.org/sdr/REXA2013072601385.md): Track · missing · Jul 26, 2013 · N8891A · Cndair CL6002B19 · Passenger Compartment Equipment
  > TRACK MISSING IN FRONT OF LAVATORY. REPLACED IAW 25-20-00.

Next page: https://openairdocs.org/aircraft/N8891A/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 = 'N8891A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8891A/reports

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