# Service difficulty reports: N307PQ

A list on [N307PQ](https://openairdocs.org/aircraft/N307PQ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR REXA2025050800570](https://openairdocs.org/sdr/REXA2025050800570.md): Unknown · fumes · May 2, 2025 · N307PQ · Cndair CL6002D24 · Air Distribution System
  > FUMES STARTING FROM ROW 14 ALL THE WAY INTO AFT LAV AND FUMES IN THE FLIGHT DECK INFLIGHT. NO VISIBLE SMOKE. STARTED IN THE AFT DURING ENGINE START. CAME INTO FLIGHT DECK AT FL300. UNPLEASANT SWEET SMELL. SUBMITTED T/S TS#002736-R1 DATA SHEET FOR SMOKE/FUME E
- [SDR REXA2024102801084](https://openairdocs.org/sdr/REXA2024102801084.md): Lug · cracked · Mar 15, 2024 · N307PQ · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT DOOR UPPER AFT LUG IS CRACKED REPAIRED IAW ENDEAVOR AIR EA CRJ952-16094 REV IR
- [SDR REXA2024102801083](https://openairdocs.org/sdr/REXA2024102801083.md): Lug · cracked · Mar 15, 2024 · N307PQ · Cndair CL6002D24 · Emergency Exits
  > LH FWD EMERGENCY EXIT DOOR UPPER AFT LUG IS CRACKED REPAIRED IAW ENDEAVOR AIR EA CRJ952-16142 REV IR
- [SDR REXA2024102801082](https://openairdocs.org/sdr/REXA2024102801082.md): Lug · cracked · Mar 15, 2024 · N307PQ · Cndair CL6002D24 · Emergency Exits
  > RH AFT EMERGENCY EXIT DOOR UPPER AFT LUG IS CRACKED REPAIRED IAW ENDEAVOR AIR EA CRJ952-16143 REV IR
- [SDR REXA2024102801081](https://openairdocs.org/sdr/REXA2024102801081.md): Floorbeam · corroded · Mar 14, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FOUND R/H 280 FLOOR BEAM TO BE CORRODED BEYOND ALLOWABLE LIMITS, REQUIRES REPLACEMENT REMOVED AND INSTALLED NEW R/H 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2024102801079](https://openairdocs.org/sdr/REXA2024102801079.md): Bulkhead Web · corroded · Mar 6, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH FS280 WEB IS CORRODED REPAIRED F.S.280 LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01
- [SDR REXA2024102801078](https://openairdocs.org/sdr/REXA2024102801078.md): Floorbeam · cracked · Mar 6, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > WHILE CONDUCTING MAINTENANCE FOUND R/H FLOOR BEAM ON AFT SIDE FS 280 TO BE CRACKED ON BOTTOM RADIUS AND REQUIRES REPAIR REPAIRED RIGHT HAND FLOOR BEAM IAW MHIRJ REO# 690-53-11-1695 REV. -- DATED 2024-02-29
- [SDR REXA2024071600555](https://openairdocs.org/sdr/REXA2024071600555.md): Floorbeam · corroded · Mar 1, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FOUND L/H 280 FLOOR BEAM TO BE CORRODED BEYOND ALLOWABLE LIMITS, REQUIRES REPLACEMENT FOUND L/H 280 FLOOR BEAM TO BE CORRODED BEYOND ALLOWABLE LIMITS, REQUIRES REPLACEMENT REMOVED CORRODED UNSERVICEABLE L/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2024031500284](https://openairdocs.org/sdr/REXA2024031500284.md): Step · corroded · Mar 1, 2024 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > SERVICE DOOR STEP PLATE IS CORRODED ALONG THE INBOARD FWD EDGE UNDERSIDE REMOVED AND REPLACED SERVICE DOOR STEP PLATE (P/N SH670-31407-7)
- [SDR REXA2024071600554](https://openairdocs.org/sdr/REXA2024071600554.md): Post · corroded · Feb 29, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > RH DOOR POST AT FS 280 IS CORRODED BEYOND ALLOWABLE LIMITS AROUND FASTENERS AT FLOOR LEVEL. REQUIRES CRJ 900 SRM 53-11-10-201-006-A01 REPAIR. REPAIRED RH DOOR POST AT FS 280 IAW CRJ900 SRM REPAIR 53-11-10-201-006-A01.
- [SDR REXA2024031500283](https://openairdocs.org/sdr/REXA2024031500283.md): Hinge Fitting · corroded · Feb 29, 2024 · N307PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > UPON FURTHER INVESTIGATION WHILE CHANGE A/C SIDE OF NLG AFT DOOR PIN BUSHING FOUND HINGE FITTING ASSY ON LH AND RH SIDE OF A/C TO BE CORRODED AND REQUIRE REPLACEMENT. INSTALLED NEW LH AND RH FITTING, HINGE, NLG, AFT DOOR P/N: CC670-32212-7 IAW CRJ900 SRM 51-42
- [SDR REXA2024030700248](https://openairdocs.org/sdr/REXA2024030700248.md): Panel · chafed · Feb 29, 2024 · N307PQ · Cndair CL6002D24 · Wing Structure
  > PANEL 584AB IS CHAFED. REMOVED AND REPLACED PANEL.
- [SDR REXA2024071600552](https://openairdocs.org/sdr/REXA2024071600552.md): Post · corroded · Feb 27, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > LH FS280 LOWER DOOR POST REPAIR IS CORRODED WITH LOOSE FASTENERS. LH FS280 LOWER DOOR POST REPAIR IS CORRODED WITH LOOSE FASTENERS. REMOVED EXISTING REPAIR AT LH LOWER DOOR POST, IAW CRJ-900 SRM 51-42-13-001-001-A01. FABRICATED REPAIR PARTS IAW 53-11-10-201-00
- [SDR REXA2024071600550](https://openairdocs.org/sdr/REXA2024071600550.md): Web · corroded · Feb 26, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE FS 280 WEB CORRODED ABOVE FLOOR SILL. R/H F.S. 280 WEB FOUND TO BE CORRODED BEYOND LIMITS IAW CRJ-900 SRM 53-00-00-101-001-A01. REMOVED CORRODED WEB AND BUTT SPLICE, FABRICATED AND INSTALLED NEW SERVICEABLE R/H F.S. 280 WEB AND BUTT SPLICE IAW CRJ-900
- [SDR REXA2024071600549](https://openairdocs.org/sdr/REXA2024071600549.md): Floorbeam · corroded · Feb 26, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH SIDE 280 FLOOR SILL IS CORRODED. REPAIRED R/H F.S. 280 FLOOR SILL IAW CRJ-900 SRM 53-21-43-201-002-A01.
- [SDR REXA2024071600548](https://openairdocs.org/sdr/REXA2024071600548.md): Angle · corroded · Feb 26, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "280 BULKHEAD J-ANGLE HAS SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. 280 BULKHEAD J-ANGLE HAS SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. REMOVED STA 280 ""J"" ANGLE FOUND NO ALLOWABLE LIMITS IN SRM REQUIRES REPLACEMENT IAW CRJ900 SRM 51-42-06-001-001-A01 A
- [SDR REXA2024040100321](https://openairdocs.org/sdr/REXA2024040100321.md): Web · cracked · Feb 26, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FWD EQUIPMENT BAY FLOOR WEB IS CRACKED AT F.S.193. REPAIRED WEB IAW REPAIR TYPE 2 IAW CRJ900 SRM 53-11-43-201-001-A01
- [SDR REXA2024102801075](https://openairdocs.org/sdr/REXA2024102801075.md): Diaphragm · cracked · Feb 25, 2024 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H MLG WHEEL BIN DIAPHRAGM IS CRACKED. REMOVED L/H MLG WHEEL BIN DIAPHRAGM. INSTALLED NEW SERVICEABLE L/H MLG WHEEL BIN DIAPHRAGM P/N CC670-39205-7 IAW CRJ900 SRM 51-41-04-001-001-A01 AND 51-41-02-001-001-A01
- [SDR REXA2020102600729](https://openairdocs.org/sdr/REXA2020102600729.md): Angle · bent · Oct 4, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MOUNTING ANGLES FOR THE LIGHTNING DIVERTER PANELS AT FS 295-333 RIGHTSIDE ARE BENT AND MISSING ATTACHING RIVETS. REMOVED & REPLACED SUPPORT ANGLES (2) FS 295-349 RBL 27, IAW SRM 51-42-10-001-001-A01.
- [SDR REXA2020102600725](https://openairdocs.org/sdr/REXA2020102600725.md): Angle · corroded · Oct 3, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER MIDCAP ANGLE (FUSELAGE) IS CORRODED. INSTALLED NEW MID CAP ANGLE P/N SH670-31825-9, IAW SRM 51-42-11-001-001-A01 AND 51-42-02-001-001-A01 AND REINSTALLED GROUND, IAW AMM 51-80-00-910-804-A01.
- [SDR REXA2020102600720](https://openairdocs.org/sdr/REXA2020102600720.md): Panel · chafed · Oct 2, 2020 · N307PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > FLAP LEADING EDGE PANELS 584ET AND 584HT ARE CHAFED. REPAIRED 584ET, IAW SRM 51-25-01-001-001-A01. REPLACED 584ET LOCATED DRILLED, IAW SRM 51-400-11-001-001-A01. WVAC EMP #6027.
- [SDR REXA2020102600726](https://openairdocs.org/sdr/REXA2020102600726.md): Angle · corroded · Sep 30, 2020 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR KICKPLATE ANGLE IS CORRODED. REPAIRED CORROSION DAMAGE ON PAX DOOR KICK PLATE ANGLE P/N: SH670-31875-7S BY REMOVING AND REPLACING, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2020102600722](https://openairdocs.org/sdr/REXA2020102600722.md): Intercostal · corroded · Sep 30, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 2 INTERCOSTALS AND 2 ANGLES BETWEEN FS 349 AND FS 364, STGR 26L TO STGR 26R ARE CORRODED. TCI: 53-20-313. REMOVED AND REPLACED ANGLES AND INTERCOSTALS, IAW CRJ 900 SRM 51-42-06-001-001-A01. WVAC EMP STAMP 711 MTC. ADDITIONAL PARTS REPLACED: INTERCOSTAL P/N
- [SDR REXA2020102600724](https://openairdocs.org/sdr/REXA2020102600724.md): Seat Track · corroded · Sep 28, 2020 · N307PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN SEAT RAIL IS CORRODED BETWEEN FS 722.00 AND 724.00. REPLACED SEAT RAIL, IAW CRJ 900 AMM 53-00-49-400-801-A12. WVAC EMP STAMP 711 MTC.
- [SDR REXA2020102600730](https://openairdocs.org/sdr/REXA2020102600730.md): Door Sill · corroded · Sep 27, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SURROUND LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE, IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01, AND 51-42-36-001-001A-01.
- [SDR REXA2020102600727](https://openairdocs.org/sdr/REXA2020102600727.md): Mount · corroded · Sep 27, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > GALLEY MOUNT FITTING ON FLOOR SUPPORT STRUCTURE AT FS 285 JUST OUTBOARD OF RBL 12 IS CORRODED, TCI 53-20-315. REMOVED 1 EA CORRODED FITTING. LOCATED, DRILLED, AND INSTALLED 1 EA NEW FITTING P/N: SH670-32149-3 AT FS 285 OUTBOARD OF RBL 12, IAW CRJ 900 SRM 51
- [SDR REXA2020102600721](https://openairdocs.org/sdr/REXA2020102600721.md): Skin · chafed · Sep 27, 2020 · N307PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > RT INBOARD FLAP PANEL 684GB IS CHAFED. LOCATED, DRILLED, DEBURRED AND COUNTERSINK NEW SERVICEABLE PANEL 684GB, IAW CRJ 900 SRM 51-40-11-001-001-A01. WVAC EMP STAMP 774 MTC.
- [SDR REXA2020102600728](https://openairdocs.org/sdr/REXA2020102600728.md): Floor Support · corroded · Sep 25, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL AT FS 280 AND FS 319.70 IS CORRODED. TCI 53-20-315. REMOVED LIGHT SURFACE CORROSION FROM THE RT FLOOR SILL A FS 280-319.70, IAW CRJ 900 SRM 51-26-06-001-001-A01. NO NOTABLE MATERIAL LOSS. REMOVED AND REPLACED FILLER SEGMENT, IAW CRJ 900 SRM 5
- [SDR REXA2020102600719](https://openairdocs.org/sdr/REXA2020102600719.md): Skin · chafed · Sep 24, 2020 · N307PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > PANEL 584GB IS CHAFED. FOUND PANEL 584GB TO BE OUT OF LIMITS. RECEIVED SERVICEABLE PANEL P/N: CC670-14178-1. LOCATED, DRILLED, AND COUNTERSUNK HOLES, IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2020102600723](https://openairdocs.org/sdr/REXA2020102600723.md): Floorbeam · corroded · Sep 23, 2020 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 FWD J ANGLE CORRODED. REMOVED UNSERVICEABLE 280 CROSSBEAM FWD J ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED SERVICEABLE J ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-010-A01. WVAC EMP STAMP 77
- [SDR REXA2019042500518](https://openairdocs.org/sdr/REXA2019042500518.md): Light · inoperative · Apr 25, 2019 · N307PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY FLOOR TRACKS MISSING AT ROW 12 REPLACED FLOOR TRACK IAW AMM 33-51-01 P/N: ON PL1100LH07
- [SDR REXA2018012300046](https://openairdocs.org/sdr/REXA2018012300046.md): Oxygen Mask · leaking · Jan 23, 2018 · N307PQ · Cndair CL6002D24 · Crew Oxygen System
  > DURING STEP 8 OF TREND 8418, FOUND THE FIRST OFFICER`S OXYGEN MASK LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.
- [SDR REXA2017113001210](https://openairdocs.org/sdr/REXA2017113001210.md): Oxygen Mask · frayed · Nov 30, 2017 · N307PQ · Cndair CL6002D24 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK IS FRAYED. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12.
- [SDR REXA2017030800360](https://openairdocs.org/sdr/REXA2017030800360.md): Angle · corroded · Mar 8, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN ENTRY DOOR LOWER SILL ANGLE IS CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED MAIN ENTRY DOOR LOWER SILL IAW SRM 51-42-21 AND SRM 51-42-06. PAX DOOR OPS CHECK GOOD IAW MM 52-11-00-710-801.
- [SDR REXA2017030600362](https://openairdocs.org/sdr/REXA2017030600362.md): Housing · cracked · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS BAY DOOR HANDLE HOUSING IS CRACKED. REMOVED AND REPLACED THE E/E BAY DOOR HANDLE ASSY IAW AMM 52-42-03, AND SRM 51-42-21. OPS TESTED MAIN AVIONICS BAY DOOR GOOD IAW AMM 52-42-00-710-801.
- [SDR REXA2017030600361](https://openairdocs.org/sdr/REXA2017030600361.md): Post · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 DOOR POST LWR CORNER HAS CORROSION AT LBL 11 JUST ABOVE FLOOR LEVEL. REPAIRED DOOR POST IAW REO-670-53-11-745.
- [SDR REXA2017030600359](https://openairdocs.org/sdr/REXA2017030600359.md): Floorbeam · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION JUST AFT OF THE BS 280 BULKHEAD AT RBL 42 TO 45. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-21-139 REV A.
- [SDR REXA2017030600358](https://openairdocs.org/sdr/REXA2017030600358.md): Door Sill · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN ENTRY DOOR LOWER SILL MID CAP CORRODED. REMOVED AND REPLACED MID CAP ANGLE IAW SRM 51-41-02, AND SRM 51-42-06.
- [SDR REXA2017030600356](https://openairdocs.org/sdr/REXA2017030600356.md): Floorbeam · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON LT BS 280 FLOORBEAM. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-22, 51-42-21, AND REO 670-53-11-265.
- [SDR REXA2017030600355](https://openairdocs.org/sdr/REXA2017030600355.md): Floorbeam · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON BS 280 RT FLOORBEAM. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-22, 51-42-21, AND REO 670-53-11-265.
- [SDR REXA2017030600354](https://openairdocs.org/sdr/REXA2017030600354.md): Bulkhead Web · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > BS 280 BULKHEAD WEB CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 670-53-11-594 REV A, SRM 53-11-10, 53-00-00, 51-21-11, 51-25-06, AND 51-25-16.
- [SDR REXA2017030600353](https://openairdocs.org/sdr/REXA2017030600353.md): Bulkhead Web · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > BS 280 BULKHEAD AFT FACE HAS CORROSION AT FLOOR LEVEL BETWEEN RBL 42 AND 45. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS, REPAIRED THE BULKHEAD IAW BOMBA REO 670-53-11-594 REV, SRM 51-21-06, 53-11-10, 51-42-06, 51-42-13, 51-21-11, 51-25-06 AND 51-2
- [SDR REXA2017030600352](https://openairdocs.org/sdr/REXA2017030600352.md): Floorbeam · corroded · Mar 6, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE FWD SIDE, BS 280 CORROED BETWEEN LBL12 AND RBL 12. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED AND REPLACED THE ANGLE IAW SRMS 51-21-06, 53-00-00, 51-42-06, 51-25-06, 51-21-11, AND 51-40-11.
- [SDR REXA2017030400357](https://openairdocs.org/sdr/REXA2017030400357.md): Drag Angle · cracked · Mar 4, 2017 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT SIDE BY THE PULLEY DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT SIDE PULLY DRAG ANGLE IAW SRM 52-11-04, AND REO 670-52-11-072.
- [SDR REXA2017030300351](https://openairdocs.org/sdr/REXA2017030300351.md): Door · cracked · Mar 3, 2017 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT SIDE SECOND STEP FROM THE TOP LOWER CORNER BY THE HAND RAIL BRACKET AREA IS CRACKED. REMOVED DAMAGE AND REPAIRED IAW REO 670-52-11-104 AND SRM 52-11-04.
- [SDR REXA2017030300350](https://openairdocs.org/sdr/REXA2017030300350.md): Step · cracked · Mar 3, 2017 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT SIDE 3RD STEP FROM THE TOP LOWER CORNER ARE IS CRACKED. REMOVED DAMAGE AND REPAIRED IAW SRM 52-11-04.
- [SDR REXA2017030100349](https://openairdocs.org/sdr/REXA2017030100349.md): Bracket · cracked · Mar 1, 2017 · N307PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD SIDE SECOND STEP FROM THE TOP LOWER CORNER BY THE HAND RAIL BRACKET AREA IS CRACKED. REPAIRED PAX DOOR FWD SIDE 2ND STEP SIDE PANEL IAW REO 670-52-11-104.
- [SDR REXA2017022800348](https://openairdocs.org/sdr/REXA2017022800348.md): Frame · corroded · Feb 28, 2017 · N307PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > BS 333 FRAME FWD AND AFT FACE HAS CORROSION BETWEEN STRINGERS 26 AND 27R. REPAIRED THE FRAME IAW REO 670-53-21-1281.
- [SDR REXA2017010900022](https://openairdocs.org/sdr/REXA2017010900022.md): Oxygen Mask · unwanted deploy · Jan 9, 2017 · N307PQ · Cndair CL6002D24 · Passenger Oxygen System
  > 02 MASK OVER 5AB FELL OUT. RESECURED AS REQUIRED.
- [SDR REXA2016070101193](https://openairdocs.org/sdr/REXA2016070101193.md): Life Vest · unserviceable · Jul 1, 2016 · N307PQ · Cndair CL6002D24 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW EE900 AND AMM 25-61-03.

## 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 = 'N307PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N307PQ/reports

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