1. REMOVE AFFECTED FASTNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REFER DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 103 WORKSHEET NO: 50173. 3. INSTALL FASTENERS IAW SRM - [SDR UIEA2025041400461](https://openairdocs.org/sdr/UIEA2025041400461.md): Seat Track · cracked · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1730, RBL 75.92.(
1. ACCOMPLISHED W/S NO: 50170 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2025041400462](https://openairdocs.org/sdr/UIEA2025041400462.md): Seat Track · cracked · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, RBL 75.(1. ACCOMPLISHED W/S NO. 50172 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2025041400463](https://openairdocs.org/sdr/UIEA2025041400463.md): Seat Track · cracked · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > CRACK - FOUND M/D FLOOR STRUCTURE TRACK SUBSTITUTE CRACK BETWEEN STA 980 TO STA 1000, LBL 75.92.(1. ACCOMPLISHED W/S NO. 50160 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2025041400464](https://openairdocs.org/sdr/UIEA2025041400464.md): Seat Track · cracked · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings > CRACK - FOUND M/D CGO COMPT SUB SEAT TRACK CRACK BETWEEN STA 660 TO STA 720, LBL 75.92, TTL 3 EA.(1. ACCOMPLISHED W/S NO. 50182 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR UIEA2025041400465](https://openairdocs.org/sdr/UIEA2025041400465.md): Floorbeam · corroded · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage Main, Floor Beam > CORROSION - MFOUND M/D FLOOR BEAM CORROSION AT STA 2240 RBL 57 TO RBL 85.(1. REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103 W/S 50176 AND EI NO: T2025A53M-546 REV 1. 3. INSTALL FASTNERS IAW SRM 5 - [SDR UIEA2025041400468](https://openairdocs.org/sdr/UIEA2025041400468.md): Floorbeam · corroded · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage Main, Floor Beam > CORROSION - FOUND M/D FLOOR BEAMS TOP SURFACE CORROSION STA 1500 BETWEEN LBL 55 TO LBL 75.92.(
1. REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103, W/S NO: 50169 AND EI NO: T2025A53M-4 - [SDR UIEA2025041400469](https://openairdocs.org/sdr/UIEA2025041400469.md): Splice Angle · corroded · Apr 15, 2025 · N453PA · Boeing 74746NF · Fuselage Miscellaneous Structure > CORROSION - FOUND SPLICE ANGLE CORROSION AT M/D COMPARTMENT BETWEEN STA 2280 TO STA 2300, RBL 68.(
1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 65B38694 SHEET 3 REV C. 3. CONDITION CHECK - [SDR UIEA2025041400471](https://openairdocs.org/sdr/UIEA2025041400471.md): Bracket · corroded · Apr 15, 2025 · N453PA · Boeing 74746NF · Aerodynamic Fairings > CORROSION - BRACKET LOWER FUSELAGE WING-TO-BODY SUPPORT BRACKET STA 920 BL 0.(
1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 14240130 SHEET 1 REV A. 3. JOB COMPLETED AND CONDITION CHECK N - [SDR UIEA2025041400473](https://openairdocs.org/sdr/UIEA2025041400473.md): Elt · expired · Apr 15, 2025 · N453PA · Boeing 74746NF · Emergency Locator Beacon > FWD M/D FIXED ELT BATTERY NEAR DUE DATE (03JUN25).(
1. REPLACED ELT TRANSMITTER IAW SWPM 20-60-06. 2. STEP A & B PERFORMED ELT INSTALLATION TEST IAW T/C NO: 23-024-00-03. THE RESULT WAS SATISFACTORY.
) - [SDR UIEA2025021600148](https://openairdocs.org/sdr/UIEA2025021600148.md): Engine · vibration · Feb 16, 2025 · N453PA · Boeing 74746NF · Engine (Turbine/Turboprop) > ENG 1 VIB 4.0, N1 FAN, STEADY INCREASE THRU UPPER 20'S FLIGHT LEVEL.(RAN ENG 1 PER 71-00-00-705-057-J00. NOTED 3.1 VIBRATION PEAK PER MCC ENGINEERING. OPS CHECK NORMAL.
) - [SDR UIEA2024061200516](https://openairdocs.org/sdr/UIEA2024061200516.md): Line · broken · Jun 12, 2024 · N453PA · Boeing 74746NF · Humidity Control System > ADVISORY MSG "SMOKE CREW REST " AROUND 800 TO 1000 FEET AFTER T.O., FOLLOWED BY FUMES ON THE FLIGHT DECK.(R/R CREW REST AREA TRIM AIR MODULATING VLV, REAPIRED BROKEN WATER SEPERATOR LINE, AND REPLACED COALLESOR BAGS PER AMM 21-61-16. OPS CHK GOOD.
) - [SDR UIEA2024032800229](https://openairdocs.org/sdr/UIEA2024032800229.md): Unknown · faulted · Mar 28, 2024 · N453PA · Boeing 74746NF · Flight Control System > DURING TAKEOFF NOTICED UNCOMMANDED ROLLING, ALSO ON LANDING AIRCRAFT ROLLED UNCOMMANDED TO LEFT.(ABNORMALITY PRESSURIZED HYD, & TRIM RUDDER TO NEUTRAL, RUDDER & RUDDER TRIM CONTROL SYS OPS CHECK NORMAL PER AMM 27-21-00 WITH FULL FLAP FULL UP, SPOILER OPS & - [SDR UIEA2024021900092](https://openairdocs.org/sdr/UIEA2024021900092.md): Winglet · not reported · Feb 19, 2024 · N453PA · Boeing 74746NF · Wing Main, Frame Structure > LEFT WINGLET SCRAPED.(
TRANSFERED TO DMI 203268 IAW CDL 57-28-01 DUE DATE 18JUN24. PLACARD INSTALLED.
) - [SDR UIEA2023052600524](https://openairdocs.org/sdr/UIEA2023052600524.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > COCKPIT - RH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(COCKPIT - RH RUDDER PEDAL CAVITIES, RH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-212 CRACK AREA REPAIRED IAW RI-53-16279 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023052600525](https://openairdocs.org/sdr/UIEA2023052600525.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > COCKPIT - LH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(COCKPIT - LH RUDDER PEDAL CAVITIES, LH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-210 CRACK AREA REPAIRED IAW RI-53-16-16279 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023052600527](https://openairdocs.org/sdr/UIEA2023052600527.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > 1EA SURFACE CRACK FOUND ON LH STA 2231 STR 21L TO STR 22L REVEAL CRACK APPROX 2.375" IN LENGTH.(STA 2231 STR 21L TO 22L, #5 DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000528](https://openairdocs.org/sdr/UIEA2023053000528.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > AFT CARGO STA 1700 FLOOR BEAM MIDDLE AREA FOUND CHAFING.(AFT CARGO STA 1700 FLOOR BEAM UPPER CHORD P/N: 65B07373-3 CHAFING AREA REPAIRED IAW RI-53-60-16278 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000539](https://openairdocs.org/sdr/UIEA2023053000539.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW I/B FORE FLAP UPPER SURFACE 59" TO I/B EDGE FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000540](https://openairdocs.org/sdr/UIEA2023053000540.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW I/B FORE FLAP UPPER SURFACE 145" TO I/B EDGE FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000541](https://openairdocs.org/sdr/UIEA2023053000541.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW I/B FORE FLAP MID L/E FAIRING SKIN FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000542](https://openairdocs.org/sdr/UIEA2023053000542.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW I/B FORE FLAP UPPER SURFACE 226" TO I/B EDGE FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000543](https://openairdocs.org/sdr/UIEA2023053000543.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW O/B FORE FLAP O/B L/E FAIRING SKIN FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023053000544](https://openairdocs.org/sdr/UIEA2023053000544.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > RHW O/B FORE FLAP L/E FAIRING SKIN 127" TO I/B FOUND DELAMINATION(PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060100552](https://openairdocs.org/sdr/UIEA2023060100552.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > LH STA 720 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(STA 720 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060100553](https://openairdocs.org/sdr/UIEA2023060100553.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > RH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(STA 760 RH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060100554](https://openairdocs.org/sdr/UIEA2023060100554.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > LH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(STA 760 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060400564](https://openairdocs.org/sdr/UIEA2023060400564.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW I/B AILERON UPPER SURFACE AFT O/B CORNER FOUND DELAMINATION(PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-06 PAR 5G. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060500565](https://openairdocs.org/sdr/UIEA2023060500565.md): Shear Tie · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND RBL 33.99(STA 1000 RBL 33.99 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 APRT 8 AND RI-53-43-16281 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060500566](https://openairdocs.org/sdr/UIEA2023060500566.md): Shear Tie · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND LBL 75.92(STA 1000 LBL 75.92 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 6 AND RI-53-43-16285 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060500567](https://openairdocs.org/sdr/UIEA2023060500567.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE FOUND CRACK(BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE CRACK AREAS REPAIRED IAW RI-53-40-16280 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060500568](https://openairdocs.org/sdr/UIEA2023060500568.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > 1EA THOUGHT THICKNESS CRACK FOUND ON LH BS2231 S16 STRAP (COUNT FROM O/B SECOND LAYER) RUNNING FWD AT 4 O/C POSITION (VIEW LOOKING O/B).(M/D - STA 2231 STR 16L FRAME STRAP P/N: 65B01849-25 CRACK AREA REPAIRED IAW RI-53-60-16284 REV.A. NO FURTHER DEFECTS NOT - [SDR UIEA2023060500569](https://openairdocs.org/sdr/UIEA2023060500569.md): Longeron · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > STA 1480 RH LONGERON EXTENSION FTG FOUND CRACKED(
STA 1480 RH LONGERON EXTENSION FTG P/N: 65B15034U24 REPLACED AND INSTALLED IAW EO 4453A818 PART 4. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060500570](https://openairdocs.org/sdr/UIEA2023060500570.md): Longeron · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > STA 1480 LH LONGERON EXTENSION FTG FOUND CRACKED(STA 1480 LH LONGERON EXTENSION FTG P/N: 65B15034U23 REPLACED AND INSTALLED IAW EO 4453A818 PART 3. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060600581](https://openairdocs.org/sdr/UIEA2023060600581.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > DAMAGE LOG D-4-15 - DENT BOTTOM OF BULK CARGO FRAME, STA 1992 WL175, L=3/4" X W=3/4" X D=1/32", PER SRM 53-00-01-1A-1 TABLE 1 DETAIL 3 ADL LIMIT.(FX - STA 1992 STR 42R TO STR 43R SKIN DAMAGED AREA REPAIRED IAW RI-53-61-16293 REV.A. NO FURTHER DEFECTS NOTED< - [SDR UIEA2023060600582](https://openairdocs.org/sdr/UIEA2023060600582.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Cabin Equipment/Furnishings > FWD CARGO AFT ROW BALLMAT MID PANEL RH AFT CORNER CRK(
FWD CARGO COMPT AFT CTR BALLMAT PANEL P/N: 192511-3 CRACK AREA REPAIRED IAW RI-53-20-16283 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060700597](https://openairdocs.org/sdr/UIEA2023060700597.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > LH BS 740 TENSION TIE FWD CHANNEL 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT 12 O'CLOCK AND 6 O'CLOCK POSITION.(STA 740 LH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060700608](https://openairdocs.org/sdr/UIEA2023060700608.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Doors > LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING(LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING AREA REPAIRED IAW RI 52-82-16282 REV A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060800609](https://openairdocs.org/sdr/UIEA2023060800609.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > EO 4453A516 PART 4, STA 400 RH WAS A REPAIR PREVIOUSLY INSTALLED IN THE MODIFICATION AREA.(FX STA 400 RH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 4 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060800610](https://openairdocs.org/sdr/UIEA2023060800610.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Fuselage Structure (General) > FX STA 400 LH NOSE WW AFT CORNER SKIN CRACK(FX STA 400 LH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060900613](https://openairdocs.org/sdr/UIEA2023060900613.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Cabin Equipment/Furnishings > M/D SCD AFT DR SILL O/B ASSY UPPER SKIN LWR SIDE FOUND CORROSION CRACK.(M/D SCD AFT DOOR SILL O/B SILL ASSY CHANNEL CORROSION CRACK AREA REPAIRED IAW RI-25-50-16314 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060900614](https://openairdocs.org/sdr/UIEA2023060900614.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > RHW T/E O/B AFT FLAP O/B UPPER PANEL FOUND CHAFING(PERFORMED REPAIR AT CHAFING AREA AS PER RI-57-50-16296 REV.A. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060900615](https://openairdocs.org/sdr/UIEA2023060900615.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW T/E I/B FORE FLAP MOST O/B UPPER PANEL FOUND TWO DENTS(PERFORMED REPAIR AT DENTS AREA PER SRM 51-70-10 REPAIR2 FIG203. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023060900616](https://openairdocs.org/sdr/UIEA2023060900616.md): Unknown · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Flight Control System > LHW T/E I/B AFT FLAP UPPER O/B PANEL FOUND CHAFING(PERFORMED REPAIR AT CHAFING AREA IAW SRM 51-70-10 REPAIR 2 FIG 203. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023061200637](https://openairdocs.org/sdr/UIEA2023061200637.md): Battery Pack · unknown · Jun 12, 2023 · N453PA · Boeing 74746NF · Lighting System > MAIN DECK EMERGENCY LT FND INOP DURING OPS CHK(EMERGENCY LT BATTERY PACK M5170 REPLACED AS PER AMM 33-51-04. OPS CHECK GOOD
) - [SDR UIEA2022070800758](https://openairdocs.org/sdr/UIEA2022070800758.md): None · none · Jul 11, 2022 · N453PA · Boeing 747 · Trailing Edge Flap Control System > FOUND PITTING IN STRUCTURE SURROUNDING #6 CARRIAGE SPINDLE BEARING(R/R RH INBD MID FLAP IAW AMM 27-50-00
) - [SDR P5CA2022021600041](https://openairdocs.org/sdr/P5CA2022021600041.md): None · none · Feb 13, 2022 · N453PA · Boeing 74746NF · Fuselage Main, Structure > FUSELAGE SKIN (P/N 65B23673-4) - PUNCTURE DAMAGE AT STA 690, BETWEEN S-34R AND S-35R(THE DAMAGED SKIN PORTION WAS TRIMMED OUT, DETAIL VISUAL INSPECTION, SURFACE AND OPEN-HOLE HFEC INSPECTIONS WERE PERFORMED
- [SDR P5CA2021080300272](https://openairdocs.org/sdr/P5CA2021080300272.md): Controller · faulted · Aug 1, 2021 · N453PA · Boeing 74746NF · Compressor Bleed Valve
> DURING CLIMB OUT #1, #2 & #4 BLEED VALVE OFF LIGHT ILLUMINATED WITH BLEED SWITCHES SELECTED ON, CYCLED VALVES WITH NO RESOLUTION.( REMOVED AND REPLACED #3 BLEED PRV CONTROLLER IAW B747 AMM 36-11-19, REMOVED AND REPLACED #3 PRSOV IAW B747 AMM 36-11-04,
Next page: https://openairdocs.org/aircraft/N453PA/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 = 'N453PA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```
This list as a web page: https://openairdocs.org/aircraft/N453PA/reports
---
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