# Service difficulty reports: N571JB

A list on [N571JB](https://openairdocs.org/aircraft/N571JB.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 · 88 reports

- [SDR YENA2026081700689](https://openairdocs.org/sdr/YENA2026081700689.md): Pump · leaking · Aug 15, 2026 · N571JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > FLT 585, JFK-RDU (AIRTURN BACK TO JFK) G RSVR KO LVL ON TAKEOFF-ECAM-HYD PAGE SHOWED B SYS RSVR LO LVL.. R & R GREEN SYS EDP (1030EK) IAW AMM 29-11-51 UP TO SUBTASK 29-11-51-860-001-A. OPS+LEAK CHK IAW AMM 29-11-51-400-010-A FROM SUBTASK 29-11-51-860-040 TO C
- [SDR YENA2025102801060](https://openairdocs.org/sdr/YENA2025102801060.md): Apu · odor · Oct 24, 2025 · N571JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#1233, MCO-SJU. "DURING CLIMB AND CRUISE INFLIGHT CREW REPORTED STRONG ODOR/SMELL OF STINKY CHEESE/DIRTY SOCKS. REPORT FROM FWD GALLEY TO ROW 4. MODERATE INTENSITY LEVEL2. FOM POLICY COMPLIED WITH AND CALLS TO DISPATCH AND MX. IRRITATING NOSE SMELLS; ACCOM
- [SDR YENA2025100100989](https://openairdocs.org/sdr/YENA2025100100989.md): Battery · failed · Oct 1, 2025 · N571JB · Airbus A320232 · Emergency Lighting
  > FLT#591, BOS-TPA. "DURING CHECK OF EMERGENCY BATTERY CABIN IAW AMP TASK 335100-03-1 FWD L BATT FAULT FOUND; REMOVED AND REPLACED L FWD BATT 10WL IAW AMM 33-51-38 CKD GOOD."
- [SDR YENA2025100100988](https://openairdocs.org/sdr/YENA2025100100988.md): Battery · failed · Oct 1, 2025 · N571JB · Airbus A320232 · Emergency Lighting
  > FLT#591, BOS-TPA. "EMERGENCY EXIT SIGNS AIRCRAFT RIGHT REMAINED ON ENTIRE FLIGHT AND AIRCRAFT RIGHT WAS OFF ENTIRE FLIGHT; ED TSM 33-51-00-810-837A PERFORMED EPSU OPS BITE CK IAW AMM 33-51-00 FOUND 11WL BATT FAULT DURING BITE(L EMERG EXIT BATT) R&R 11WL BAT
- [SDR YENA2025022500193](https://openairdocs.org/sdr/YENA2025022500193.md): Cooling Fan · leaking · Feb 25, 2025 · N571JB · Airbus A320232 · APU Core Engine
  > FLT#1979, DCA-FLL. 'UPON LANDING INFLIGHT WORKING REAR OF AIRCRAFT COMPLAINED OF ODOR ON DECENT, NO SMELL IN COCKPIT OR FRONT CABIN; FOUND APU COOLING FAN LEAKING REF LOG PG 4236461-2 COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. LEVEL 1 TYPE 1 WAS P
- [SDR YENA2024111201470](https://openairdocs.org/sdr/YENA2024111201470.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 20 LH SIDE FROM HOLE 7 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.135 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00027) REF AE WO 2024-275/1. N/R# 2024 -
- [SDR YENA2024111201469](https://openairdocs.org/sdr/YENA2024111201469.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 20 RH SIDE FROM HOLE 3 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I IS 0.045 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00028) REF AE WO 2024-275/1. N/R# 2024
- [SDR YENA2024111201468](https://openairdocs.org/sdr/YENA2024111201468.md): Door · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LH SIDE FROM HOLE 7 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.097 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00029) REF AE WO 2024-275/1. N/R# 2024 -
- [SDR YENA2024111201467](https://openairdocs.org/sdr/YENA2024111201467.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE 8 OF JOOGLE AREA LOC ATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.087 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00031) REF AE WO 2024-275/1. N/R# 2024
- [SDR YENA2024111201466](https://openairdocs.org/sdr/YENA2024111201466.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.16 RH DOOR STOP FITTING 7 LOWER I/B HOLE. CRACK DEPTH IS 0.165 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00032) REF AE WO 2024-275/1. N/R# 2024 - 538515. REMOVED AND RE
- [SDR YENA2024111201465](https://openairdocs.org/sdr/YENA2024111201465.md): Door Frame · no discrepancy · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: (RESOLVED ON W/O: 1318564 TASKCARD: NR-00033) REF AE WO 2024-275/1. N/R# 2024 - 538516. REMOVED AND REPLACED INTERCOSTAL FITTING LOC. ON FR.16 LH DOOR STOP FITTING 7 I.A.W. A320 SRM 53-11-12-300-010 STEP 2.A. FIGURE 001 (SHEET 1) AND
- [SDR YENA2024111201464](https://openairdocs.org/sdr/YENA2024111201464.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.16 LH DOOR STOP FITTING 7 LOWER I/B HOLE, CRACK DEPTH IS 0.123 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00034) REF AE WO 2024-275/1. N/R# 2024 - 538517. REMOVED AND RE
- [SDR YENA2024111201463](https://openairdocs.org/sdr/YENA2024111201463.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE A OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.084 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00035) REF AE WO 2024-275/1. N/R# 2024 -
- [SDR YENA2024111201462](https://openairdocs.org/sdr/YENA2024111201462.md): String · corroded · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L AND BTW FR58 TO FR60 AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1318564 TASKCARD: NR-00036) REF AE WO 2024-275/1. N/R# 2024 - 538624. PERFORMED PERMANENT REPAIR ON STRINGER 43L AND BTW FR58 TO FR60
- [SDR YENA2024111201461](https://openairdocs.org/sdr/YENA2024111201461.md): Stringer · corroded · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L AND BTW FR58 TO FR59 AFT CARGO COMPARTMENT (CPCP FINDING);(RESOLVED ON W/O: 1318564 TASKCARD: NR-00037) REF AE WO 2024-275/1. N/R# 2024 - 538625. PERFORMED PERMANENT REPAIR ON STRINGER 42L AND BTW FR58 TO FR59 A
- [SDR YENA2024111201460](https://openairdocs.org/sdr/YENA2024111201460.md): Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE B OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.081 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00039) REF AE WO 2024-275/1. N/R# 2024 -
- [SDR YENA2024111201459](https://openairdocs.org/sdr/YENA2024111201459.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE D OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.101 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00040) N/R# 2024 - 538560. PERFORMED PE
- [SDR YENA2024111201458](https://openairdocs.org/sdr/YENA2024111201458.md): Fastener · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.20 RH DOOR STOP FITTING 7 UPPER I/B HOLE. CRACK DEPTH IS 0.081 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00041) REF AE WO 2024-275/1. N/R# 2024 - 538513. PERFORMED REPA
- [SDR YENA2024111201457](https://openairdocs.org/sdr/YENA2024111201457.md): Stabilizer · worn · Nov 6, 2024 · N571JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: WEAR ON HINGE 6 UPPER SIDE LOWER AREA ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00042) REF AE WO 2024-275/1. N/R# 2024 - 538686. REMOVED AND REPLACED HINGE #6 ON VERTICAL STABILIZER IAW A320 SRM 51-42-11, A320 SRM
- [SDR YENA2024111201456](https://openairdocs.org/sdr/YENA2024111201456.md): Hinge · worn · Nov 6, 2024 · N571JB · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FASTENER HOLE FR16 RH STOP FITTING 7 UPPER I/B HOLE. CRACK DEPTH IS 0.18; EF AEROMAN W.O. 2024 275/1 NR 538514 * PERFORMED REPAIR ON FR.16 RH DOOR STOP FITTING 7 UPPER I/B HOLE IAW A320 SRM 53-11-12-300-010. THIS R
- [SDR YENA2024111201455](https://openairdocs.org/sdr/YENA2024111201455.md): Service difficulty · Nov 6, 2024 · N571JB · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: WEAR ON STRINGER 39R LOCATED BTW FR47 TO FR 48 AFT CARGO COMPARTMENT; REF AERMAN W.O. 2024 275/1 NR 538884 * REMOVED AND REPLACED STRINGER 39R LOCATED ON AFT CARGO COMPARTMENT BWT FR 50 AND FR 51 IAW A320 SRM 51-72-11 AND DWG D5347
- [SDR YENA2024111201454](https://openairdocs.org/sdr/YENA2024111201454.md): Hinge · worn · Nov 6, 2024 · N571JB · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 31R LOCATED BTW FR64 TO FR65 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN WO 2024 275/1 NR 538820 * REMOVED AND REPLACED STRINGER LOC. FR64 TO FR65 STRG 31RH IAW A320 SRM 51-42-11 AND DWG D53480505, D5348006
- [SDR YENA2024111201453](https://openairdocs.org/sdr/YENA2024111201453.md): Hinge · worn · Nov 6, 2024 · N571JB · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / PRESSURE BULKHEAD / HOLES #2 & 6 / CRACK DAMAGE – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-9052-24 REV. 0 (COVER + PARTS 1-5) /2/ AIRBUS RDAF 81474600/004/2024#A /3/ AIRBUS MES
- [SDR YENA2024111201452](https://openairdocs.org/sdr/YENA2024111201452.md): Door Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 20 RH / DOUBLE JOGGLE AREA / DOOR STOP FITTING 7 HOLE 6 / CRACK - PERMANENT REPAIR (FRAME REPLACEMENT); REFERENCES: /1/ AEROMAN EA 53-9051-24 REV. 0 (COVER & PART 1 - 2) /2/ AIRBUS SB A320-53-1374 REV
- [SDR YENA2024111201451](https://openairdocs.org/sdr/YENA2024111201451.md): Frame · cracked · Nov 6, 2024 · N571JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9043-24 COVER REV.0 & PART 1-5 /2/ AIRBUS SB A320-53-1331 (REF. FAA AD
- [SDR YENA2024071600997](https://openairdocs.org/sdr/YENA2024071600997.md): Pressure Switch · failed · Jul 12, 2024 · N571JB · Airbus A320232 · APU Oil System
  > FLT#1691, JFK-LIR. (AIRCRAFT DIVERTED TO MCO) 'APU AUTO SHUTDOWN IN CRUISE FLIGHT -ATTEMPTED RESTART IN COORDINATION WITH MCC BUT IT WAS NOT SUCCESSFUL UNIT REMAINED OFF FOR DURATION OF FLIGHT; PER TSM 49-00-81-810-819A REMOVED AND REPLACED LOW OIL PRESSURE S
- [SDR YENA2024071100952](https://openairdocs.org/sdr/YENA2024071100952.md): Unknown · odor · Jul 11, 2024 · N571JB · Airbus A320232 · Air Distribution System
  > FLT#131, MCO-LAX. 'ON FINAL APPROACH FLIGHT ATTENDANT NOTED BR/EF DIRTY SOCK TYPE ODOR. THIS WENT AWAY SHORTLY AFTER LANDING ROLL-OUT. NEITHER CAPT NOR F/O NOTICED ANYTHING; SEE LOG PAGE 4087210, ITEM 2 (COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ISO
- [SDR YENA2024051500747](https://openairdocs.org/sdr/YENA2024051500747.md): Unknown · odor · May 12, 2024 · N571JB · Airbus A320232 · Air Distribution System
  > FLT#975, JFK-MSY. ' ODOR IN AFT CABIN ON DESCENT; C/W INFO NOTED, 2017-7015 SEC:A ISOLATED FAULT TO TYPE. 10. REF: 75M 05-50-00, ACFT OK FOR SERVICE.'
- [SDR YENA2024031400422](https://openairdocs.org/sdr/YENA2024031400422.md): Unknown · odor · Mar 12, 2024 · N571JB · Airbus A320232 · Air Distribution System
  > FLT#1079, JFK-MBJ. 'ODOR EVENT BEGAN AT TOP OF DESCENT. LAST 5 ROWS OF A/C EXPERIENCED A CLEANING LIKE SMELL REPORTED TO FLT CREW AT GATE. ( PACKS); "COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL "B" WAS ACCOMPLISHED PER TSM 05
- [SDR YENA2023111301372](https://openairdocs.org/sdr/YENA2023111301372.md): Unknown · unknown · Nov 11, 2023 · N571JB · Airbus A320232 · Air Distribution System
  > FLT#5, JFK-PTP. 'BEGINING AROUND 12000 FEET ON DEC. BEGAN TO SMELL STRONG DIRTY SOCK SMELL.CONTACTED #1 FA AND ALL CREW MEMBERS EXPERIENCED THE SAME SMELL BUT STRONGER. OIP- SWITCHED OF PACK 2 AND SMELL DIS; REFERENCE L/P 3819610-2 (COMPLIED WITH INFORMATION N
- [SDR YENA2023100201168](https://openairdocs.org/sdr/YENA2023100201168.md): Unknown · unknown · Sep 29, 2023 · N571JB · Airbus A320232 · Air Distribution System
  > FLT#1167, HPN-PBI. 'APPARENT TRICRESYLPHISPATE FUMES ( OIL FUMES) ON DEP OUT OF HPN. DISSIPATED QUICKLY MUCH STRONGER FUMES ODOR ON IDLE DESCENT PACK 1 OFF USING ODOR ISOLATION PROCEDURE SEEMED TO MINIMIZE ODOR PHYSIOLOGICAL EFFECTS FELT BY BOTH PILOTS ( PACK
- [SDR YENA2022071200664](https://openairdocs.org/sdr/YENA2022071200664.md): Blade · damaged · Jul 9, 2022 · N571JB · Airbus A320232 · Turbine Engine Compressor Section
  > FLT#1359, JFK-KIN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' BIRD STRIKE ON TO ROLL ENG 2 VIBE (N1) N 5.1 ON CLIMB OUT AND NOTICED HIGHER ENG 2 VIB ON GROUND WITH REV THURST APPLIED ON LDG OVERWEIGHT LANDING SMOOTH; ACCOMPLISHED BIRD STRIKE INSPECTION IAW
- [SDR YENA2022050600450](https://openairdocs.org/sdr/YENA2022050600450.md): None · none · May 2, 2022 · N571JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#2295, EWR-MIA. ' DIRTY SOCK SMELL FROM T/O AND DURING DECENT. GOT A CALL FROM FA( AFT) AT 15000 CLEAR SKIES DURING DESCENT. RAINING DURING TAKE OFF APU WAS OFF FOR T/O AND DESCENT. DID PERF FCOM 1 ODOR ISOLATION TO NO CHANGES; LEVEL ODOR DEEMED LEVEL A/
- [SDR YENA2021042300264](https://openairdocs.org/sdr/YENA2021042300264.md): Flap System · warning message · Apr 23, 2021 · N571JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLT 2894, MIA-EWR. F/CTL FLAPS LOCKED - WING TIP BRK ON ECAM CAME ON WHEN CONFIGURING TO LAND. IN SELECTING FLAPS 2 THE FLAP HANDLE OVERSHOT 1/1 WAY TO FLAPS 3. IN RETURNING THE HANDLE TO THE FLAPS 2 POSITION WE POTENTIALLY TRIGGERED THE ECAM; PERFORMED BITE
- [SDR YENA2021032500189](https://openairdocs.org/sdr/YENA2021032500189.md): Unknown · odor · Mar 20, 2021 · N571JB · Airbus A320232 · Air Distribution System
  > FLT 2459, BDL-FLL. DURING FINAL TO ILS 28L, F/O SMELLED DIRTY SOCK SMELL. AFTER LANDING FLT ATT'S REPORTED NOTHING SIGNIFICANT UNTIL REACHING GATE. (NO AIR/BLEED ON); COMPLIED WITH INFORMATION NOTICE 2017-TO15 SECTION A. AIRCRAFT IO OK FOR SERVICE.
- [SDR YENA2020101900491](https://openairdocs.org/sdr/YENA2020101900491.md): Proximity Sensor · out of adjust · Oct 15, 2020 · N571JB · Airbus A320232 · Emergency Equipment
  > FLIGHT NR 104, SDQ-EWR. L1 DOOR SLIDE INDICATION INOPERABLE. REMOVED AND REINSTALLED SLIDE PAC AT L1 DOOR TO VERIFY PROPER INSTALLATION, REF AMM 25-62-44. ADJUSTED L1 DOOR PROXIMITY SENSOR & CHECK OPERATIONS GOOD, IAW AMM 52-73-11. A/C OK FOR CONTINUED SER
- [SDR YENA2020072200396](https://openairdocs.org/sdr/YENA2020072200396.md): Valve · failed · Jul 19, 2020 · N571JB · Airbus A320232 · Pneumatic Distribution System
  > FLT 2137, AFTER TAKEOFF ECAM NR 1 AIR BLEED FAULT. RETURNED TO FIELD. EMERGENCY DECLARED. R & R BOTH HP VALVE & PRESSURE REGULATING VALVE. PERFORMED A BLEED HEALTH MONITERING CHECK IAW MCC REQUEST. OPS CHECKED GOOD IAW AMM 36-11-00.
- [SDR YENA2020072200395](https://openairdocs.org/sdr/YENA2020072200395.md): Valve · failed · Jul 19, 2020 · N571JB · Airbus A320232 · Pneumatic Distribution System
  > FLT 2137, AFTER TAKEOFF, ECAM NR 1 AIR BLEED FAULT. RETURNED TO FIELD. EMERGENCY DECLARED. R & R BOTH THE HP VALVE, & PRESSURE REGULATING VALVE. PERFORMED BLEED HEALTH MONITERING CHECK IAW MCC REQUEST, OPS CHECKED GOOD IAW AMM 36-11-00.
- [SDR YENA2020072200394](https://openairdocs.org/sdr/YENA2020072200394.md): Valve · failed · Jul 19, 2020 · N571JB · Airbus A320232 · Pneumatic Distribution System
  > FLT 2137, AFTER TAKEOFF, ECAM NR 1 AIR BLEED FAULT. RETURNED TO FIELD. EMERGENCY DECLARED. R & R BOTH THE HP VALVE & PRESSURE REGULATING VALVE. PERFORMED BLEED HEALTH MONITERING CHECK IAW MCC REQUEST. OPS CHECKED GOOD IAW AMM 36-11-00.
- [SDR YENA201907200415](https://openairdocs.org/sdr/YENA201907200415.md): Fan · failed · Jul 20, 2019 · N571JB · Airbus A320232 · Air Distribution Fan
  > FLT 61, BOS-SJU. EXCESSIVE NOISE FROM BLOWER FAN FOLLOWED BY A WIFF OF SMOKE. SELECTED FAN TO OVRD. ( BLOWER FAN - NO AVNCS SYS FAULT ECAM CAUTION); ACCOMPLISHED INSPECTION AS PER TSM 05-50-00 / AND BLOWER FAN TSM 21-26-00-11600-00-A. ITEM PLACED ON MEL 21-2
- [SDR YENA2018092860392](https://openairdocs.org/sdr/YENA2018092860392.md): Floorbeam · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42699: FR16 FLR BEAM -Y1292 CORR; REF NR 42699 FOR ALL WORK ACP: CORR BEYOND LIM RPL FLR BEAM -Y1292 FR16 PER SRM 51-72-11.
- [SDR YENA2018092860391](https://openairdocs.org/sdr/YENA2018092860391.md): Floorbeam · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42517: FR68 FLR BEAM Y1292 CORR; REF NR 42517 FOR ALL WORK ACP: CORR BEYOND LIM RPL FLR BEAM Y1292 FR68 PER SRM 51-72-11.
- [SDR YENA201809260390](https://openairdocs.org/sdr/YENA201809260390.md): Floor Support · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42698: FR20 FLR BEAM Y1292 CORR; REF NR 42698 FOR ALL WORK ACP: CORR BEYOND LIM RPL FLR BEAM FR12-24 PER SRM 51-72-11.
- [SDR YENA2018092860389](https://openairdocs.org/sdr/YENA2018092860389.md): Door Sill · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42515: L2 DR SILL CUTOUT CORR ON FR68 STR23 LH; REF NR 42515 FOR ALL WORK ACP: RPL L2 DR SILL IAW SRM 51-72-11-911-001.
- [SDR YENA2018092860388](https://openairdocs.org/sdr/YENA2018092860388.md): Seat Track · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42590: CABIN SEAT TRACK Y765 FR16 CORR; REF NR 42590 FOR ALL WORK ACP: RPL FLR SEAT TRACK PER SRM 51-72-11.
- [SDR YENA2018092860387](https://openairdocs.org/sdr/YENA2018092860387.md): Attach Angle · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42595: CABIN FLR BEAM ATTACH ANGLE CORR RH FR20; REF NR 42595 FOR ALL WORK ACP: CORR BEYOND LIM RPL BEAM ANGLE RH FR 20-24 WEB BEAM PER SRM 51-42-11.
- [SDR YENA2018092860386](https://openairdocs.org/sdr/YENA2018092860386.md): Beam · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42589: CABIN DUMMY BEAM AT Y512 FR16L CORR; REF NR 42589 FOR ALL WORK ACP: CORR BEYOND LIM RPL DUMMY BEAM PER SRM 51-42-11.
- [SDR YENA2018092860385](https://openairdocs.org/sdr/YENA2018092860385.md): Web · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42568: AFT CARGO COMP WEB SILL UPR SKIN FR53-FR55 CORR; REF HAECO NR 440504-42568: AFT CARGO COMP WEB SILL UPR SKIN FR53-FR55 CORR.
- [SDR YENA201809286384](https://openairdocs.org/sdr/YENA201809286384.md): Web · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42465: FWD CARGO COMP WEB SILL FR26-FR28 CORR; REF NR 42465 FOR ALL WORK ACP: CORR BEYOND LIM RPL WEB SILL FR26-FR28 PER SRM 51-42-11.
- [SDR YENA2018092860383](https://openairdocs.org/sdr/YENA2018092860383.md): Floorbeam · corroded · Sep 26, 2018 · N571JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED, REF HAECO NR 440504-42534: RH AFT CABIN FLR BEAM -Y1292 CORR 11IN FWD FR67; REF NR 42534 FOR ALL WORK ACP: CORR BEYOND LIM RPL FLR BEAM -Y1292 PER SRM 51-72-11-911-001.

Next page: https://openairdocs.org/aircraft/N571JB/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 = 'N571JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N571JB/reports

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