# Service difficulty reports: N842UA

A list on [N842UA](https://openairdocs.org/aircraft/N842UA.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 3 · 107 reports

- [SDR CALA2026071617843](https://openairdocs.org/sdr/CALA2026071617843.md): Unknown · odor · Jul 15, 2026 · N842UA · Airbus A319131 · Air Distribution System
  > FA REPORTS FUEL ODOR AFT GALLEY ON GROUND AND FOR FIRST 30 MIN OF FLIGHT HAD CREW FILL OUT SMOKE AND ODOR FORM. PREFORMED GVI OF AREA AROUND APU FOR FUEL LEAK. NO FUEL LEAK FOUND. WALKED TO BACK OF A/C TO SEE IF FUEL ODOR WAS PRESENT. NO FUEL ODOR PRESENT. NO
- [SDR CALA2026022514060](https://openairdocs.org/sdr/CALA2026022514060.md): Battery Pack · inoperative · Feb 24, 2026 · N842UA · Airbus A319131 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST FOUND EPSU BATT FAIL MESSAGE ON LIGHT TEST DISPLAY PANEL R&R REAR EPSU BATT REF AMM 33-51-38, COMPLETED ASSOCIATED EPSU LOAD PROGRAMMING PROCEDURE REF AMM 33-51-00. BITE TESTS AND OPS CHECK GOOD.
- [SDR CALA2025112111375](https://openairdocs.org/sdr/CALA2025112111375.md): Gauge · no discrepancy · Nov 19, 2025 · N842UA · Airbus A319131 · Escape Slide
  > R2 DOOR SLIDE GAUGE IS NOT READABLE. R2 DOOR SLIDE GAUGE IS IN THE GREEN BAND AND READABLE.
- [SDR CALA2025082107994](https://openairdocs.org/sdr/CALA2025082107994.md): Warning Message · false activation · Aug 18, 2025 · N842UA · Airbus A319131 · Door Warning System
  > DOOR FWD CARGO ECAM AFTER LANDING OPEN AND CLOSED FWD CARGO DOOR. INSPECTED PROX SWITCH AND CLEANNED TARGET. NO FAULTS NOTED OPEN AND CLOSED INDICATIONS ARE NROMAL IAW AMM 52-31-00-810-801-A.
- [SDR CALA2025063006041](https://openairdocs.org/sdr/CALA2025063006041.md): Warning Message · false activation · Jun 25, 2025 · N842UA · Airbus A319131 · Door Warning System
  > ON LANDING FWD CARGO DOOR UNLOCK WITH ECAM MOMENTARY. SELF CANCELLED IN REF TSM 52-31-00-810-801-A PERFORMED OPS TEST, TEST GOOD. CLEANED PROX SENSORS. NO FAULTS NOTED. OK FOR CONTINUE SERVICE.
- [SDR CALA2025060905379](https://openairdocs.org/sdr/CALA2025060905379.md): Mount · corroded · Jun 6, 2025 · N842UA · Airbus A319131 · Engine Mount Section
  > #1 ENGINE #6 AFT MOUNT OUTER PIN HAS CORROSION. REMOVED & REPLACED #1 ENG #6 AFT MOUNT OUTER PIN IAW A319 AMM 71-22-11-200-804-A 4.A.(7).
- [SDR CALA2025061005429](https://openairdocs.org/sdr/CALA2025061005429.md): Frahm · cracked · May 27, 2025 · N842UA · Airbus A319131 · Fuselage Main, Frame
  > L/H FR16 DOUBLE JOGGLE HOLE #2 HAS A CRACK INDICATION IN THE FRA ME LAYER AT THE 9 OCLOCK POSITION. REPAIRED HOLE #2 AT LH FR16 DBL JOGGLE IAW SRM 53-11-12-300-012.REAMED HOLE 2 TO.3240 ACMP'D HFEC NO DEFECTS NOTED. FINAL REAM #2 HOLE TO.3260.
- [SDR CALA2025061005428](https://openairdocs.org/sdr/CALA2025061005428.md): Frame · cracked · May 27, 2025 · N842UA · Airbus A319131 · Fuselage Main, Frame
  > RH FRAME 16 DOUBLE JOGGLE HOLE #C HAS A CRACK INDICATION IN THE FRAME LAYER @ 6 OCLOCK POSITION VIEW FROM OUTSIDE. RH FR16 DBL JOGGLE IAW SRM 53-11-12-300-012. REAMED HOLE # C TO.2040 ACMP'D HFEC WITH NO INDICATIONS NOTED. FINAL REAM HOLE C TO.2170.
- [SDR CALA2025052905083](https://openairdocs.org/sdr/CALA2025052905083.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A WATER INGRESS INDICATION IN THE TOP SKIN 118 " OTBD 17" FROM TE 3" IN DIAMETER. DRILLED WITNESS HOLES IN L/H ELEVATOR UPPER SKIN 118IN O/B 17IN FROM T/E 1.5IN DIA IAW A319 AMM 55-20-00-200-006-A01 ZONE A. FOU ND NO LIQUID REPAIRED AREA IAW
- [SDR CALA2025052905082](https://openairdocs.org/sdr/CALA2025052905082.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A WATER INGRESS INDICATION IN THE TOP SKIN 78" OTBD 19" FROM TE 2" DIA. DRILLED WITNESS HOLES ON L/H ELEVATOR UPPER SKIN 78IN FROM O/B 1 9IN FROM T/E IAW A319 AMM 55-20-00-200-006-A01 ZONE A. FOUND NO LIQUID. REPAIRED IAW A319 SRM 55-21-11
- [SDR CALA2025052905081](https://openairdocs.org/sdr/CALA2025052905081.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR TOP SKIN HAS A WATER INGRESS INDICATION 109 IN FR OM INBD, 15.5 IN FROM TE, 1"DIA. DRILLED WITNESS HOLES ON R/H ELEVATOR UPPER SKIN 109IN FROM I/B 15.5IN FROM T/E 1.5IN DIA IAW A319 AMM 55-20-00-200-006-A01 ZONE A.FOUND NO LIQUID. REPAIRED IAW
- [SDR CALA2025052805038](https://openairdocs.org/sdr/CALA2025052805038.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A DISBOND IN THE TOP SKIN 31" OTBD 15" FROM TE 1" IN DIAMETER. REPAIRED LEFT ELEVATOR IN THE TOP SKIN 31" OTBD, 15" FROM TE 1" IN DIAMETER AS REQUIRED IAW A319 SRM 05-21-11-300-004A CATEGORY A REPAIR.
- [SDR CALA2025052805037](https://openairdocs.org/sdr/CALA2025052805037.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A WATER INGRESS INDICATION IN THE TOP SKIN 106 " OTBD 17" FROM TE" 3"IN DIAMETER. DRILLED WITNESS HOLES ON LEFT ELEVATOR IN THE TOP SKIN 106" OTBD, 17" FROM TE 3" IN DIAMETER IAW A319 AMM 55-20-00-200-006-A01 Z ONE A FOUND NO LIQUID. REPAI
- [SDR CALA2025052805036](https://openairdocs.org/sdr/CALA2025052805036.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A WATER INGRESS INDICATION IN THE TOP SKIN 92" OTBD 12" FROM TE 3" IN DIA. DRILLED WITNESS HOLES ON LH ELEVATOR UPPER SKIN 92" O/B 12" FROM T/E IAW A319 AMM 55-20-00-200-006-A01 ZONE A. FOUND NO LIQUID. REPAIRED IAW A319 SRM 55-21-11-300-004
- [SDR CALA2025052805035](https://openairdocs.org/sdr/CALA2025052805035.md): Skin · contaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A WATER INGRESS INDICATION IN THE TOP SKIN 82" OTBD 20"FROM TE 3" DIA. DRILLED WITNESS HOLES ON LH ELEVATOR UPPER SKIN 82" O/B 20" FROM T/E 3" IAW A319 AMM 55-20-00-200-006-A01 ZONE A FOUND NO LIQUID. REPAIRED IAW A319 SRM 55-21-11-300-004-A
- [SDR CALA2025052805034](https://openairdocs.org/sdr/CALA2025052805034.md): Skin · debonded · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR TOP SKIN HAS DISBOND 157IN FROM INBD 9.0" FROM TE 1"DIA. REPAIRED RIGHT ELEVATOR TOP SKIN 157" FROM INBD 9.0" FROM TE 1" DIA, AS REQ IAW A319 SRM 55-21-11-300-004A CATEGORY A REPAIR.
- [SDR CALA2025052805033](https://openairdocs.org/sdr/CALA2025052805033.md): Skin · delaminated · May 27, 2025 · N842UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR TOP SKIN HAS A DISBOND 122 IN FROM INBD 16.5IN FR OM TE 1" DIA. REPAIRED RIGHT ELEVATOR TOP SKIN 122" FROM INBD 16.5" FROM TE, 1 " DIA. AS REQ IAW A319 SRM 55-21-11-300-004. CATEGORY A REPAIR.
- [SDR CALA2025061005427](https://openairdocs.org/sdr/CALA2025061005427.md): Gusset · cracked · May 23, 2025 · N842UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LEFT FRAME 68 AT GUSSET STR 16 3RD FASTENER HOLE DOWN HAS CRACK INDICATION IN FRAME LAYER OVER 100% S.H. PER LCQ N/R 9292180/42180. R&R GUSSET AND RPRD 3RD FASTENER HOLE DOWN AT LH FR68 STR16 IAW SRM 53-41-12-300-018 SOLUTION 2. HOLE MEASURED.2514 ACP HFEC
- [SDR CALA2025020302186](https://openairdocs.org/sdr/CALA2025020302186.md): Computer · faulty · Feb 2, 2025 · N842UA · Airbus A319131 · Electrical Power System
  > DURING CRUISE, AN ELECTRICAL ODOR WAS NOTED BY THE CABIN CREW AR OUND ROWS 10-12, A SLIGHT HAZE WAS OBSERVED IN THE SAME AREA. NO SMOKE WAS NOTED EMANATING FROM ANYTHING IN THE VICINITY OF THE HAZE. NO ODOR OR HAZE WAS NOTED IN THE FLIGHT DECK. CHECKLIST 2. 80
- [SDR CALA2025012402005](https://openairdocs.org/sdr/CALA2025012402005.md): Pressure Switch · cracked · Jan 23, 2025 · N842UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > HYD Y ENG 2PUMP LO PR ECAM/RAN ECAM WE DID HAVE PRESSURE FLUCTUA TION AIRCRAFT WAS AT 29K FEET IN CLIMB OUT. WHEN AIRCRAFT ARRIVED AT GATE, YELLOW SYSTEM WAS BELOW NORMAL LIMITS. PRESSURE FLUCTUATION DROPPED AS LOW AS 2300 PSI. FOUND ENG 2 HYDRAULIC PRESSURE S
- [SDR CALA2025012100157](https://openairdocs.org/sdr/CALA2025012100157.md): Skin · cracked · Jan 16, 2025 · N842UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > A/C 4042 FUSELAGE FR2-FR5 LH FWD SKIN HAS DENTS FROM BIRDSTRIKE. ECRA 5311-03323 REV A PART 3 STEP 1 INSTRUCTS TO REQUEST ENGIN EERING TO CONTACT AIRBUS FOR REPAIR INSTRUCTIONS. REQUIRES RFTS. GEN BY V061673 ON HAECO LCQ NR 9296001/34001 MAPPED OUT AND MEASUR
- [SDR CALA2025010201749](https://openairdocs.org/sdr/CALA2025010201749.md): Pump · failed · Dec 29, 2024 · N842UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > HYD Y SYS LO PR YELLOW SYS EMPTY. WILL LOOK FOR LEAKS #2 ENGINE PUMP REPLACEMENT. PERFORMED AMM 29-13-51-860-001-A. PERFORMED FLUID CHECK OF YELLOW SYSTEM PER AMM 29-30-00-200-002-A. FLUID CHECK OK. PERFORMED TEST OF YELLOW HYD SYSTEM PER AMM 29-13-00-710-00
- [SDR CALA2023090402708](https://openairdocs.org/sdr/CALA2023090402708.md): Unknown · faulty · Aug 31, 2023 · N842UA · Airbus A319131 · Air Distribution System
  > VENT SKIN VALVE FAULT EXTRACT VALVE STUCK OPEN. POST FLIGHT FAULT REPORTS "VENT SKIN VALVE FAULT", "VENT BLOWER VALVE (2140HM) REF AMM 21-26-41 NO DEFECTS NOTED OPS CHECK GOOD FAULT" AND "VENT EXTRACT FAULT". T/S REF TSM 21-26-00-810-836-A, NO ECAM STATUS MESS
- [SDR CALA2022120203270](https://openairdocs.org/sdr/CALA2022120203270.md): Power Supply · failed · Dec 2, 2022 · N842UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - FAILED TEST MSG EPSU INT LOAD EMER R CABIN EMEGENCY EXIT POWER SUPPLY WAS BORROWED FROM AMERICAN AIRLINES JFK. PN 3214-54-10, SN 010004, RH POSITION. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1553584
- [SDR CALA2022100302611](https://openairdocs.org/sdr/CALA2022100302611.md): None · none · Oct 2, 2022 · N842UA · Airbus A319131 · Standard Practices/Structures
  > SPILL CLEANUP GENERAL PROCEDURES REQUIRED UNDER AFT GALLEY PER ECRA 2011-01000AB DUP TO LP 9617126 ACCOMPLISHED PAR. 2.A. IMMEDIATE CLEANUP. DIP PAR. 2.B. FOR 7 DIP PER EC 2011-01000 DAYS. OK TO DIP THE IN-DEPTH CLEAN FOR 7 DAYS REF ECRA 2011-01000. TOMC-APPRO
- [SDR CALA2022090502278](https://openairdocs.org/sdr/CALA2022090502278.md): Fitting · none · Sep 5, 2022 · N842UA · Airbus A300* · Empennage Structure
  > DURING REMOVAL OF RUDDER HINGE FITTING #4 DUE TO REPLACEMENT SOME ENLONGATED HOLES WERE FOUND. DO REPAIR TO ENLONGATED HOLES AS PER SRM TASK 55-36-45-300-008 REV.141. AS NOTED ON LTPR NR# 5001174244-0010. REMOVED & REPLACED RUDDER HINGE ARM #4.
- [SDR CALA2022090502265](https://openairdocs.org/sdr/CALA2022090502265.md): Fitting · cracked · Sep 3, 2022 · N842UA · Airbus A300* · Fuselage Main, Frame
  > DURING NDT INSP FOUND CRACK ON CONTINUITY FTG LH/RH. AS NOTED ON LTPR NR# 5001168209-0010. WINDSHIELD FRAME LH & RH CONTINUITY FITTINGS CRACKS WAS REPLACED IAW EO-A32F-53-13777-00-FINAL COVERED BY UAL EC/RA#5311-02867 REPAIR IS PERMANENT CATEGORY A WITHOUT ANY
- [SDR CALA2022090502267](https://openairdocs.org/sdr/CALA2022090502267.md): Door Sill · corroded · Sep 3, 2022 · N842UA · Airbus A300* · Fuselage Structure (General)
  > CORROSION ON R2 DOORSILL FR68. AS NOTED ON LTPR NR#5001169410- 0020. PERFORMED REPAIR ON R2 DOOR SILL BEAM AT FR68 IAW SRM 53-41-14-300-001 REPAIR PRINCILE 7, CAT "A" MAJOR REPAIR WITH NO ADDITIONAL REQUIREMENTS REFER TO PREVIOUS SIGN OFF FOR WORK PERFORMED. W
- [SDR CALA2022090502266](https://openairdocs.org/sdr/CALA2022090502266.md): None · corroded · Sep 3, 2022 · N842UA · Airbus A300* · Fuselage, Stabilizer Attach Fittings
  > STRINGER RH 41 FR 61-63 CORRODED, REQUIRES FURTHER EVALUATION. AS NOTED ON LTPR NR# 5001170029-0010. CORRODED STRINGER AND SECTION-CONNECTING BTW FR.61-63, STGR.41RH INSPECTED BY HT1218. PERFORMED REPLACEMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11 REV.142.
- [SDR CALA2022090502263](https://openairdocs.org/sdr/CALA2022090502263.md): Battery · none · Sep 2, 2022 · N842UA · Airbus A300* · Lighting System
  > DURING EMERGENCY BATTERY CAPACITY TEST; EPSU BATTERY (11WL) FAIL TEST AND NEED TO BE REPLACE. AS NOTED ON LTPR NR# 5001168100-0010. EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTING BATTERY CAPACIT P/N ON:AD3214-31, S/N ON:261200, QTY:1EA, B/N ON:N842UA3133. Y
- [SDR CALA2022090502262](https://openairdocs.org/sdr/CALA2022090502262.md): Battery · none · Sep 2, 2022 · N842UA · Airbus A300* · Lighting System
  > DURING EMERGENCY BATTERY CAPACITY TEST; EPSU BATTERY (13WL) FAIL TEST ND NEED TO BE REPLACE. AS NOTED ON LTPR NR# 5001168102-0010 EPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTING BATTERY P/N ON: AD3214-31, S/N ON: 287722, QTY:1EA B/N ON:N842UA3135. CAPACITY TE
- [SDR CALA2022090502261](https://openairdocs.org/sdr/CALA2022090502261.md): Battery · none · Sep 2, 2022 · N842UA · Airbus A300* · Lighting System
  > DURING EMERGENCY BATTERY CAPACITY TEST; EPSU BATTERY (10WL) FAIL TEST AND NEED TO REPLACE. AS NOTED ON LTPR NR# 5001168079-0010 EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTING BATTERY P/N ON:AD3214-31, S/N ON: 287719, QTY:1EA, B/N ON:N842UA3134. CAPACITY TEST
- [SDR CALA2022090502260](https://openairdocs.org/sdr/CALA2022090502260.md): Battery · none · Sep 2, 2022 · N842UA · Airbus A300* · Lighting System
  > DURING EMERGENCY BATTERY CAPACITY TEST; EPSU BATTERY (12WL) FAIL TEST AND NEED TO BE REPLACE. AS NOTED ON LTPR NR# 5001168101-0010 EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTING BATTERY 1EA. P/N ON: AD3214-31, S/N: ON:273394, QTY:1EA, B/N ON: N842UA3 CAPACIT
- [SDR CALA2022090502256](https://openairdocs.org/sdr/CALA2022090502256.md): None · cracked · Sep 2, 2022 · N842UA · Airbus A300* · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON RH FR16 UPPER HOLE #6 DOUBLE JOGGLE FASTENER HOLE. EVALUATE AND REPAIR AS NECESSARY IAW APPLICABLE REPAIR MANUALS. AS NOTED ON LTPR NR #5001169542-0010. REVISION OF ECRA 5311-02860 ON OR BEFORE 31176 TTL FLT CYC''S AND THERE AFTER REP
- [SDR CALA2022090502255](https://openairdocs.org/sdr/CALA2022090502255.md): Skin · dented · Sep 2, 2022 · N842UA · Airbus A300* · Wing, Landing Gear Attach Fittings
  > LH SLAT #2 LEADING EDGE DENTED, FURTHER EVALUATION REQUIRED. A3NB-05-3-6103 XONE:500 SEQ:1391. AS NOTED ON LTPR NR#5001170241 -0010. DENT FOUND BEYOND ALLOWABLE LIMITS IAW A319 SRM REPORTING. 57-40-00-283-001. AREA REPAIRED IAW A319 SRM 57-40-00-300-221 AND CO
- [SDR CALA2022090502254](https://openairdocs.org/sdr/CALA2022090502254.md): Fitting · none · Sep 2, 2022 · N842UA · Airbus A300* · Empennage Structure
  > THE FOLLOWING ITEMS ARE OR MAY BECOME OVERTIME: 13) TASK, A319, ()A-CK ESCALATION 6A1 TO 4A1 PHZ-IN 17-0552-8-0045 14) TASK, A319, ? HYD PWR SYS ACCUM VCK IOL 1C1 17-0529-8-0029 15) TASK, A319, MAG CHP DET / ENG START SVC IOL 1A1 17-0579-8-0001 16) TASK, A319
- [SDR CALA2022082402153](https://openairdocs.org/sdr/CALA2022082402153.md): Slat · damaged · Aug 24, 2022 · N842UA · Airbus A319131 · Leading Edge Slat Control System
  > RH SLAT #3 TRACK #7 LOWER FWD ANTI-ROTATION STOP DAMAGED, FURTHER EVALUATION REQUIRED. AS NOTED ON LTPR NR#5001171165-0010 PERFORMED REPAIR ON RH SLAT #3 TRACK RIB #7 AS PER A319 SRM TASK 57-40-00-300-112 REV 142. THE REPAIR IS CLASSIFIED AS MAJOR CATEGORY "A"
- [SDR CALA2022082402152](https://openairdocs.org/sdr/CALA2022082402152.md): Slat · damaged · Aug 24, 2022 · N842UA · Airbus A319131 · Leading Edge Slat Control System
  > RH SLAT #3 TRACK #7 LOWER FWD ANTI-ROTATION STOP DAMAGED, FURTHER EVALUATION REQUIRED. AS NOTED ON LTPR NR#5001171165-0010 PERFORMED REPAIR ON RH SLAT #3 TRACK RIB #7 AS PER A319 SRM TASK 57-40-00-300-112 REV 142. THE REPAIR IS CLASSIFIED AS MAJOR CATEGORY "A"
- [SDR CALA2022081602104](https://openairdocs.org/sdr/CALA2022081602104.md): Skin · dented · Aug 15, 2022 · N842UA · Airbus A319131 · Fuselage Floor Panel
  > DENT LH FR 28-29 STGR 38-39, REQUIRES EVALUATION AS PER A319 SRM TAS 53-21-11-283-020 REV.141. AS NOTED ON LTPR NR# 5001172215-0010. 53-21-11-205-068. INSPECTION THRESHOLD FROM EMBODIMENT 60000FC & FH. REF SRM 53-21-11-300-087 AND SRI 53-21-11-205-068 FOR REPA
- [SDR CALA2022081602101](https://openairdocs.org/sdr/CALA2022081602101.md): Fitting · cracked · Aug 15, 2022 · N842UA · Airbus A319131 · Fuselage Main, Frame
  > HOLES #1 AND #3 INTERCOSTAL FITTING 7 FR15-16 RH FOUND WITH CRACK. AS NOTED ON LTPR NR#5001169091-0010. EVALUATED THE INTERCOSTAL AT RH FR16 #7 DOOR STOP HOLES #1 #3, REMOVED FITTING AND REAMED HOLES PER DRW R53113118, SRM 51-42-11 & SRM 51-44-11, CRACK STILL
- [SDR CALA2022081602100](https://openairdocs.org/sdr/CALA2022081602100.md): Fitting · cracked · Aug 15, 2022 · N842UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > HOLES #1 AND #3 INTERCOSTAL FITTING 7 FR15-16 LH FOUND WITH CRACK. AS NOTED ON LTPR NR# 5001169092-0010 EVALUATED THE INTERCOSTAL AT LH FR16 #7 DOOR STOP HOLES #1 & #3, REMOVED FITTING AND REAMED HOLES PER DRW R53113118, SRM 51-42-11 & SRM 51-44-11, CRACK STIL
- [SDR CALA2022081002013](https://openairdocs.org/sdr/CALA2022081002013.md): Door Sill · corroded · Aug 8, 2022 · N842UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > DURING INSPECTION OF THE AFT ENTRANCE AREA SEVERAL SPOTS OF CORROSION WERE FOUND ON R2 DOOR STILL BTW FR 66-68. (A3NB-53-3-6222, ZONE 262, SEQ#2102) AS NOTED ON LTPR NR# 5001169410-0030. THE REPAIR PERFORMED ON R2 DOOR SILL BEAM FR66 IS MAJOR PERMANENT CATEGOR
- [SDR CALA2022080801985](https://openairdocs.org/sdr/CALA2022080801985.md): None · corroded · Aug 5, 2022 · N842UA · Airbus A300* · Fuselage, Stabilizer Attach Fittings
  > AFT CRG THRESSHOLD CORRODED, REQUIRES FURTHER EVALUATION. A3NB-05-3-6022. SEQ#9 ZONE #153. AS NOTED ON LTPR NR# 5001170024-0010.
- [SDR CALA2019091701556](https://openairdocs.org/sdr/CALA2019091701556.md): Brake · leaking · Sep 16, 2019 · N842UA · Airbus A319131 · Brake
  > LEAKING LEFT OUTBOARDBRAKE ON THE LEFT MAIN GEAR. FOUND ON WALK AROUND. REPLACED BRAKE PER AMM 32-42-00-860-070-A SER # ON 1684 SER# OFF4962
- [SDR CALA2019062701066](https://openairdocs.org/sdr/CALA2019062701066.md): Skin · gouged · May 23, 2019 · N842UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > GOUGE FROM FRAMES 8 TO 13.5, ABOVE STRINGER 23L. BLENDED AND PERFORMED DVI. NO DEFECT NOTED. ACCOMPLISHED LEFT FUSELAGE SKIN INTERIM REPAIR IAW EC/RA 5331-02392.
- [SDR CALA2017100903573](https://openairdocs.org/sdr/CALA2017100903573.md): Power Supply · faulty · Oct 9, 2017 · N842UA · Airbus A319131 · Emergency Lighting
  > ACCOMPLISHED EMERGENCY LIGHT TEST, TEST FAILED. FAULTED FOR INTERIOR LIGHTS FWD. FOUND ESPU AT THE L1 DOOR FAULTING, REPLACED ESPU IAW AMM 33-51-38-00-001. TEST PASSED.
- [SDR CALA2017100903572](https://openairdocs.org/sdr/CALA2017100903572.md): Power Supply · malfunctioned · Oct 9, 2017 · N842UA · Airbus A319131 · Emergency Lighting
  > DURING A CIDS EMERGENCY LIGHT TEST, MAINTENANCE MESSAGE EPSU EXT LOAD FWD L DISPLAYED. RESET EPSU 10WL. OPS CHECKED GOOD.
- [SDR CALA2017100903571](https://openairdocs.org/sdr/CALA2017100903571.md): Light · no test · Oct 9, 2017 · N842UA · Airbus A319131 · Emergency Lighting
  > ESPU EMERGENCY EXT L, CIDS FAULT DURING A NR 2 SERVICE EMERGENCY LIGHT TEST. FOUND BOTH LEFT OVERWING LIGHTS FAILED. REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-15-000-001, ACCOMPLISHED IDT INSPECTION IAW GMM 09-10-05 AND AMM 33-51-38-00 -01. NO DEFECTS NOTED.
- [SDR CALA2017081802739](https://openairdocs.org/sdr/CALA2017081802739.md): Oven · odor · Aug 18, 2017 · N842UA · Airbus A319131 · Buffet/Galleys
  > FLT ATT. REPORTED A BURNING RUBBER SMELL NEAR THE FWD AFT LAV. GALLEY POWER SWITCH WAS SWITCH SHUT OFF AND SMELL DISSIPATED. ACCOMPLISHED CHK PER AMM05-51-10-200-801C1. ALL ELECTRICAL EQUIPMENT WAS OPERATED IN AFT CABIN AND GALLEYS. CHECKED CABIN AND GALLEYS A
- [SDR CALA2017063002059](https://openairdocs.org/sdr/CALA2017063002059.md): Light · malfunctioned · Jun 30, 2017 · N842UA · Airbus A319131 · Emergency Lighting
  > EXIT LIGHT ON IN EXIT ROW. CYCLED EMERGENCY EXIT LIGHT SWITCH. LIGHTS EXTINGUISHED. OPS NORMAL.

Next page: https://openairdocs.org/aircraft/N842UA/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 = 'N842UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N842UA/reports

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